Supercritical CO2 Extraction of Oil from Henna Flower ...
Transcript of Supercritical CO2 Extraction of Oil from Henna Flower ...
United Arab Emirates UniversityScholarworks@UAEU
Theses Electronic Theses and Dissertations
4-2012
Supercritical CO2 Extraction of Oil from HennaFlower: Experimental, Mathematical Modeling,and Antioxidant ActivityBushra Saeed Mohammed Dohai
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Recommended CitationMohammed Dohai, Bushra Saeed, "Supercritical CO2 Extraction of Oil from Henna Flower: Experimental, Mathematical Modeling,and Antioxidant Activity" (2012). Theses. 581.https://scholarworks.uaeu.ac.ae/all_theses/581
Faculty of Engineering
United Arab Emirate Univer ity
Faculty of Engineering
Q l.:UAIl Q..;! .. U5U' LJ IJ La � I ii.sto l.;l United Arab Emirates University
M.Sc. Program in Petroleum Science & Engineering
SUPERCRITICAL CO2 EXTRACTION OF OIL FROM
HENNA FLOWER: EXPERIMENTAL, MATHEMATICAL
MODELING, AND ANTIOXIDANT ACTIVITY
By
Bushra Saeed Moham med Dohai
A thesis Submitted to
United Arab Emirates University
In Partial fulfilment of the requirements
For the Degree ofM.Sc in Petroleum Science & Engineering
April 20 12
Faculty of Engineering
United Arab Emirates University
Faculty of ngineering
oll1All Ci..M J.StII w IJ La � I Cuto l.;1 United Arab Emirates University
M. c. Program in Petroleum Science & Engineering
SUPERCRITICAL CO2 EXTRACTION OF OIL FROM
HENNA FLOWER: EXPERIMENTAL, MATHEMATICAL
MODELING, AND ANTIOXIDANT ACTIVITY
By
Bushra Saeed Moham med Dohai
A thesis Submitted to
United Arab Emirates University
In Partial fulfilment of the requirements
For the Degree of M.Sc in Petroleum Science & Engineeling
Supervisor Ali H . Al Marzouqi
Associate Professor in chemical Engineering
Department of Chemical & Petroleum Engineering
Collage of Engineering
United Arab Emirates University
April 2012
ABST RACT
Henna i a plant that ha been u ed tradit ional ly [or coloring nai l , kin, and hair,
and a medicinal plant. The upercritical fluid technology offers a con iderable promi e
a e traction media due to it ad antage 0 er other conventional e traction technique .
The extraction of volat i le components from flower of henna wa tudied using
upercri t ical carbon dioxide at temperatures and pres ures ranging from 35 to 55°C and
80 to 1 20 bar, re pect ively. A maximum extraction yield of 3 1 % from 2g of henna
flower was obtained at 45 °C and 1 20 bar. The composition of the extracts was
inve t igated by gas chromatography technique. Furthem10re, the extract were te ted for
their antibacterial and ant ioxidant activit ies . No inh ibit ion zone was ob erved in the
antibacteria l study; however the extracts obtained at most of the extraction conditions
exhibited antiox idant activity.
A mathematical model of the extraction curve based on mass transfer principles
was developed at all extract ion conditions. Powell optimization method \ as used to
obtain the model parameters by adj usting to experimental results. The calculated
e tract ion yields were in good agreement with experimental results .
I
ACIC TO\VL E D G E I\lE � T
Prai e be to God for h i unl imited grace and help to complete the requirement of
thi work.
Fir t and [oremo t , I would l ike to extend my deepest gratitude to my supervi or
Dr. Ali Al Marzouqi [or hi guidance, encouragement valuable suggestion , upport, and
advi e that are u eful in personal and profes ional l i fe. I would especially l ike to thank
him [or haring hi knowledge in supercritical fluid extraction ( SFE), e sential oi l
maU1ematicai model ing, and programming.
econdly, 1 would l ike to thank the assistance of the fol lowing individuals who
upported me in the analysis, Dr. Agnes Sonnevend from Faculty of Medicine and Health
c ience for her a i tance in conducting the antibacterial test . I thank Mr. Babucarr lobe,
and Mr. Saj id Maqsood from Faculty of Food and Agriculture for sharing their
knowledge on conducting antioxidant tests. The assistance of Dr. Ali Dowaidar in Gas
Chromatography and part icle characterization is al 0 great ly appreciated.
I would l ike a lso to thank my close friend Eng. Hanifa Taher; a PhD tudent from
Chemical and Petroleum Engineering Department for her support and assistance on using
End ote oftware. Al 0 I would l ike to acknowledge my friend Negin Farah, a master
tudent from Chemical and Petroleum Engineering Department for reviewing the Engl ish
wri t ing of thi thesis.
Also, I wish to thank a l l the faculty members and staff of the Chemical and Petroleum
Engineering Department at UAE University for supporting me during my research
studies.
Last but defmite ly not the least ; I thank my family members, who I can never thank
enough for bel ieving in me and helping me to go through the chal lenging period of my
studies at UAE University.
I I
TABL E O F C Ol TT E , TTS
B TRACT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1
A K OWLEDGEME T . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ll
T BLE OF CO TE T . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. . . . . . . . . . . . . I I I
L I T O F F IGURE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. . . . . . . . . . . . . . . . . . .. .. . . . . . . . . . . . . . . . . . . . . . . . . .. . . . . . . . . . . . . . . . . . .. V I
L I T OF TABLES . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. . . . . . . . . . . . . . . . . . V I I I
onlenclature . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IX
1 TRODUCTIO . . . . . . . . . . . . . . . . . . . . . .. . . . . . . . . . . . . . . . .. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1
1 . 1 Problem tatement . . . . . . . . . . . . . . . . . . .. . . . . . . . . . . . . . . . . . . . . . . . . . . . .. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1
1 .2 Scope . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2
1 .3 Objectives . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2
2 BACKGROUN D AND L ITERATURE SURVEY . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3
2 . 1 Henna plant ( Syn. Lawsonia inerrnis Linn. Lytheraceae ) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3
2 .2 Supercrit ical fluids ( SCFs) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5
2 .3 Extraction Technologies . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 0
2 .3 . 1 Soxhlet Extraction . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 1
2 . 3 . 2 Hydrodist i l lat ion . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 2
2 . 3 . 3 Microwave- Assisted Extraction (MAE) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 3
2 . 3 .4 Supercritical Fluid Extraction ( SFE) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 4
2 . 3 .4 . 1 Extraction parameters . . . . . . . . . , . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 6
I I I
2 .3 .4.2 Mathematical Model ing . . . . . .. . . . . . . . .. . . . . . . .. .. . . . . . . . . . . . . . .. . . .. . . . . . . . . . . . . .. . . . . . . . . . . . . 1
2 .3A.2 . 1 olubi l i t of olute in upercritical fluid pha e . . ..... . . . . . . . . . . . . . . . . . . . . . . . 1 9
2 .3 .4 .2 .2 Model ing the e tract ion curve ..... . . . . . . . . . . . . . . .. . . . . . . . . . .. . . . . . . . . . . . . . . . . . .. . . . . . . 25
3 E PERIME TAL ET P AND METHODOLOGI E .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ... . . . 35
3 . 1 ample preparation . . . . . . . . . . . . .. . . . . . .. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ..... 35
3 .2 Supercri tical fluid e traction . . . . . . . . . . . . . . . . . . . . .. . .. . . . . . . . . . . . . . . . . . . . . ..... . . . . . . . . . . . . . . . . . . . . . . .. . . . 3 5
3 .3 Ga Chromatography analy is . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 36
3 . 4 Antibacterial Activity Test . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 37
3 . 5 Antio idant Acti ity test . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. . . 37
3 . 5 . 1 FRAP ( Fenic reducing antioxidant power) assay . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 37
3 . 5 .2 DPPH radical scavenging activi ty . . . . . . . . . . . . . . . . . ... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 38
4 RESU LTS AND DISCUSS ION . . . . . . . . . . . .. . . . . . . . .. . . . . . . . . . . . . . . . . . . . . . . . . . . ........ . . . . . . . . . . . . . . . . . . . .. . . 39
4. 1 Supercri t ical carbon dioxide extraction of henna flower.. . . . . . . . . . . . . . . . . . . ..... . . . . . . . . . 39
4 . 1 . 1 Effect of temperature . . . . . . . . .. . . . . . . . . . . . . . . . . . . . . . . . . . . . .. . . . . . . . . . . . . . . . .. . . . . . . . . . . . . . . . . . . . . . . . . . . 43
4 . 1 .2 Effect of pressure . . . . . . . . . .. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .... . . . . . . . . . .. . . . . . . . . . . . . . . . . . . . . . . 48
4 .2 Extract Analysis . . . . . . . . . . . . . . . . . ... . . . . . . . .. . . . . . . . . . . . . . . . . . . . . . . . . . . . . ... . . . . . . . . . . . . . . . . . . . . . . . . . . .. . . . . . . . . 50
4 .2 . 1 GC-Analysis . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ... . . . . . . . . . . . . . . . . . . . . . . .. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 50
4 .2 .2 Antibacterial activity . . . . . . . . . . . . . . . . . . . . . . . . . . .. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . · . . . . . . . . . . . . . . . . . . . . . . . .. 54
4 .2 .3 Antiox idant act ivi ty . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 55
4 .2 .3 . 1 FRA P ( Ferric reducing ant ioxidant power) assay . . . . . . . . . . . . . . . . . . . . . .. . . . . . . . . 55
IV
4.2 .3 .2 DPPH cavenging acti i ty . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 57
5 D T MODELL G . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 60
5 . 1 De cliption of the e traction mechanism . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 60
5 .2 Theoret ical principle of the extraction proces . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6 1
5 .2 . 1 Part ic le Pha e rn a tran fer . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 62
5 .2 . 1 . 1 Transfer of solute from solid phase . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 62
5 .2 . ] .2 Di ffu ion within part ic le pores . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 65
5 .2 .2 F lu id Phase mas tran feL . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 67
5 .2 .2 . 1 F i lm d iffu ion . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 68
5 .2 .2 .2 Bu lk d iffu ion along the extraction bed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 68
5 .2 .2 . 3 Model parameters . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 72
6 MODEL IN G RESU LTS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 74
7 Conclu ion and recommendations . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 78
8 REFERENCES . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 80
9 APPEND ICES . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 89
v
L I ST O F F I G URES
Figure I Pha e diagram of O2 . .. . . . .. . . . . .. . . . . .. . . . . .. . . . . . . . . . ... .. . . . . .. .. . . . . . . . . . . ... . . .. . . ....... . . . . .. . . .. . . .. . . 6
FIgure 2 The change in den ity of CO2 with pre ure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7
Figure 3 oxhlet Extractor . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 2
Figure 4 chmatic diagram of SFE apparatus . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 5
Figure 5 Supercri tical Extraction Experimental Set up . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 36
Figure 6 Effect of cool ing temperature a t 45 °C and 1 00 bar.. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4 1
Figure 7 E ffect o f cool ing temperature at 55 °C and 80 bar.. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4 1
Figure 8 Effect of flow rate at 55 °C and 1 00 bar . . . . . . . . . . . . ... ..... . . . . ... .. . . .. . .. . . . . . . . . . . . . . .. . . . . . . . ... 42
Figure 9 E ffect of £10\ rate at 55 °C and 1 20 bar.. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 43
Figure 1 0 Effect of temperature on the extraction yield at 80 bar.. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 44
Figure 1 1 E ffect of temperature on the extraction yield at 1 00 bar . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 45
F igure 1 2 E ffect of temperature on the extraction yield at 1 20 bar . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 46
Figure 1 3 Effect of temperature and pressure on solubi l ity of henna flower extract in SC-
CO'2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 48
F igure 1 4 E ffect of pressure on the extraction yield at 3 5 °C . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 49
F igure 1 5 Effect of pressure on the extraction yield at 3 5 °C . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 49
Figure 1 6 Effect of pressure on the extraction yield at 55 °C . . . . . . . . . . . . . . . . . . . . . . . . .. . . . . . . . . . . . . . . . . . 50
Figure 1 7 GC chromatogram for extract obtained at 55 °C and 1 20 bar . . . . . . . . . . . . . . . . . . . . . . . . . . 5 1
Figure 1 8 Results of antibacterial test. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. .. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 55
Figure 19 FRAP Reduction reaction . . . . . . . . . . . . . . . . . . . . . . . . . . .. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 55
Figure 20 FRAP assay results for extract of henna flowers . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 56
Figure 2 1 DPPH reduction by antioxidant . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 58
VI
Figure 22 DPPH a ay re ull for extract of henna flower . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5
Figure 23 Mechani rn of FE proce . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6 1
Figure 24 lnterpha e rna tran fer rnechani rn . . . . , . . . . . . . . . . . . . . ' . . . . . . . . . . . . . . . . . . , . . . . . . . . . . . . . . . . . . . . . . . . . 63
Figure 25 Ma tran fer in the pat1icle pha e . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 65
Figure 26 Fluid phase rna transfer rnechani 111 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 68
Figure 27 Ma tran fer in the fluid pha e . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 69
Figure 28 Extraction curve at 80 bar . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 75
Figure 29 Extract ion curve at 1 00 bar . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 76
Figure 30 Extraction curve at 1 20 bar . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 76
Figure 32 Cal ibrat ion curve for FRAP as ay . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 03
Figure 33 Cal ibrat ion curve for DPPH as ay . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 03
V I I
L I ST O F TABL E S
Table 1 Major volat i le component i n henna flower (Wong & Tong, 1 995 ) . . . . . . . . . . . . . . . . . . . . . 5
Table 2 Some of the phy ical properties of ga , l iquid and upercritical fluid . . . . . . . . . . . . . . . . . . . 6
Table 3 Most Common upercritical fluid . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9
Table 4 Maximum yield and olubi l ity of SFE of Henna flower extract . . . . . . . . . . . . . . . . . . . . . . . . 40
Table 5 Compo it ional analy i of extract from henna flower by GC . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 52
Table 6 Adju table model parameters . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 77
V I I I
F
FE
G
H PLC
T
P
C
q
r
R
L
� o menclatu re
Supercri t ical Fluid
upercritical Fluid E traction
upercri tical carbon dio ide
Ga Chromatography
High Pre sure Liquid Chromatography
Temperature, Kelvin
Pres ure, bar
Bed poro ity
Particle poro ity
Concenh"ation of solute in the partic le phase, kg/m3
Init ia I Concentration of solute in the particle phase, kg/m3
Concentration of solute at the particle surface, kg/m3
Concentration of solute in the fluid phase, kg/m3
Init ia l concentration in the fluid phase, kg/m3
Concentration of solute in the sol id phase, kg/m3
Init ia l Concentration of solute in the solid phase, kg/m3
Part ic le diameter, m
Particle radius, m
Bed rad ius, m
Bed length, m
IX
D
A
F
z
M ample
y
pc
pr
�r
Dax
Bed diameter m
Bed era ectional area, m2
Bed volume m3
Flo\ rate of C-C02, kg/s
uperfi ia! e!ocity, rnls
Inter t it ia! e!ocity, ml
Axial coordinate, m
Weight of charged sample, kg
I nit ial rna s in the ample, Kg
Extraction yield percentage
fraction of oi l ini t ia l ly dissolved in the fluid phase
Density of SC-C02, kg/m3
Vi cosity of SC-C02, Pa.s
Cri t ical temperature of CO2, K
Critical volume of C02, m3/mol
Critical density of CO2, kg/m3
Crit ical iscosity of CO2 Pa.s
Reduced density of CO2
Reduced viscosity of CO2
Axial d iffusivity coefficient, m2/s
Effect ive d iffusivity coefficient, m2/s
x
K
r
r
z
l
Film coefficient mJ
E · l ·b· 3 / 3 qUl \ num con tant, m \Old m sp
Ad . ffj · -\ � / ] orphon coe lC lent, s m- \old m- s.p
Radiu coordinate, m
ize of part ic le increment, m
ize of bed increment, m
Time increment, m
Number of particle increment
umber of bed increments
Number of time increments
X l
1 I N T R O D U C T I O N
1 .] Problem tatemen t
Henna plant (Lawsonia inermis) extracts have historical u age in cosmetic and
medicine field . The plant extract give temporary color, which is used for tattooing
e pecia l ly in Middle Ea t region. Moreo er, the extract of henna exhibit biological
act i \ itie , including antimicrobial , antioxidant, and anticancer activities.
onventional ly, chemical 01 ents are employed for extraction of components
from henna lea e , seeds, and roots. Only few studies are avai lable for the extraction
from henna flower using olvent extraction . These toxic and expensive chemical
olvents hinder the explorat ions on valuable extracts from henna. Furthermore, separat ion
proce es are not efficient enough, and are risky, especia l ly when extracts are used for
food or medicine. Moreover, volat i le components can thermal ly degrade i f other
conventional techniques such as steam dist i l l ation are used.
The supercritical fluid technology is a pronlls lllg field, which has in some
application replaced the traditional extraction techniques. This is typical ly due to the
favorabl e transport properties of supercritical fluids. In part icular, supercritical carbon
dioxide has gained a great deal of attention since it is nontoxic, inexpen ive, inert
chemical and nonflammable. In addition to these properties, supercritical conditions of
carbon dioxide are eas i ly reachable ( 3 1 °C and 73 bar).
1.2 cope
upercri tical carbon dioxide can be uti l ized to extract olati le component from
henna flowers with comparable quality and yield to conventional e traction technique .
Furthermore, the effect of e traction on e tract o lubi l ity and yield i inve t igated. The
phy ical trend of the extract ion cur e i tudied by proposing a mathematical model
ba ed on law of con ervation of rna s.
1.3 Objecth es
The main target of this thesis is to examine the validity of supercritical fluid to
extract olati le component of henna flowers. This main target has the fol lowing specific
target :
I. Optimization of supercrit ical extraction condit ions.
2 . Compositional analysis of the extracts by gas chromatography
3 . I nvestigation o f antibacterial and ant ioxidant act ivities of the extract .
4 . Development of mathematical model for the supercrit ical extraction process.
2
2 B ACKG ROU D AND L I T E RATURE URVEY
2 . 1 Henna plant (S n . La" son ia i nermis Linn. L� theraceae )
Henna i a flowering plant grown in dry tropical and ubtropical region uch a
Middle East, OJ1h Africa, India and Sri lanka. The plant extract are traditional ly u ed
for cosmetic purpo e and appl ied to hands, feet, nai ls and hair to give temporary color.
The major component of the extract is the lawsone (2-hydroxy- I 4-naphtboquinonel )
which i the dying molecule that uppl ie red-orange pigment. In addition it is used to
reduce body temperature in case of high fever. Hanna's extracts are prepared by finely
grinding the dried leaves and mix ing them with water at room temperature.
In addit ion to the cosmetic purposes, henna is considered as medicinal p lant since
the extracts showed biological acti it ies including antimicrobial (Hsouna et aI . , 20 1 1 ;
Ja l lad & Espada-Jal lad, 2008; Priya et a I . , 20 1 1 ), ant i fungal (Chaudhary et aI . , 20 1 0;
Shanna & Shanna, 20 1 1 ), anti- in flammatory and antipyretic ( BH . et a I . , 1 995; Mikhaeil
et aI . , 2004), and antiox idant (Hsouna et aI . , 20 1 1 ; Uddin et aI . , 20 1 1 ) . Henna extracts are
used a medicine for jaundice, leprosy smal lpox, and skin complaints. Moreover it was
a serted by Priya and co-authors that the ethanol extracts of henna roots exhibited
sign ificant antitumor activ ity, which explained the fact that henna has a long history for
the treatment of cancer (Priya et a I . , 20 1 1 ) .
The leaf extracts took the attention of most henna investigators. The biological
activ ities of the leaf extracts from henna trees were scanned . Anis and his col leagues
figured out that the chemical components of L . inennis leaves have good antiox idant
capacities, and it is possible to use those extracts as a potential source of new natural
3
antioxidant ( H ouna et a I . , 20 ] 1 ) . Furthermore. leaf ample were analyzed for their
antimicrobial potential and showed obviou antibacterial activity again t E cherichia coli
( H ouna et a I . , 20] I; Jal lad & � pada-JaUad, 200 ; Priya et at. , 20 1 1 ) . Be ides, isolation
of Law one from lea e ' e tract revealed trong antifungal activity (Sharma & Shanna,
20 1 1 ) . The extract hO\ ed anticancer act ivi ty a wel l against l iver and colon cancer cel l
(Endrini et a I . , 2007; Uddin et a I . , 20 1 1 ) .
On the other hand there is only one tudy publ ished on the flower part. Wong and Tong,
1 995 e tracted the volati le component of helIDa flowers by solvent extraction. They
analyzed the extract and identified the major components by GC and GC-MS for red and
yel low flower . The research re ealed the presence of volat i le components in the yel low
flower uch as: (E)-3 -hexenol , diethyl oxalate, ! inalool, dihydro-�- ionone, benzyl
alcohol , 2-phenylethanol, �- ionone, and dih ydro-�-ionol . Other volat i le components were
detected in the red flower including' hexanal , eugenol , and ethyl l inolenate. Volatile
component in yellow and red henna flowers with their corresponding composi t ion are
presented in Table 1 .
4
Table I �ajor \ olatllc component. in henna flo\\ er (\\ ong &. Tong. 1 995)
Component Compo ition in yellow flower (wt %) Compo ition in red flower (wt 00) Hexanal - 1 .4
He anol 1 .6 1 . 5
(E)-2-hexenal - 5 .4
( E)-2-hexenol - 2.2
(E)-3 -hexenol 5 .4 3
Diethyl oxalate 1 .4 3 . 1
Linalool 1 9. 8 1 2 .7
Methyl sal icylate - 1 . 8
Ethyl nicotinate - l .2
Dihydro-�-ionone 2 . 5 -Benzyl alcohol 3 . 3 6
2-phenylethanol 5 .8 1 1 . 5
�-ionone 48 .6 2 .5
D ihydro-�-ionol 1 .4 -
Eugenol - 1.1 Ethyl palmitate - 1 . 1
Ethyl l inoleate - 2 . 5
E thyl l inolenate - 8.9
2.2 Supercritica l fluids (SCFs)
A supercritical fluid is a substance beyond its critical pressure and temperature
\ here only one phase exists. Figure 1 i l lustrates a phase diagram for carbon dioxide.
SCF physical and chemical properties intennediate between gases and l iquids . As
indicated in
Table 2, SCFs have d iffusivit ies h igher than pure l iquids, and v iscosities h igher than
those for pure gases. A SCF has the gaseous property of being able to penetrate and the
l iquid property of being able to dissolve materia ls into their components. SCFs possess
5
no urface ten ion hence no capi l lary force wi l l appear during extraction. The olvating
power of the F fol low the change in the den ity.
1 00
90
0 Critical Poin
Supercritical Fluid
,-.. 70 '- --�-----(31.5°C,73.9 ar) '" .:J 60 '-' (J
50 '-=' '"
40 Sol id '" (J ... Q. 30
20
10
0 -78.5
LiQu i d /
Gas
-33.5 - 1 8 .5 -3.5 1 1 .5 26.5
Temperature °C
FIgure I Pha e dIagram of CO2
- SublImation - Melting
Vaporization
Table 2 ome of the ph) ical properties of gas. l iquid and supercritical fluid
Phy ical State Density (kg/m3) Viscosity ( cp) Diffusivity (mm2/s)
Gas 1 0.0 1 1 - 1 0 Supercritical Fluid 1 00-800 0 .05 -0. 1 0.0 1 -0. 1
Liquid 1 000 0.5- 1 0 .00 1
AroUfld the critical point, the density, v iscosity and diffusivi ty of the fluid are tunable and
sensit ive to pre ure, for example, a smal l change in the pressure results in large changes
in densit ies and hence large change in the solvating power of the fluid. Figure 2 presents
the change of density of carbon dioxide with pressure at 1 5 DC and 32 DC . It is c lear from
the figure that at 1 5 DC, pressure has smal l influence on density of the fluid, however at
32 DC, which i close to the critical temperature; the change is drastic around the critical
pre ure ( 73 .9 bar).
6
uch combination of fluid propertie provide the dri e for applying CF a a
preferable alternat ive to conventional organic olvent . The higher diffu ion coefficient
of F compared to that of l iquids al lows SCF to penetrate into ol id material easier
than organic olvent . ince the density can ea i ly be control led by pres ure, eparat ion
of ub tance [rom F is ea y to handle which reduces separation costs. In addition to
the e benefit , the olubi l i ty in S F can be enhanced by adding modifiers to change the
fluid polarity and impro e it electivity. Different supercritical fluids are l i sted in Table
3 with their corre ponding critical conditions and appl ications.
900 • • • • • • • a( 15"C .., a(32 E ....... ao 600 ..lO:
>- _Vapor -'iii c:
300 �Supercritical QJ 0 Liquid
a
60 80 100
Pressure (bar)
Figure 2 The change in den lty of CO:c \\ Ith pressure
Among a l l l i sted supercritical fluids in Table 3 , the most commonly used fluid is
the carbon dioxide due to it benign chemical and physical characteristics which are: the
easi ly reachable critical temperature which saves energy, being nontoxic, inflammable,
and noncorrosive. In addition, from economic aspects it i s readi ly available with low co t
compared to other fluids. Supercri tical carbon dioxide is hydrophopic which al lows easy
disso lution of l ight hydrocarbons. The low polarity of SC-C02 increases its stabi l i ty
which i environmental ly acceptable.
7
Although the pecial characteri t ic of upercri tical fluid \ ere ftf t di co ered in
1 879 by Hannay and Hogarth, appl ication of supercritical fluid technology marked
crucial place on the re earch area 0 er the la t three decades. SCF ha e been u ed in
di fferent indu trie : eutracuet ical, Phannaceutical , Cosmetic , Polymers textiles and
c lothing, o i l remediation, and renewable energy (McHugh & Krukoni , 1 994) .
Re earcher have u ed SCF in d ifferent unit operat ion techniques including extraction
and impregnation, fractionation, chromatography, drying, coating dying, and a reaction
media. It is worth mentioning that SCF techniques are available in commercial scale with
more than 200 plants around the world . Most of the industrial technique are upercritical
fluid extraction ( SFE) , supercritical fluid fractionation ( SFF) supercritical fluid
chromatography ( SFC), and supercritical fluid reaction ( SFR) . These techniques are
briefly discus ed in the fol lowing paragraphs.
In analytical chemi try supercrit ical chromatography i prefered approach to
l iquid chromatography due to it shorter time consumption, safety since it acquires lower
organic olvents, and simple decompression is needed to obtain the products (Garcia
Risco et al . , 20 1 1 ) . Supercritical chromatography is employed for separation of mixtures,
detennination of binary d iffusion coefficients of solutes (Guiochon & Tarafder, 20 1 1 )
and detection of dyes in food samples ( Rezaei & Temel l i , 2000).
8
Table '" 10 t Common upercritical fluid
ompound Tc (0C) Pc ( bar) pplication
Itrogen - 1 47 33.9 Polymer proce ing due to its mert propertIes , Gass assIsted injection moulding process
I Ethylene 282.4 48.2 Polymer proces ing
arbon coffee and tea decaffeination, extraction of
dIoxide 3 1 .5 73.9 e ential 011 : spice , fragnces, dyes,
pharmacuetical compounds, and polymerization A a soh ent and oxidant for organic functional
'Itrous group since the byproduct i N� which is 36.4 72.5 en ironmenta l ly acceptab le, Extraction of: oxide
Amine , pharmacuetical compounds from animal feed, and l ipids from human plasma. Production of: isoparaffins byFischer-Tropsch
Butane 9 1 . 46.2 synthesis from synthe is gas, and emul ifiers by enzynle-catalyze glyceriysis reaction Deasphaltation of petroleum, regeneration of
Propane 96.6 42.5 acti ated carbon fiber in l iquid petroleum gas processes ( LPG), and Manufacture of metaJlocene catalysts in polyolefin production Synthe is of carbon nanotubes, heterogenous
Ammonia 1 32 .5 1 1 2.8 catalytic processes, ammonothermal growth of GaN in the manufucture i f I ight emitting devices ( LEDs) Biodiesel production : to ketali e the byproduct
Acetone 235 46.9 glycerol into slketal , Chemical recycl ing of polynlers, thermal dehydration of fructose, and themlal degradation of cellulose
Chemical recycling of polymers, Biodiesel ;-"'lethanol 239.4 I production, and synthesis of metal and metal
oxide nanoparticles, and nanonuids
Ethanol 243 63.8 Biodiesel production, and polymer processing
Tetrahydrof 267 5 1 . 8 Chemical recycl ing of polymers
uran (THF) Chemcial recycling of polymer , extraction of
Toluene 3 1 8.6 4 1 petroleum pitch, oi l shale processes, and l iquefaction of coal
Supercritical water oxidation in waste treatment processes, hydrothemlal synthsis of
Water 374 22 1 multicomponents oxide in particle formation, gasification and refomling of biomass, and reaction media fo polymerization and conversion processes
9
Reference
(Okubo. 2005: Zhang et al.. 20 I I )
(Yeo & KJran, 2005)
( B.Gupta & hill, 2007)
(Ashraf-Kborassam et al .. 1 990: Poh et aI., 1 999)
(Ceni et a l . . 20 1 0: Valeno et a l . . 2009: Yoneyama et a I . , 2009)
(Chihara et at. . 20 1 2 ; J. Wang et a l . . 2004)
(Fischer et aI . , J 999: Hashimoto et a I ., 2005: Shao et al., 2009: Vyalov et aI . , 20 1 1 : S . Wang et a l . . J 999)
( Hwang et a I ., 1 999; Royon et aI . , 20 1 1 )
(Okubo, 2005: Quesada-Medina & Olivares-Carri l lo, 20 1 1 ; Sawangkeaw et aI . , 2009: Tan et a I . , 20 1 0; C. Wang et a I . , 20 1 l : Zhou et a l .,20 1 0)
(Gonen et aI., 20 I I : Gui et a I . , 2009)
( Lee & Hong, 1 998)
( Abourriche et a I . , 2009: Joung et a I . , 1 999: Pan et al , 2006: Sangon et a l . . 2006: Zhuang & Thies. 1 999) (Brurmer, 2009; Kipcak et a I . , 20 1 1 : Kruse & Dinjus. 2007: Lachance et aI., 1 999: Letel l ier et a I . , 20 1 0: Leusbrock et al.. 20 I 0; Marias et a l . . 20 I I ; Ot u & Oshima. 2005: Savage, 2009: an Bennekom et aI., 20 1 1 : Vogel et aI., 2005: Yoshida et a l . . 2004: Zheng et a I ., 2008)
upercntIcal fluid al act a good react ion media due to their beneficial phy Ical
characten t iC , \\. hlch \\.ere dl cu ed earl ier. The rea on behmd carrying out reaction
under upercntical condi t ion i the p ib i l t ty of contro l l ing reaction condit ion la
temperature and pre ure. In mult i- tep reaction the upercri tical media can be the
choice 1 11 the a e of di ffu i n l imited reaction due to the high di ffu ion coefficient of
F . upercri tical media can al 0 hift the reaction balance tOy ard the product
\\. hen the later one i prefered t di 01 e in certain pha e, thu the electi ity can be
enhanced. 1any re earcher ha e in e l igated the u e of upercritical media in chemical
reactIOn uch a ; eth Ibenzene di propol1 ionation ( otelo et a I . , 20 1 0), synthesi of
\ Itamin E ( . " ang et a I . , 2000) , de u l furization and demetal l izaiotn of ga oi l (Vogelaar
et aI. , 1 999) .
2.3 E x t ract ion Technologie
Extraction i u ed to reco er compound from raw material . The raw material
can be o l id uch a herb and meat , or l iquid uch as crude oil and gel . The
phenomenon behind extra tion i the olubi l ity of the de ired compound can di olve in
another ub tance or pha e according to their molecular propert ie uch a polarity. Many
indu trie are u ing e traction among which are; pharmaceutical, food, co metics,
em Ironmental & petroleum indu tries. The mo t common extraction technique i Soxhlet
extract IOn and team d i t i l lation or hydro-di t i l lation. The new extract ion technology
\vhich ha taken a great attention recent ly i the upercrit ical fluid extraction. The e
extraction technique are d i cu ed below with extended deta i l for SCF extraction.
1 0
2.3. 1 oxh let E t raction
oxhlet extraction al 0 knO\ n a olvent extraction wa fir t introduced by on
oxhlet in 1 79 a a ol id-l iquid extraction technique. It ha been u ed for more than a
century and con idered a the main reference to e aluate the performance of other
ex traction method . In oxhlet extract ion an organic 01 ent is u ed to dissol e a de ired
compound [rom solid raw materia l . Th cri teria for electing appropriate solvent are: higb
oh ent power, electi i ty, and chemical stabi l ity, being recyclable, inexpen ive, nontoxic
and noncorro i e, low i cosi ty, avoid emulsion, and al low fonnation of im111 i cible
l iquid pha e ( Luque de Ca tro & Priego-Capote, 20 1 0) .
I n oxhlet e tractor the olvent i placed in a reservotr and heated up to
e\ aporat ion and i pa ed through a dist i l lation tube. The solvent vapor is condensed
indirect ly by cold water and dripped into the chamber holding the solid sample. During
dripping, the extraction takes place and once the sample chamber is fil led with the wann
o l \'ent, the later one return back to its starting reservoir via siphon am1 holding the
de ired extract. A further eparation is acquired to obtain the extract. F igure 3 shows the
chematic d iagram for Soxhlet extractor.
1 1
ndenser
Siphon arm 1 '1,. ........ -+ Extraction Chamber
I Igure : '- 0 hlel Extractor
ing this extraction approach one can en ure the cont inuous contact between
ample and fre h olvent which improve the driving force and hence the mass transfer.
Al 0 the equipment is economical compared to microwave-assi sted extraction and
uperclit ical extraction. Moreover, the selectivity can be enhanced by altering the solvent
polari ty. The drawback of thi techn ique include; time consumption, large amount of
o lvent which increa e the co t and environmental impact, and thermal degradation of
ome compounds which may happen s ince the process is performed at a temperature
cIo e to the boi l ing point of the solvent ( Luque de Ca tro & Garcia· Ayuso, 1998).
2.3.2 H� d rodist iUat ion
One of the o ldest extraction methods i hydrodist i l l ation which uses water as
solvent for the extract ion of water soluble compounds. Adequate amount of water is
poured into the vessel containg the sol id sample. Heat i suppl ied to boi l water and steam
is a l lowed to penetrate into the sample to release the desired compounds from its raw
materia l . The l eaving steam containing the extract ( dist i l late) is condensed by indirect
1 2
co l ing and flow into a eparator v here extract i automatical ly i olated from di t i l l ate
'v\ ater.
The main advantage of thi teclmique is it feasibi l ity and low 01 ent co t .
Bearing in mind that i t uffer [rom eriou di ad antage including; low extraction
efficiency since team cannot penetrate into the inner pore , t ime consumption and
degradation of olat i le component hich are thermally ensitive material ( Damjanovic
et aI. , 2005; Khajeb et al. 2005 ) . In addition to these drawbacks, the long contact t ime of
plant material can cau e the hydroly i s of essent ial oil compounds such as e ters into
acid and alcohol ( Handa et at., 2008 ) .
2.3.3 Micro" a\f- Assisted E. t raction (MA E)
Microwave- A isted extraction i s a new technique appl ied firstly in 1 986 by
Salgo et al for extraction of organic compounds. MAE is being commercia l ized with two
type ; c lo ed extraction essels and focused microwave ovens ( MandaI et aI. , 2007) .
1AE i main ly based on convert ing the e lectromagnetic energy in microwaves into heat
energy at frequency of 2450 M Hz. It aves energy since heating occurs in c losed sy terns,
and ave t ime compared to other conventional extraction techniques (Armstrong, 1 999;
Duvemag et aI. , 2005; Franke et aI., 1 996; Ganzer et aI. , 1 986) . The extract ion takes
place when moisture in ide the sample cel ls is heated up and evaporate pushing the cel ls
wal ls from ins ide. As a result of the pressure, the wal l s stretch and rupture relea ing the
act ive compounds into the surrounding solvent (MandaI et aI. , 2007) .
The process i s l imited by the solvent nature s ince only polar solvents can absorb
microwave heating. Therefore, MAE is not a favorable technique for recovery of non
1 3
polar compound . Moreo er ha l ower electi ity than FE, hence fractionation
cannot be avoided to enrich or purify the e tract . fter e traction cooling and
depre urizing of the e el are required which on ume energy and time ( un & Lee,
2003 ; Taathke & Y Jai wal, 20 1 1 ) . Another drawback i the en ironmental impact due
to 01 ent u age . Another di ad antage mentioned i the ign ificant thermal degradation
of analyt e tmcted by M E ( han et aI., 20 1 1 ) .
2.3.4 S u pcrcrit ical Flu id E xt raction (SFE)
FE i imply can-ied out by passing a SCF ( usual ly CO2) through ample
material uch a dried plant . Due to the tran p0l1 propert ies the compound of interest
tran fer into SCF pha e. The proces is restricted by temperature, pressure, fluid flow
rate, t ime, and sample ize. The SFE process i chematica l ly hown in Figure 4. CO2
flow from the cyl inder into a pump and a heater where temperature and pressure are
adju ted to reach the supercritical tate. The SC-C02 passes through the extraction vessel
\ hich i charged by the sample material . The de ired compounds dis olve in the
upercri tical fluid as a re ult of contact between the two phases. The SC solution ( SC
CO2 containing the extract) lea es the extraction vessel . Final ly, the extract is col lected
by vent ing SC-C02 at ambient condit ion into a vial . I t should be noted that CO2 can be
recycl ed and the proce s can be performed continuously to reduce the cost and faci l itate
the operation work .
14
Syringe Pu mp
- - - - - -
I Oven
Extraction " es el
- - - - - - -
Figure 4 chmati c d iagram of FE apparatus
I - ,
The perfonnance of SCF proces can be assessed by three parameters which are; product
yield, product quali ty, and efficiency. Y ield is defined as the amount of extract obtained
b SFE over the amount of ample charged in the extraction ves e l .
0'0 Yie ld = W e tract x l 00 \V,ample ( 1 )
On the other hand the product qual ity is described by analytical techniques such as gas
chromatography ( GC) and high perfomlance l iquid chromatography ( H PLC) . The
product has high qual i ty when h igh removal of impuri ties or high abundance of desired
compounds was obtained from extraction process. Extraction efficiency is defined as the
amount of extract obtained by SFE over the amount of extract in i tial ly present in the
charged sample . The amount of extract ini t ia l ly present in a sample is found by a
reference conventional extraction technique such as Soxhlet extraction . .
15
ff· . Wextract 1 00 % E lC le ncy = X Wextr.1CI an charged sample ( 2)
upercri t ical fluid e tra t ion ha numerou advantage that can be u eful for everal
appl ication in d i fferent fi eld ; food, co metic pharmaceuticals c lothing, and etc. The
proce environmental l y acceptable and con idered a green technology since no tox ic
o lvent i u ed thu reducing harmful re idue . Moreover the 01 ating power of
supercri tical fluid is ea ily control led by temperature and pre sure. Another advantage i
that i olation of CF from the extract i feasible since SCFs are separable at room
temperature and thu reduce the separation expen es. In addition, due to the high
01\ ating power of upercrit ical fluids, extract ion of high boi l ing point compounds is
achie\ able at lower temperatures. Thermal degradation of sensit ive valuable compounds
can be avoided in supercritical fluid extraction.
The main reported drawback of supercrit ical fluid extraction is the high capital
co t of the equ ipment which can be covered by the reco ery of valuable and commercial
compound with h igher yield and quality. A d isadvantage of SC-C02 is that it is a good
olvent only for non polar compounds; however addition of modifiers such as ethanol
could increase the solubi l ity of polar compounds.
2.3 .4. 1 E xt raction para meters
The extraction process trongly depends on several factors inc luding; temperature,
pres ure, t ime, solvent flow rate, and part ic le size. E ffects of these factors are discussed
bel low.
1 6
Th effect of pre ure on the e traction proce related to sol ent den ity and
01 ent power. It i wel l known that when the pre ure i increased, the 01 ent den i ty
mcrea e ele at ing the 01 ent power, thu reducing amount of 01 ent needed. I n other
word increa jng the extract ion pres ure wi l l re ult in more molecule being forced into
the o lution, therefore more solutes wi l l di olve in the supercritical fluid. This behavior
i favorable when higher e traction yield is desired. It should be brought to attention that
an increase in extraction pre ure wi l l reduce the extraction selectivity since higher
o lub i l i ty mean dis olving more compound . Consequent ly the extraction pressure can
b u ed to tune the select ivity since den ity is sensit ive in supercri t ical region.
Temperature E ffect
The extraction yie ld is trongly influenced by extraction temperature. It is obvious
that change in extraction temperature is associated by change in supercritical fluid density
and o lute volat i l i ty \ hich affect the solute solubi l ity in opposite way . Such behavior of
the extraction temperature i s commonly known as the crossover phenomena where both
parameters ( den ity and volat i l i ty) are competing factors are dominant . By increasing the
extraction temperature the volat i l i ty of the extract increases, which increases the
solubi l i ty, hence extraction yield goes up. The extraction yield goes down with increasing
temperature when den ity of supercri t ical fluid decreases cau ing reduction in the
solub i lity.
Effect of sol ent flow rate and extraction t ime
1 7
The o lvent flo\ rate i in er ely proport ional to e traction time. lncrea ing the
oh ent flow rate wi l l make the e traction proce fa ter. At higher solvent flo rate , the
contact t ime between olvent and ample wi l l be lower, and the sol ent may not have
enough time to penetrate into ample pores effect ively. As a re ult lower amount of
di oh ed compound wi l l exi t in the upercritical fluid, tbu reducing extraction yield.
lze
ample preparation i needed before performing the extraction
proces . One of the preparation teps is grinding the sample into smal ler size. I t is well
known that when the ample part ic le ize is decreased, the surface area i ncrease and the
contact between the olvent and ample material wi l l be more. As a result of increa ing
the contact between the ample and olvent more extract wi l l be released from the
ample ce l l and hence extract ion yield is enhanced.
everal investigator reported that in some cases decreasing the sample particle
size can lead to lower yie ld . The reason behind this behavior is that the smal l particles are
packed together forming bed caking al lowing the solvent to flow through channels along
the extraction bed ( Bernardo-Gi l et a 1 . 2007; J ia et a I . , 2009b; Langa Cacho et a I . , 2009;
Langa, Porta et aI. , 2009; Liu et a I . , 20 1 0 ) .
2.3. 4. 2 ,\/athematical .\/odelillg
The potent ia l interest i n supercritical fluid extraction is the need for mathematical
and theoretical description of the extract ion process. A mathematical model of a process
helps in predict ing the proce s design parameters such as solvent flow rate particle size,
1 8
and equipment dimen ion
mathematical prediction
oreo er, due to high capi tal in e tment of FE a
needed to a se the proce cale-up fea ibi l ity. The
mathematical model of the proce reflect the ph sical trend of the experimental data .
The extTaction proce mainly de cribed by an e traction curve; a plot of
extract weight ver u CO2 \ oJume. imulation of extraction curve can be accompli bed
b under tanding the e traction mechanism and olute behavior in the SCF pha e.
Briefly, in the extraction proce the tran port of olute occurs in three phases namely;
olid pha e, part ic le pha e, and fluid phase. First, the solute moves from the solid particle
the pore , then, d iffuses in ide the pore wi l l take place, and the fmal step i the a ial
di ffu ion along the bed. The extraction process is affected by the solubi l ity and diffusion
of the olute in upercri t ical fluid pha e.
1.3. .1. 2. 1 Solubility o/solute in Slipercritical fluid phase
Solubi l ity data of the intere ted compounds are needed to model the supercritical
fluid proces e . !nve t igator have u ed many approaches to ob erve the behavior of a
o lute in the upercrit ical fluid region. Those approaches can be divided into two main
categories; mathematical and experimental depending on the nature of the existing
compounds . The mathematical approach uses two main tools; empirical correlations and
them10dynamic models .
• Thermodvnamic solubilitv
The thermodynamics models for sol ub i l ity or phase equi l ibrium data are based on
equations of state along with various mixing rules. Typical ly, a system reaches
equi l ibrium state when it meets one of the three conditions; minimum Gibbs free energy,
19
ame hemical potential of ea h pecie in all pha e , and the equali ty of the fugacity of
pure olute to it fugac ity in upercrit ical fluid pha e. The equi l ibrium data can be
de crib d by the fugacity coefficient which i obtained by equations of tate . The
calculation tart with common a umption including; the olubi l i ty of tbe fluid in olute
pha e i negl igible and the molar olume of solute pha e i con tant . At equi l ibrium the
fugaci ty of the solute in the ol id phase is equal to the fugacity of the olute in the
upercri tical pha e ( Eq. 3 ). The fugacity of pure species at olute phase and supercri tical
pha e are calculated using equat ion 4 and 5 re pe ti vely.
Ii sol id = t;SUperCTitical
Fsupercritical _ p 1 i - Yi <Pi
( 3 )
(4 )
(5) Where f i the fugacity and i refer to component i in the mixture P is the pre sure, T is
the temperature, v i s o lute molar volume, R i s the universal gas constant, Nat is the
aturation pre ure found ei ther in l iterature or calculated using Antoine equation ( Eq .
(6 ) ) , <pfat i fugacity coefficient for species i at saturation and can be taken as unity, and
<Pi i the fugacity coefficient of species i in supercritical fluid phase which is calculated
by equations of state such as; Peng-Robhinson, Van del' waals, and Redl ich-Kwong
equation of state.
B log psat = A - -- Eq. (6 ) TCK) -C
where A, B, and C are Antoine constants for pure species, T is the operating temperature
20
e eral inve t igator u ed equat ion of tate for olubi l ity calculation. Recently,
Yazdladeh et aI . , 20 1 1 modeled the olubi l it ie of 52 mo t ly u ed olid compound in
up rcnt ical carbon dioxide. In their model, they appli ed the Peng-Robin on and
mael izadeh-Ro hanfekr equation of tate along with everal mix ing rule including
Wong- andler and an der aal . Their re ult howed good agreement with
e perimental data found in l iterature (Yazdizadeh et a I . , 20 1 1 ) . Gracia et. ai, 2009 tudied
the pha e behavior of egetable o i l in supercritical carbon dioxide. In their approach,
they con idered that any egetable o i l consist of two key components; oleic acid and
triolein. The cubic equat ions of tate Soave-Redl ich-Kwong and Peng-Robinson-Bo ton
Mathia were u ed along with mi ing rules with modifications. The equat ions were
included in A pen-P lus software package and the re ul ts fitted the experimental data
fairl wel l (Gracia et a I . , 2009). Another group, Esmael izadeh et a1 . ( 2009) developed a
new mi ing rule to simulate the solubi l ities of aromatic hydrocarbons, al iphatic
carboxylic acid , aromat ic acids, aromatic and a l iphatic alcohols in supercrit ical carbon
dioxide . Their new e cess G ibbs free energy ( Gex) mi ing rule was employed along with
PR and SRK and compared with five mix ing ru les namely' Wong-Sandler, Orbey-
andler, Van der waals with one adj ustable parameter, Van der Waals with two
adju table parameters, and covolume dependent rules. Their model gave satisfactory
re u l t wi th minimum de iation from experimental results compared with other
models(E maeilzadeh et a I . , 2009 ). Madras (2004) proposed a thermodynamic model for
the o lub i l ity of fatty acids in supercritical carbon dioxide . He used Redich-Kwong
equation of state coupled wi th Kwak-Mansoori mix ing rules with one adju table
parameter. Furthermore, he correlated the interaction parameter to the chain length of the
2 1
fatt acid by l inear re lation hip and concluded that the model can be u ed to predict the
o lubi l ity f variou [att acid . Hi re ult matched experimental data publi hed in
l iterature (Madra , 2004). In addition, Correa et a1 . ( 20 I 0) reported new olubil ity data
for qualene in upercrit ical carbon dio ide. They u ed combinat ion of Peng-Robinson
equat ion of tate and Van der Waal mixing rule and their result agreed with
experimental olubi l ity data ( Martinez-Correa et a l . , 20 1 0 ) .
• Empirical olubilit\.'
Variou tudie ha e been conducted on relating the solubi l ity of materials in
up rcri t ical fluid by empirical correlations. In 1 982 Chrast i l could relate the solubi l ity
of \ 'arious omponents direct ly to the density of supercritical carbon dioxide by the
equation:
( 7 )
where y i the olubi l i ty of olute expre ed in giL, p i den ity of the supercritical fluid
in g/L,T i the temperature in K, k i s association number, and the constants a and b are
rel ated to aporization and olvating heat and molecular weights of solute and
supercritical fluid . The model is based upon the fact that one molecule of solute A
as ociates w ith k molecules of solvent B and combine to give the complex ABk. The
Chra t i l equation fi tted the experimental solubil ities of the interested compounds fairly
wel l 0 er temperature range from 40 to 80 °C and pressure range from 80 up to 250 atm
(Chra t i l . 1 982) . Further modification was employed to Chrast i l equation by Del Val le
and Aguilera ( 1 988) to be more general and val id for wider range of temperatures and
pressures. Thei r equation can be appl ied for calculating the solubil ity of vegetable oi ls in
22
upercri t ical arbon dio ide for temperature from 20 to 0 0 , pre ure from 1 50 atm to
8 0 atm, and olubi l i t ie I er than 1 00 giL . The Del a I le and Agui lera equation i
e prc cd:
I n y = 1 0. 724 In p exp (40 .36 _ 1 8708 + 2186840) T T2 ( )
Gong and Cao ( 2009) u ed hra til and Mendez- antiago-Teja empirical model to
corr lat experimental solubi l ity data of art imi inin in supercritical carbon dioxide. The
Mendez- ant iago-Teja model i ba ed on the theory of d i lute solut ions ( Santiago & Teja,
\ 999) . The compared the empirical model with the experimental mea urements and
obtained an average de iation of 8% for both model . The model is expres ed by the
fol loV'. ing equat ion, where the con tants A B and C are adjustable parameters ( Gong &
Cao, 2009) .
Tln(yP) = A + Bp + CT ( 9 )
Another empirical model i the one proposed by Adachi-Lu involving five adj ustable
parameters. Savo a et a 1 . ( 200 1 ) used Adachi-Lu model to quant ify the solubi l ity of
grape and b lackcurrent oils in upercrit ical carbon dioxide in addition to Chrastil Del
Val le and Agui lera models . The Adach-Lu model fitted the experimental data fairly wel l
but the other model showed better agreement . The Adachi-Lu model with Savova s
adj ustable parameters i s expre sed by Eq. ( 1 0)
00002 2 -5000 Y = p 1.4+0.0048p-0.0 P exp ( ) T-10. 1 4
23
( 1 0)
• Experimental ollibilil}'
olub ! l i ty of pure component can be mea ured e perimenta i ly a de cribed in l i terature
( nite cu & Ta laride , 1 997; hen et a i . , 20 1 1 ; Chra t i l , 1 982; Del al 1e & Agui lera,
1 98 : 0 ova et a 1 . , 200 I ) . I l ov,'ever the e y tems are l imited for olubil ity of pure
compound not mi ture . In addition solubi l i ty measurement are time con uming since
they are canied out at low Dow rate . A typical e perimental approach to detennine the
olubi l i t i [rom the experimental extraction curve . The solubi l ity i simply equal to the
init ial lope of the l inear part of the extraction curve. Thi approach is preferable
e pecia l ly if the e tract con i t of d ifferent unknown compound
The mathemat ical olubi l i ty model are l imi ted to common compounds and pure species .
The thennodynamic model can be complicated when the extract is a mixture of several
pecie . When the extract contain many compounds, there wi l l be a need for the physical
prope11ie which are not widely available. Moreover, physical properties are not always
mea urabl e or computable . Correlations and fonnulas for physical properties can be val id
only within a certain range. For example, the saturation pre sure which i calculated by
Antoine equation i s l imited for temperature and pres ure ranges, and also the Antoine
con tants are not avai lab le for a l l compounds. Besides the lack of physical properties the
behavior of a component is d ifferent when it is in a mixture. For example, d iffusivity and
beat capacity parameters for pure components vary when they are in a mixture due to the
effect of other component d iffusivity and heat capacity based on their compositions.
U ual ly the empirical models are not widely accepted in the scient ific community
because they are l imi ted by process conditions, e .g. temperature and pressure ranges.
24
M re \ er, the adju table parameter cannot be general ized for a l l kind of e tract .
Furthermore, the adj u table parameter are appl icable to common extract and fitted
without phy ical ign ificance. In other word , the adju table parameter do not reflect the
ph ical behavior of the compound and do not e plain the theory behind the extraction
curve to faci l itate pro e s scal ing-up.
A a re ult of the l imited mathematical tool for getting the solubi l i ty the appropriate
approach i the init ial lope of the extraction curve which ensures sufflcient accuracy of
olubi l i t value and demon trate the phy ical behavior of solutes in superclitical
extraction proce
1.3 . .:1.1.1 lIodelillg the extractioll curve
N umerous studies simulated the extraction curve of the supercritical extraction
proce . The a ai lable models in the l i terature vary depending on d ifferent scient ific
\ iew and d i fferent postu lation . Recently, Grosso et a l . ( 20 1 0) publi hed a study dealing
wi th d ifferent mathematical model for upercritical CO2 extraction of volat i le oils from
aromatic plant . I n general the models are found in four main categories' empirical
models, shrinking core models, models based on heat transfer analogies, and models
ba ed on d ifferent ia l rna s balances ( Gro so et a ! . , 20 1 0) .
General as umptions common to almost a l l models types include; 1 ) isobaric and
i othermal process, 2) constant physical properties a long the process; porosity and initial
o i l content, 3 ) uniform superficia l velocity and solvent flow rate, 4) extract content is
di tributed uniformly between particles, all sol id part ic les have the same uniforrll shape
and 5 ) l inear relationship between sol id and fluid phase.
25
reover, the adju table parameter cannot be general ized for al l kind of e tract .
Furthermore the adju table parameter are appl icable to common extract and fi tted
without phy ical igni ficance. In other word , the adj u table parameters do not reflect the
ph ical beha ior of the compound and do not e plain the theory behind the extraction
cun e to faci l itate proce a l ing-up.
A a re'ult of the l imited mathematical tool for gett ing the solubi l i ty, the appropriate
approach i the init ial lope of the extraction curve which ensures sufficient accuracy of
olubi l ity alue and demon trate the pby ical behavior of olutes in supercritical
extract ion proce
2. 3. ,/. 1. 2 llodelillg the extractioll curve
umerous studie simulated the extraction curve of the supercritical extraction
proce . The available models in the l iterature ary depending on d ifferent scient ific
\ iev\> and d i fferent po tulations. Recently Gros 0 et al. (20 1 0) publ ished a study deal ing
\ i th di fferent mathematical models for supercri t ical C02 extraction of volat i le o i l from
aromatic p lants. In general the models are found in four main categories· empirical
models, shrinking core models, models based on heat transfer analogies, and models
based on d ifferential mass balances (Grosso et a l . , 20 1 0) .
General a umptions common to almost a l l models types include; 1 ) isobaric and
isothem1a l process, 2) constant physical properties along tbe process; porosity and init ia l
o i l content, 3) uni fonn superficial velocity and solvent flow rate, 4 ) extract content is
d istributed unifonnly between particles, a l l sol id partic les have the same unifonn shape,
and 5 ) l inear relationship between sol id and fluid phase.
25
• EII/prrica/ models
n empirical m del \ a prop ed by aik et al . in 1 9 9 to de cribe the extraction
f perfume and nav r fr m plant material . The i l l u trated the ariation of the
e"\tra tl n ie ld \ er u t ime b imple mathematical Eq. ( \ 1 ) . Thi model de cribe the
e"\tractl n le ld \ r u e"\tra ti n t ime by a Langmuir ga ad orption i otherm . Langmuir
a LImed mon layer coverage of the olid matri including the olutes, which force a
con traint to the ma"\imal amount of olute in the ub trat depending on its peciftc
·urface. De pite the good agre ment with e peri mental data, thi model doe n't con ider
both the IIlteraction bet\ een olute and ol id matri and the fractionation of o i l during
the pro e . e\ eral r earch r employed thi empi rical model and optimized the
adJu table parameter; they found that parameter b vane with ma s flow rate, pre ure,
and temperature ( E qUI el et a I . , 1 999; Papamichail et a I . , 2000) .
Y = Yoo t
b + t ( 1 1 )
where Y i extraction yield defined a the ratio of the ma s of o i l extracted in kg at time t
( ) to the in it ial ma s feed Yoo i Y after infinite extraction time, , and b i adju table
model parameter.
Lmearization of Eq. ( 1 1 ) l ead to l i near relation hip between the inverse of the yield and
i l1\ er e of the extraction time with a lope equal Yoo and intercept equal to �. In b Yoo
addition, Y 00 can be a umed to be the maximum yield obtained experimental ly, thLl the
number of adju table parameter w i l l reduce. Furthermore, Huang et a l . (20 1 1 ) defined
Y the recovery T as - and obtained the relation hown in Eq. ( 1 2 ) . They determined Yoo
26
parameter b from the ' I pe f the curve reciprocal reco\ ery ver U reclpr cal of the
extract IOn tim
t r =
b + t ( 1 2 )
( I I uang et a I . , �O l l ) de cribed the extraction rate a a fir t order chemical reaction
\\ a. lq. ( 1 3 ) . cording t the m del , the e tract avai lable i n the ol id matrix i
decrea mg \'. ith time exponent ia l ly b rate con tant k and expre ed mathematical ly by
Eq. ( 1 4 ) \\ ith initial con entrat ion Cso . The e traction rate constant ( k ) i related to
di ffu 1 \ I t _ and part ic le dimen ion by q. ( 1 5 ) . In thi model Yo and k can be obtained by
fitting the m del to experimental data ( a ik et a I . , 1 9 9) .
des = -kC dt 5
\\' t th 0\ eral l extract ion yield given b
Y = Yo [ l - exp (-kt)]
\ here
k = DS Vd
And
5 6(1-Ep) v dp
27
( 1 3 )
( 1 4 )
( \ 5 )
( 1 6 )
( 1 7 )
\" here Cs I th extract on entratl n in the o l id matrix 10 g I , dp i part ic le diameter in
m. d i the bed diameter 10 m, D i ' lute d iffu ion oefficient, Ep i part icle poro ity,
and are part ic le urfa e area in m2
and olume in m-�, re pectivel .
Regardle f the implicit and the large capa it f the empirical model , which are the
onl ad\ antage . u h m del uffer from lack of theoretical or ph ical meaning . A a
re ul t emplri al model are not uitabl for cal ing up the upercritical e traction
( Bernardo-Gi l & a qui lho, 2007).
• Heal transfer analogi . models
The e model de crib the extraction phenomena a a heat tran fer phenomena by
con idering each o l id part ic le a a hot phere cool ing in a unifOIm cool medium. Thi
oolmg of hot phere i u ed to imulate the concentration profi le a a function of t ime.
Deri\ation of thi mod I i carried out by applying Fick ' econd law for d iffu ion along
\\ Ith heat-rna tran fer analogy u ing Fourier tran form . The model wa propo ed by
Crank and repre ented by Re erchon u ing the fol lo\ ing equat ion (Campo et a I . , 2005;
Crank. 1 97 5 : Doker et a I . , 2004; Erne to Reverchon, 1 997; Erne to Reverchon et a l .
1 993) :
q 6 <Xl 1 ( n2rr2 Dt) - = 2 Ln=1 2 exp - --2 -qo rr n r ( 1 )
where q i the o lute concentration \0 olid pha e ( Kg/m\ qo i the init ial olute
concentration m ol id pha e ( Kg/m\ n IS an integer, D
, . phere (m- ) , t 1 extraction time ( ) .
28
solute d iffusi ity \0 olid
a par et a ! . ( 2003 imulated the extraction curve u ing heat tran fer analogy
m del v" ith the a umption of the plate l ike part ic le , 0 cal led imple ingle plate model
P) . They l ight ly modi fied the model propo ed by Bartle et a!. ( 1 990) where the
e tractable il i con idered to minimize the de iation from experimental data. It i
worth mentioning that the propo ed model by Bartle et a 1 . for the extract ion of rosemary
il howed de iation from e perimental data as a re ul t of neglecting the
equ i l ibrium tage ( early e traction tage) where the majority of oi l wa extracted. The
model wa reVvTitten in tenns of e traction degree and expre sed by Eq. ( 1 9 ). (Gaspar et
a 1 . , 2003 ) . E qui el et a ! . ( 1 999) used the arne approach to describe the ex traction of
ol ive hu k o i l . They reported that the model gave sat isfactory agreement with
experimental data at h igh uperficial veloci t ies while at low superficial velocities the
fitting wa ery poor ( Erne to Reverchon et a I . , 1 993) .
( 1 9 )
where ECt) and Eoo are the extraction degree (%) after time t ( ) and i nfinite, Dm is solute
d i ffusi ity on the part ic le plate (m2/s), 8 i s the th ickness of the part ic les (p lates) (m) and
n i an integer.
• Shrinking core model
This model divides the porous sol id matrix into two zones; inner zone which is o i l
rich core, and outer zone. The extraction proceeds as a result of i rreversible desorption of
solute from the core to the part icle pores fol lowed by d iffusion wi th in the pores ( intra-
part icle d iffusion), and d iffusion through the bulk fluid phase . When the solute
29
concentrati n in the outer zone i much h igher than the olubi l ity in the fluid pha e; a
harp b undary ( hlinking boundary) exi t betv een the two zone . During the e tract ion
proces the core of the inner region hrinks with l ime. The model wa propo ed by Goto
at a ! . ( 1 996) for de cribing the e traction cur e of o i l from rape seed . The model
a ume no ad orption of olute into the ol id matrix and ha two fi tting parameter ;
effective di ffu i \ ity and ma tran fer coefficient. Goto et a 1 . ( 1 996) ex pre sed the
hrinking core model using dimen ionless material balance in the fluid phase and sol id
pha e by e t of equat ions shown below and 01 ed the d ifferential equations numerical ly
u ing rank- ichol on' method ( Goto et a 1 . 1 996; Ol iveira et a ! . , 20 1 1 ) .
aterial balance in the bulk flu id phase:
Material balance in the part ic le pha e:
with an extraction yield expressed as
y = abE I.e X de 1 - E 0 b
( 20)
(2 1 )
(22)
Xb , Xp , Q e, Z, ( are dimensionle s groups of concentration in bu lk phase, concentrat ion
in part ic le phase, solid phase concentration, time, axia l bed coordinates and part ic le
coordinate, respectivel y, defined as:
X - Cb b - -, Csat
X _ Cp P - , Csat
30
z = :. L '
r - '!:E '> c - R
\\ here Cb the olute concentration III the bulk pha e (molfm\ Cp i olute
concentrati n of the part ic le pha e (molfm\ Csat i saturated olute in fluid pha e
(mol m\ q i o lute concentTat ion III olid pha e (m01lm\ qo ini tial solute
concentration in olid pba e (mo m\ Bi i Biolt number, Pe is Peclet number, E i bed
poro it , Ep i the part ic le poro i ty, t i t ime ( ), De i the effect ive d iffusivity (m::!/ ) , r is
radial coordinate (m) , rc i s the core radiu (m), R i s the init ial radial coordinate, z i s the
a ial coordinate in the extTactor (m), L i the extractor length (m) , and V i the inter t i t ial
\elocity of the o lvent (m/s) . The model con tants a and b are defined as fol lows:
b = � Csat
Machmudah et a l . ( 2006), Salgin et al . ( 2006), and Doker et a l . ( 20 1 0) employed the
hrinking core model for the extract ion of nutmeg o i l , sunflower o i l and sesame seed oi l
re pecti e ly . In their work they fair ly val idated the model by fitt ing the effective
d iffu i ity ince the mass transfer coefficient can be estimated using correlations
pub l i hed in l i terature.
• Differential mass transfer models
These models have more reasonable explanations for the theory behind the
supercritical extraction process . They acquire more physical properties and coefficients
of the sol id and solvent matrices such as; part ic le and bed porosity, mass transfer
3 1
coefficient and di ffu i ity coeffi ient . They are ba ed on two main mechani m ; the
equi l ibrium which occur at the earl tage of the e traction curve and the rna tran fer
mechani m at later tage. The equil ibrium i the mechan i m where the solubi l i ty of the
olute in the upercri tical region i dominant. The econd tage of the extraction tage
ccur \\ hen the concentration gradient became more dominant and it i de cribed by
ma tran fer phenomena.
I t i c lear that the mas tran fer mechanism may be control led with two resistances;
external and internal ma tran fer re i lances. Many re earcher simulated the extraction
urve ba ed on mas tran fer balance . Different assumptions where employed in order to
impl if the model . Ba ed on the e arious assumptions; the mass transfer balance
model can b c la ified into three groups according to the hypothesized contro l l ing step
namely; the external mass transfer res istance model , the internal mass transfer resistance
model , and both mass tran fer resi tance control the extraction process. Such deviations
on the e a umptions can be attributed to the di fferent structures of the material being
extracted for example d ifferent plant parts ( e.g . flowers, eeds, leaves, roots etc . ) can
yield to di fferent mass tran fer phenomena.
Reverchon and Marrone ( 1 997) forn1Ulated a mathematical model for the supercri t ical
extraction of c love bud oil con idering that external resistance is the control l ing step.
They studied the influence of both resistance and found that only s l ight deviation was
observed, which suggested that the internal mass transfer resistance can be ignored. They
asserted that the internal resistance can be ignored s ince it is insensitive to solvent flow
rate; on the other hand the external resistance is sensible to solvent flow rate. Wu and
Hou ( 200 1 ), Permt et a1 . ( 1 997) , and Kim et a ! . ( 2007) fol lowed the same scheme for
3 2
modeling the e traction of uni1o� er eed oi l , egg yolk, canola o i l and caffeine,
re pect i \ el .
Later on, intemal mas tran fer re istance wa taken into account and con idered
a the control l ing tep in the upercri tical e traction proce . The rea on behind this
con ideration \\ a explained by Re erchon et al . ( 2000) when they investigated the
tructure of hip ro e eed u mg canning electron micro cope (SEM) . The structure
re\ ealed that only ol ute near to the opemng channels are readi ly avai lable for
e ' traction. Therefore, upercri t ical olvent faces resi tance due to the d iffu ion at the
channel a i t penetrate deeply within the i rmer channels .
Moreover, it wa stated that as the e traction t ime mcreases, more extract content i
obtained. I n other word , at the beginning of the proces , the olute located at the part ic le
surface are e tracted, while solutes located inside the part ic le are transferred later on
when ea i ly extractable solutes are depleted (Nei et aL, 2008 ; Park et aL, 2007; Reis
Va co et aL, 2000: Vaquero et aL , 2006) .
The third group proposed models that consider both resistances control the
supercrit ical extract ion proce s s imultaneously which wa described by Savo a in 1 994.
She art iculated the extraction cw-ve by assuming that solutes are stored in the part ic le
cel l and protected by the cel l wal ls . During mi l l ing, some of those wal ls are broken
(broken cel ls) and olute became easi l y accessible, however the solute present in the
intact cells are inaccessible . Two resistances exist and face the extraction' the first is an
extemal resistance in the fluid phase and contro ls the process up to a l l essentia l oil in the
broken cel l is recovered. The second resistance l ies in the intact ce l ls and controls the
3 3
remaining e traction part \ hich re i t the d iffu ion of the inacces ible o i l . Based on
the e po -tulatJOn , three d i fferential ma s balance are dri en addre ed; two for the
pal1icle pha e; one in the brok n cel ls and another one in the intact cel l , and the third
balance i ll1 the Ouid pha e . Th d ifferential equat ion were integrated numelical ly with
three adju table parameter ; ma tran fer coe fficient in the solid pha e, ma transfer
coeffic ient in the Ouid pha e and the fraction of o i l init ial ly e i t in the cel l . The model
\V a ad pted for the e traction of variou o i l s including; p lumula nelumbinis by J ia et al
( J ia et a l . 2009a) . apricot kernel by Ozka l et a l . (Ozkal et a l . 2005 ), and Spanish sage by
Langa et al ( Langa, Porta et a I . , 2009) . .
Later ome modification were employed to the broken and intact cel l . Reverchon and
Man-one extended thi model by a paral le l resi tance model where solutes are transferred
with d ifferent kinetic in both broken and intact cells ( E . Reverchon & Man-one, 200 1 ) .
The d i fference between eries and the para l le l model i that the solutes are extracted
d irect ly to the fluid phase in the latter one. Fiori et al . ( 2009) combined the shrinking core
model with the broken intact cel ls model . They can idered the o i l existence in the intact
and broken cel ls, and a the extract ion proce s progresses each cel l is irreversibly
depleted cau ing the olutes to move towards the intemal hel l which is described by the
hrinking core model .
3 4
3 E X P E R I ;\ I E N T A L E T U P A ' D l\ I E T H O DO LOG I ES
3 . 1 , ample p reparat ions
l lenna nower were picked from henna tree located at AI-J imi area in Al Ain c i ty,
E during blooming ea on in October. The flower were dried to reduce the moi ture
content u ing a freeze dryer (Eyela, FDU 1 200, Japan) at -4 DC for 1 2 hour . Dried
flower were tored in a fIidge unt i l further u e.
3.2 S upercr i t ica l flu id extraction
The experimental etup hown in Figure 5 wa used for the supercritical carbon
dioxide extraction of volat i le components from henna flowers. The apparatus consists of
a 260 ml yringe pump wi th contro l ler ystem ( ISCO 260D), and an ISCO series 2000
SCF Extraction sy tern ( SFX 220) including a dual chamber extraction module with two
1 0 ml tain le tee l extraction cel ls . Each 1 0 ml stainless teel cel l ha diameter of 1 .5
em and 5 cm length. In a typical experiment, about 2 g of dried henna flower was
weighed u ing an e lectronic balance ( Precisa, Swiss), mechanical ly grinded ( Moul inex,
France), and p laced in the extraction cel l . The part ic le diameter measured by microscope
(Nikon ecl ipe Ive l 00pol, Japan ) wa obtained to be on average 0 .504 mm. The part icle
and bed poro ity were calculated and their values were 0.79 and 0.5, respectively. After
placing the ample in the cel l and sett ing the extraction temperature and pressure, the
sample was al lowed to equi l ibrate for 1 5 min with SC-C02 . Supercri tical CO2 flowed
along the extraction cel l with flow rate o f 1 m llmin. The extract col lector was immersed
in cold methanol ( -40 DC ) provided by a ch i l ler ( ULTRA-KRYOMAT, Germany) to trap
the extract whi le the CO2 was vented to the atmosphere. The extract weight was recorded
for d i fferent C02 amounts pass ing through the sample unt i l no more extract was obtained
3 5
at \\-hich time the apparatu \ a lopped. The apparalu wa thoroughly cleaned after
each experiment by flu b ing methanol and 300 ml of CO2.
CO2 Cyl i n d er
Figure 5 uperclit ical Extraction Experimental Set up
3.3 Ga Chroma tography analysis
The extracts from flowers of henna obtained by SFE were subjected to Gas
chromatography (GC) compositional analysis. Gas chromatographic ( GC ) analysis was
perfonned with a CP 3800 Varian instrument equipped with flame ionization detector and
a column (CP-Select 624 CB, DF = 1 . 8, Id = 0.32 rom, l ength = 60 m). The condi tions
were a fol lows: carrier gas ( hel ium); Oven temperature program: Ini t ia l Temp : 40 °C for
1 min, Ramp 1 : heating up to 60 °C with heating rate 20 °C/min, Ramp 2 : heating up to
1 40 °C with heating rate 2 °C/min, Ramp 3 : Heating up to 250 °C with heating rate 5
3 6
° min and hold at 250 ° for 40 min, Injector temperature: 300 °C, Injection Mode:
p l i t le , In let pre ure : 20 p i, Detector Temperature: 2 0 °C .
3.... Ant ibacterial Acth it� Te t
The extract \ ere te ted for thei r ant ibacterial acti ity USIng di c d i ffu ion
method. Gram po it i e and Gram negati e bacteria (Staphylococclis aureus A TCC25923
and E cl1erichia coli 15922 ) ere pread a lawn culture on Muel ler-H inton Agar plates
(M T , Mer ey ide, K) . Fi l ter paper di c impregnated with 10 f.! L of each herbal
e tract \ ere placed onto the agar with ma imum 6 di cs per agar plate. P late were
incubated overnight at 3 5 °C and the inhibit ion zone around the di cs was measured .
3.5 An tio idant Act iYi t� te t
3.5. 1 FRA P ( Ferric red ucing ant ioxidant pmur) a sa�
Tota l antiox idant acti ity of henna flower extracts wa measured by reducing antioxidant
act i \ ity power as ay a described by Benzie and Strain 1 996. The principle of this assay
is the reduction of ferric into ferrous ion by the ant ioxidants.
FRAP reagent was prepared by mixing stock solutions in the ratio 1 0 : 1 : 1 at the
time of use. tack o lut ions included 300 mM acetate buffer (PH 3 .6) , 1 0 mM TPTZ
(2,4,6-tripyridyl-s-triazine) s01ution in 40 mM HCI , and 20 mM FeClL6H20 solution.
The mixed solution was incubated at 3 7 °C for 30 min in a water bath ( Memmert, D-
9 1 1 26, Schwabach, Germany) . 0 .5 ml from each extract was d i l uted in l .5 ml of ethano l .
A sample ( 1 50 Il l ) of extract a t each extraction temperature and pressure was mixed with
2850 III of F RAP solution and kept for 30 min in the dark at room temperature. The
absorbance of the ferrous tripyridyltriazine complex (coloured product) was measured at
3 7
wa\ elength 593 run . ampl blank at each concentration wa prepared by omitting
Fe h from the fRAP olution and di t i l led water wa u ed in tead. The standard curve
wa prepared u ing a corbic acid ranging [rom 0 to 1 00 ppm. The activity wa expre ed
a mg A cor'bic acid equival nt ( )/ 1 00 g of henna flower extracts.
3.5.2 D PPH radical ca, cnging acth i t�
1 .5 m1 of thi ample ( about 0 .5 ml of henna extract at each extraction condition
\ a added to 1 . 5 ml of ethano l ) wa mi ed with 1 .5 ml of O. l 5 mM 2 2-diphenyl- l -picryl
h draz 1 ( DP P H ) in 95% ethano l . The mj ture wa mi ed vigorou ly and a l lowed to
tand at room temperature in the dark for 30 min . The absorbance of the resul t ing
olution \\ a measured at 5 1 7 nm using a UV- 1 60 1 spectrophotometer ( Shimadzu,
Kyoto. J apan) . The ample blank at each concentration wa prepared in the ame manner
except that ethanol wa used instead of DPPH solution. A standard curve was prepared
u ing a corbic acid in the range of 0- 1 00 ppm. The act ivi ty wa calculated and expres ed
a mg A corbic Acid equ i alents (AA)/ 1 00 g henna flower extracts.
3 8
4 R E U LTS T D D I C U S I O �
I n thi tudy fir t henna flower oil was e tracted by upercritical carbon dioxide .
The extraction experiment were perfolmed under d ifferent temperature and pre ures
\\ h l le keeping the flO\ rate of C- 02 and cool ing temperature con tant. Effect of other
ex traction parameter including the cool ing temperature and the flow rate of S -C02
\\ ere al 0 tudied. Appendi A includes the raw data for the experiment . The extract
\\ ere analyzed by GC for their composition and their antibacterial and antioxidant
act i \ itie \ ere measured.
4. 1 Supercri t ical carbon d io, ide extract ion of henna flo" er
The operat ing condition that were investigated, the maXimum yield, and
olubi l ity of extract in SC-C02 for each of condit ions are tabulated in Table 4 .The
maximum yield \ as calculated by d ividing the final extract weight over the charged
ample weight (2g) . The solubi l ity of extract in SC-C02 was calculated from the init ia l
lope of the extraction curve (rna s of extract versu mass of CO2 passed). The highe t
yield was (30 .88%) obtained at 45 DC and 1 20 bar, while the lowest yield ( 1 8 .29%) was
found at the lowest temperature ( 3 5 DC) and pressure (80 bar).
39
Table 4 1a lmum \ idds and olubt l i t\ of FF of I Ienna flo\\ er extract - ,
T P F Tcoohng P /..l v Maximwn Yield Solubil ity (0 ) ( bar) (ml mm) (0 ) (kg/mJ ) ( Pa. ) 1 0' (m�/ ) x 1 0 ( °'0) (go,tract g CO2)x 1 03
3 5
3 5
3 5
4 5
45
45
55
55
55
55
5 5
.+5
3:
5 5
8 0 1 -40 4 1 9.09 2 . 98 7 . 1 2 1 8 .29
1 00 1 -40 7 1 2 . 8 1 5 . 77 8 .09 20.53
1 20 1 -40 767.07 6 .55 8 . 54 2 1 .66
80 1 -40 24 1 .05 2. 1 0 8 . 73 2 3 . 3
1 00 1 -40 498.25 3 .60 7.23 28.88
1 20 1 -40 657.74 5 . l 3 7 . 79 30.88
80 1 -40 203 .64 2.02 9 . 9 1 2 3 . 1 3
1 00 1 -40 325 .07 2 . 5 3 7 . 79 2 7 . 79
1 20 1 -40 504.5 1 3 . 70 7 .33 25 .4
1 00 2 -40 325 .07 2 . 5 3 7 . 79 l 3 . 5 1
1 20 2 -40 504.5 1 3 . 70 7 .33 1 7. 94
1 00 1 -25 498 .25 3 . 60 7.23 1 4 .06
80 1 -25 4 1 9.09 2.98 7 . 1 2 4 .52
80 1 -25 203 .64 2.0 9 .9 1 1 3 .56
The cool ing temperature wa found to have a significant effect on both extract ion
yield and olubi l ity. As can be seen in Table 4, increasing the cool ing temperature from
-40 to -25 °C reduces the extraction yield which may be due to the loss of some of the
volati le compound . Figures 6 and 7 i l l ustrate the s ignificant effect of the cool ing
temperature on extraction yield.
40
0.54 1
0.657
0 .742
0.757
0 .9 l 3
I 0. 756
0.853
2.9
0.04
1 .2
0.6
0. 1
0 .5
0 7
0.6 45 0 , 1 00 bar = 0 5 .JM
� 04 u ro � 0.3 � .......... lill
0.2 ... ....... ..... • - 40 °C ....
0 1 .. -25 °C
0 0 200 400 600
CO2 (g)
Flgurc 6 f. ffect of cool ing tcmperature at 45 LC and 1 00 bar
0.5
0.45
0.4
0.35
:§ 0.3
�0.25 CJ
3 0.2
0. 1 5
0 . 1
0.05
55 °C, O bar .... ",. . .
.. � ....... ,
.... "�,A
"
.' / ,,�
.A
.. ...
•• ..
-
. -40C
-25C
800
35
30
25
20 ? "0
1 5 11 r
1 0
5
0
25
20
1 5 ______ o
"0 .�
10 r
5
o �--------------------------------------� a o 200 400
CO2 (g)
600
Figure 7 E ffect of cool ing temperature at 55 °C and 80 bar
800
The flow rate of SC-C02 affected the extraction yield significantly. As shown in figures 8
and 9, increasing the flow rate decrea ed the extraction yield drast ical ly . For example an
increase of the flow rate from 1 mlJmin to 2 mllmin dropped the extraction yield by 7 %
4 1
at 5 5 ° and 1 20 bar ( Table 4) . The rea on behind thi trend is the longer contact t ime
between th ample and - O2 at the lower Oow rate.
0 .6
5 5 0 , 1 00 bar 0 .5
0 .4
I 0.2 •
•• . � 0. 1 ••
I •• ••••• • •
o o 200
• ••
••
• ••
•
� . •
••
400
CO2 ( g)
Figure c HTect of flo\\ rate at 5 5 °C and 1 00 bar
42
•••••••
. 1 mUmin
2 mlImin
600 800
30
25
20 """' o o '---'
1 5 :g Q) >=
1 0
5
o
0.6
0.5
0.4 --� '--' .,..., g 0.3 .... .,..., ><! lI.l
0.2
0. 1
0
5 5 °C, 1 20 bar
0 50 ] 00
• • • • • •
•
1 50 200 CO2 (g)
Figure 9 E ffect of flo\', rate a t 5 5 °C and 1 20 bar
4. 1 . 1 E ffec t of temperat u re
250 300
30
2 5
2 0
� o e..... 15 �
. � >-
10
5
o
350
The effect of temperature on the extraction yield is shown in figures 1 0- 1 2 . The
e traction curves for a l l runs exhibited a simi lar trend, stm1ing with a l inear part for
which the rate of extraction was constant fol lowed by a continuous decrease in the rate of
extraction unti l reaching a frnal maximum yie ld value after which no more extracts
obtained. However the init ia l slope and the frnal ( maximum) yield value of extraction
yield were d ifferent for the d ifferent conditions studied in this work. This is expected as
the operating condit ion (temperature and pressure) affect fluid propert ies ( i . e . volat i l ity)
and transport propert ies ( i .e . d iffusion coefficient), aU of which affect the extraction
process.
In almost a l l cases, the temperature had a direct effect on the extraction process since the
yie ld increased with an increase in temperature. As temperature increases, density
43
lllcrea e inver ely affecting the olubi l i ty of olute and e traction yield. However,
temperature i direct ly related to olati l i ty of the olute, which direct ly affect the
o lub t l i ty of the olute and hence the extraction yield. Therefore temperature affect the
olubi l ity and extract ion yield in trend opposite way through two compet ing factor
(den it) and v olati l i ty) . Furthemlore, temperature inver ely affects the vi cosity ( as
temperature increa e , vi co ity decrea e leading to ea ier flow). Temperature i also
dIrectly and favorably re lated to d iffusion coefficient ( a temperature increases d iffusion
coefficient increa e leading to higher yield) .
s a r ul t of a l l the e factor , for most of the condition studied in this work the
temperature had a direct in fluence on the extraction yield, ugge ting that the effect of
\olati l i t , vi co i ty and transport coefficient was higher than the unfavorable effect of
den ity change with temperature.
0 6
0.5
04
� b1) 0.3 � u ell '-� >< 0.2 r.:.::
0. 1
0 1' 0 1 00
p= 80 bar
• ••• • • • ••
A •• ....
. •• •
•• •• •
• •• •• A.. • •••
A" ••• ... .,
200 300 400 CO., (g)
•••• •
500
••••••
• • ••••••
55 °C .45 °C e 35 °C
600 700
Figure 1 0 E ffect of temperature on the extraction yield at 80 bar
44
30
25
20
� � 15 ::2
.!!:! >--
10
5
0
800
0.7
0 6
0.5
bO 0.4 "--' ...... u ro .....
� 0.3 •
• 0.2 •
•
0 . 1 •
0 0 1 00 200
•
P= 1 00 bar
• • • • • •
• • • •
300 400 CO2 ( g)
• • • • • • • • • • • • • •
• • • • • • • • • • • •
55 °C
.45 °C
e 35 °C
00 600 700
figure 1 1 I:: ffeet of temperature on the extraction ) i eld at 1 00 bar
45
35
30
2 5
2 0 ,......, 0 � :2
1 5 II)
>-
10
5
0
800
0.7 35
P= 1 20 bar 0.6 � 30
... •
0.5 ". � . 25
• • • • .....
OA • • ••• 20 • • � bO •• 0
• 0 '-" •• '-" ..., ::g u .., •• • ro • 1 5 ;;: l-X 0.3
• •• • u.l • • •
••
0 2 • • •• • • ••
• .. -0. \ . ..
o . o 200
•
400 600
Figure 1 2 E ffect of temperature on the extraction yield at 1 20 bar
55 °C
.45 °C
e 35 °C
800
10
5
o
1 000
The o lub i l ity of henna flower extract in SC-C02 (extract weight/C02 weight)
wa calculated at each condit ion using the ini t ia l slope of experimental extraction curves.
A hown in Figure 1 3 . solubil ity of the extract increased with both temperature and
pre ure, \vhich matche the trend of the extraction yield . Pressure directly affects the
solubi l ity of solutes on SC-C02. As the pressure increa es, the fluid density increases,
enhancing the solvent power of CO2 which leads to higher solubi l i ty on solutes as shown
in Figure 1 3 . Therefore, as a re ult of h igher solubil ity, the extraction yield increases as
the pressure is i ncreased ( Figures 1 0- 1 2 ) .
46
Temperature affect the olubi l ity by h\ 0 competing factor ( den ity and
\ olati l i ty) . the temperature increa e the den it of CO::! decrea e , reducing it
olvent power, which lead to lower olubi l ity of the olute in CO2. On the other hand, a
the temperature increa e , the olat i l ity of olute increa e , leading to high olubi l i ty of
the olute in O2. For a l l the condition tudied in thi work, the volati l ity effect wa
dominant cau ing the olubi l i ty to increase with temperature a hown in Figure 1 3 . The
increa e in olubi l i t of henna flower extract in SC-C02 with temperature resulted in an
in rea e in the extraction yield " i lh temperature ( Figure ] 0- 1 2 ) . These result show that
e ' traction proce i direct! re lated to the solub i l ity of extract in SC -C02 . The highest
o lub i l it \ a 2 .9 mge\.tra /gcm found at 1 20 bar and 55 °C . Thi was also the fastest run
leading to a yield of 25 .4 0'0 u ing only around 400 ml of CO2 compared to other runs
\\ hich consumed about h ice as much CO2 .
Moreover, the olubi l ity re u l ts re ealed that at the highest pressure studied in this work
the effect of temperature i more noticeable compared to tho e at lower pressures . At 1 20
bar, the solub i l i ty j umped from 1 to 2 .9 mge}.tractigc02 when the temperature was increased
from 45 to 55 °C, however at 80 bar no s ign ificant change on the solubi l ity was observed
for the same change in temperature .
47
3 . 5
1 20 bar r-- 3 '" 0 - 1 00 bar () eo 2 .5 • O bar <.) ro .... .... 2 >< <t> OJ) E
1 . 5 '-' 0 ... .D - •
:::l • 0 • CI) 0 .5
0 30 35 40 45 50 55 60
Temperature ( 0C)
Figure 1 3 Effect of temperature and pressure on solub i l ity of henna flov. er extract in SCCO�
·U .2 Effect of p ressu re
Figures 1 4- 1 6 show the effect of pressure on the extraction yie ld . At a constant
temperature the extraction yield was improved as increasing pressure . This behavior was
expected ince i ncrea i ng the pressure increases the solvent density and hence the
sol ating power of SC-C02 which increases the amount of dissolved extract leading to
h igher yield. F igure 1 3 is in agreement with the results presented in figures 1 4- 1 6. As the
pressure i increased the solubi l ity increases ( Figure 1 3) leading to higher extraction rate.
48
0.5
0.45 T = 35 ° AA ••• 0.4 AA •• •
0.35 AA •• • •••••• A • • •
SO 0.3 •• •••• � • U 0.25 ••• <;) ...
• •• ;: 0.2 •••
o 1 5 .... 120 bar
til 0 1 . 100 bar
O.O� , e 80 bar
0 1 00 200 300 400 500 600 700 CO:! (g)
FIgure 1 ..+ e ffect of pre,' llre 011 the ex. traction yield at 35 °C
0.7
0.6
0.5
:§ 0.4 U co ... >< :..lJ 0.3
0.2
0. 1
0 0
T = 45 °C Jl;. A A A A A A A • • • • • • A •
JI;. A A •
A .. . . .... . . . A • • ••
• • . A • •
• • • •
A A • • • • • A · . ·
A Jj •• A A ,
.
A II" 1 20 bar
A •• A ••
., 1 00 200 300 400
CO2 (g) 500 600
. 1 00 bar
e 80 bar
700
F igure 1 5 E ffect of pres ure 011 the extraction yield at 3 5 °C
49
25
20
1 5 � 0 e..... :2 <U
1 0 r
5
0 800
35
30
25
20
1 0
5
o 800
0.6
T = 5 5 °C
r/I . • • • • • • •
0.5 � • •
• •• • • • • • .. . • • •
OA • . -• •
".-... • OJ) '--"" c:; 0 3
• � .... -'
.,1 x :.Ll •
0 2 • .. .-
. .-0. 1 •
.'
a a l Oa 200 300 400
CO2 ,g
Figure 1 6 E ffect of pre 'sure on the extraction )- ie ld at 55 °C
4.2 E x t ract An a l� is
4.2 . 1 GC-Anal�' is
1 20 bar
_ l Oa bar
e so bar
500 600 700
Henna flower extracts were analyzed by GC for their compositions. From a l is t of
40 a ai lable standard chemicals essential o i l , 27 components were observed in the
extracts at various condit ions in addition to about 79 components that could not be
identified but they appeared in the GC chromatograms with unique peaks and were
con idered in the calculation of extract composit ion ( Table 5 ) . Figure 1 7 shows a typical
GC chromatogram. The unidentified compounds are marked as unknowns and should be
identified by GC-MS and other teclmiques for future studies.
50
30
25
20
� 0 ;:...
I S :2 <l.) >-
1 0
5
a SOO
1 8000 1 6000 1 4000 SS 0 and 1 20 bar I :WOO 1 0000
> 000 E 6000 4000 2000
-20nO 5 1 5 25 95 1 05 Time (min)
Figure 1 7 GC chromatogram for extract obtained at 55 DC and 1 20 bar
The ident ified components in the extracts obtained by SFE were compared with those
obtained by Wong and Tong ( 1 995) using solvent extraction ( Table 1 ) . Some compounds
were ob erved in the extracts obtained by supercritical fluid extraction in this work were
also presented in the extracts reported by Wong and Tong such as; l imonene, eugenol,
and l inaloo l . On the other hand, �-ionone was reported by both techniques, but h igher
composition was obtained by upercrit ical fluid extraction. Moreover, some components
existed only in the SFE extracts with h.igh percentage and not found in Wong and Tong
extracts (e .g . eugenol acetate) .
The extract composition varied sign ificant ly at d ifferent conditions suggesting
di fferent quality for d ifferent extracts. For example �-ionone is a major component of
henna flower extract . This component constituted about 28 % of the extract obtained at
5 5 °C and 80 bar, whereas at 1 20 bar and at the same temperature only 1 .49% of �-
ionone was observed. Another example is eugenol acetate, for which the best condit ion to
5 1
operate wa 55 °C and 1 20 bar re ult ing in 25 .6% compo it ion. Different extract
obtained by FE are e pected to how di fferent bioacti it ies due to their d ifferent
compo it ional qual i ty. Thi i e ident from the re ult of the antioxidant acti ity.
In orne extract the compo it ion of some unknown component are higher than
ident ified one . For e ample unknown, Un64 is abundantly present in the extracts
obtained at 5 5 °C and 1 20 bar ( 33%), and 45 °c and 80 bar (63%). Since the number of
unknown compounds i significant i t would be usefu l to conduct further studies to
identify and i alate orne of the wlknown compound pre ent in the extracts, especia l ly
the e tracts that how significant antioxidant act iv i ty.
Tabl e : Composit ional anal ) is of extract from henna flower by GC
!mperature (OC) 55 55 55 45 45 45 35 35 essure (bar) 1 00 1 20 80 80 1 00 1 20 80 1 00 lme Time (min) 1 25.84 - - - - - - - 1 0.3 1 2 �xanal 27.27 - 0.285 - - - 0.676 0.895 1, 29.59 - - - - - - - 0.2 1 1 ]3 29.9 - - - - - - - 0.336 1. 30.26 - - - - - - - 0 . 1 72 1, 3 1 .22 1 .698 0.782 - - - - - 0.3 16 32.45 - 0.723 1 .429 - 1 .048 0.636 1 .4 1 5 -s-3-Hexenol 33 .3 - - - - - - - -ms-2-Hexenol 33 .88 - - - - - - - -h 34.24 - - - - - - - 0. 1 2 1h 34.46 - - - - - - - 0. 1 3 19 34.83 - - - - - - - 0.2 1 6 lin 35 .53 - 0.479 - - 1 . 3 ] 0 .7 1 2 0 .75 1 -111 36.24 - - 1 . 80 1 1 .037 - - -Dinene 37 .2 1 - - - - -�J1 4 1 .3 - 1 .048 4.004 1 . 337 3 .628 1 .788 4. 1 1 1 ·pinene 4 1 . 74 - 0. 1 97 0 . 1 22 In 43 . 1 ] - - - - - 0.3 1 4 - 0. 1 3 11� 43 .89 - 0.709 ethyl Oxalate 44.56 - 0.62 ] monene-S-R 45.6 ] - 1 .973 0.44 1 .607 7 .424 0 . 1 88 lIS 45 .76 - 0.06 0. 1 99 0. 1 43 0.32 ] Deole 46.55 - 3 .648 116 47. 1 4 - 0.366 1 , 48.05 - 0.293 1emisia ketone 48.72 - 0.46 l . l 58 0 .576 1 .039 0.655 1 .246 0. 1 67 11� 48.99 - 0 . 1 59 0.222 0. 1 8 0.58 1 119 49.36 - 9.576
5 2
3 5 1 20
0.954 -----
0.374 ----
0.829 --
0.628
0.727
"able 5 ComDositi, mal analvsls 0 extract from helma t10\� ?r hv (T(' (COI7I.) n,( 49.62 - 0.427 9 .9 1 9 n�1 50.04 1 .736 1 .245 2 1 .778 enzyl Alcohol 50.3 - 1 . 7 1 9 n" 50.82 - 0.305 0. 1 08 n'l 50.94 - 0. 1 94 n, 5 1 .25 - 0.47 1 1 .373 0.927 0.873 0.837 ,nalool 5 1 .63 - 0.525 0.888 1 .979 1 .699 1 . 588 0.4 1 n,� 5 1 .87 - 0.244 0.7 0.448 1 .9 1 2 0.438 n�� 52.22 - 1 . 1 85 n'7 54.43 - 1 .548 3 .838 2 .34 3 A42 2.082 3 .753 0 .207 0.84 1 rPhenylethanol 54.7 1 - 2 A88 0 . 1 08 0,057 ��b 55 .34 - 0.785 0 .265 Jh 55.56 - 3 .646 0,685 0.433 0.605 OA I 2 enthone 55 .87 -enthol 56,57 - 2 .745 omeol 57,02 - 0.3 1 4 0.392 ethyl Salicylate 57.97 0.5 1 3 5 ,2 1 7 0.548 0.879 0 . 1 4 1 0.775 �hydroca" one 58 .3 - 0.039 ih) I ntcotmate 58.83 7 .5'22 0,907 3 . 709 1 .279 1 . 785 1 . 1 94 1 .928 1 .0 1 1
n30 59.08 - 0.775 0 , 1 32
b11 59.36 - 0.209 IV one 60.44 - 0.344 0,27
enth,,1 acetate 60.86 - OA95 0.362 0.364 :>m) I acetate 6 1 1 6 -llbomyl Acetate 6 1 .-+6 - 1 ,065 a3' 62.07 - 3 ,37 2 . 1 56 4.086 2 .9 1 1 a,n 62.42 9 .38 2 .9 1 4 3 .305 0,289 Pl 62.82 1 ,348 0,52 1 .074 0.88 1 1 ,238 0,68 1 1 .095 4,30 1 0.658
" 63.08 - 0.345 0. 35 1 0.304 l AO I
1/1 63 .29 0.4 1 6 OA99 0 . 1 72 0.092
�3- 63 .44 0.336 Pllene 63.89 0.23 1 0.092
Pll\ 64.42 0.347 OA03 \genol 64 .84 2 .445 0.524 4A58 4,887 4 .06 2 . 1 1 4
�lQ 65.25 4.907 1 3 .429 3 . 1 64 3 .904
�o 65.7 2 .045 6 . 1 78 6. 776 4.386 0.639 6.745
III 66 ,3 1 OA52 0.302 0.406 0.459 0.439 0.929 �arvophyl lene 66.52 0.288 OA25 0 ,64 1 0.675 0.8 1 6 0.538
l' 66.72 0,967 4.659 2 .9 1 3 1 .029 2 .5 1 1
�1 67.47 0.394 Ihydro-B-Ionone 67,69 0 .459 1 . 834 0.54 1 1 . 1 82 1 . 1 07 0.79 K umulene 67.89 0.3 1 5 0.9 1 3 0,5 7 1 0.353
i4l 68.09 1 ,089
i14� 68.72 0,9 1 3 3 .456 1 . 1 1 9 henene 69.28 Uonone 69.74 1 .4 9 1 0.834 28 .0 1 9 1 0. 1 2 1 4.307 1 0.99 0.939 3 1 . 1 1 2
i4� 69.88 0 .335 0.326 0.044
Ill- 70.27 0,507 0 . 1 29 0.5 1 2 0.539
llR 70.49 2 .433 0.203 [genol acetae 70.84 25 .684 2 .804 1 .284 1 6.34 1 3 .972 3 . 1 98 0.725 2 .979
'-'9 7 1 .24 47 .063 3 .457 0 . 1 75
,�O 72.26 1 .609
l� r 72.73 0 . 1 76 0.343 0.796
,�, 73 ,24 0.457
�q 73,73 0.499 0.533 0.9 1 0 .475 0.559 0.592 0.92 1 .208 0.90 1
154 74.06 0.2 1 7
53
lable 5 Comnositi :))131 ana" "IS , . extract from hecna 'l(I\\ 'r hv Gl i ,-nn!.) l iethvl Phthalate 74 44 0.985 0 .406 larophyl lene o\lde 75.2 0 .68 1 n .. 75 ,4 0 774 0.377 0.092 0.496 n." 76.2 0.383 0.605 0.602 0 .3 8 1 0.66 1 n" 77. 1 0 .56 1 n •• 78 .04 0.545 1 . 877
n59 78.34 0.62 1 . 1 98 0.579 L l 73 l A33 0.64 1 . 1 97 fl1nn 79.29 0.772 6. 1 36 4 .335
i161 79A8 3 .79 1 . 593 2. 1 32 1 .734 !1;,1 80A 1 0.33 1
n..� 8 U8 8.842 J . 735 3 .642 1 0.209 5 .207 20.697 1 .244 7 .076
� 82. 1 9 33 .297 62.666 1 3 .629 1 9.796 1 .087 0.75 1 0.259 Iv.. 83.47 1 . 1 45
/It.h 83.75 1 .553 1 . 355
no' 84. 1 9 0 .4 1 8 0.708 3 .746 2 .406 3 .7 1 7 2.332 2 .4 1 4
h.., 84.56 I A4 1 1 ,48 0.993 ! . I 5 0 .8 1 6
p"Q 85.36 1 . 2 1 1 7.023 6.928 8.054 2.696 5 .569 8.574 noo 87.0 1 1 . 32 n71 87.55 0.638 0.443 h" 88.32 0.865 0 .904 n7� 90.35 0.342 n, 9 1 .05 0.822 0.303 n,< 93.43 1 .849 2.267 2.386 0.509 1 . 894
'6 94.3 1 j .238 -- 95.77 1 .005
-, 98. 1 2 0.902 1 . 1 24
-9 1 0 L5 8 6.35 1 2 .47 1 l . 293 Total 1 00.00 1 00.00 1 00.00 1 00.00 1 00.00 1 00.00 1 00.00 1 00.00 1 00.00
.t.2 . 2 Ant ibacterial acth i ty
The antibacterial act ivity test showed that no inhibit ion zone existed for the henna
flo\ er extract, sugge t ing no antibacteria l activity for the flower extracts . However, other
re earcher reported that the leaves extracts exhibi ted sign ificant ant ibacterial activity.
F igure 1 8 hows the re ul ts of antibacterial test where no inhibit ion zones against E . co l i
trains around the extracts di cs ( disc where numbered 1 to 9) compared to antibiotic
control .
54
Inhibibon zone for antibiotic control
Figure l �' Re ults of ant ibacteria l te t
4.2.3 Ant io idant actiYit)
-1. 1.3. 1 FRAP (Ferric reducing antioxidant power) assay
The F RA P as ay measures the abi l ity of the extract to reduce a ferric salt (TPTZ-
Fe ( I l l ) to a ferrous product (TPTZ-Fe( I I ) . The reaction mechanism is electron transfer
reaction hown in F igure 1 9. The reduction is due to the existence of antioxidants in the
extract \ h ich involve electron-denoting groups such as hydroxyl group. The fonnation
of the ferrous product is noticed as the color gets deeper from yel low to intense blue and
quantitati ely measured by the absorbance at 539 run wavelength .
[Fe llI)(TP _ J:t Deep Blue
Figu re 1 9 F RA P Reduction reaction
5 5
The ab orbance of each e tract mi ed with the FRAP olut ion wa mea ured and the
c ncentration of antio idant \ ere calculated a ascorbic acid equi alent from a
calibrat ion urve ( ppendi ). The re u l ts of FRA P a say for e tracts at each extraction
condition are hown in Figure 20. The FRAP a ay re ealed that compound obtained by
FE of henna Dower e hibited antio idant activity.
2 . 5 ..-., � c..> - 80 bar ce .... >< - 1 00 bar c..> co 2
0 1 20 bar 0 --
r::r c..> -< 1 . 5 -< co E '-' � >
� c..> ce � c cc X 0 0. 5 � c cc
0.. -< � !.L. 0
3 5 4 5 5 5
Temperature C Oc)
Figure 20 F RAP a ·sa.\ re 'ults for extract of henna flO\\ ers
Extracts obtained at d ifferent extract ion temperature and pressure showed
d ifferent antioxidant content. The maximum antioxidant activity was observed at 45 °C
and 1 20 bar and the minimum was at 55 °c and 1 00 bar. A c lear trend of antioxidant
activity with extraction pressure can be observed at 3 5 and 45 °C. However, at elevated
56
temperature of 55 °C 10\ e t antio idant acti ity was obtained at 1 00 bar. The ariation
in the antiox idant act i \ ity [ di fferent e tract are expected to be due to the d ifference ill
the compo it ion of compound in the e tract . For e ample the extract at 3 5 °C and 0
bar ha the highe t compo it ion of compound uch a ; Limonene-S+R and the unknown
n63 . The e, tract obtain d at 45 °C and 1 20 bar i the only extract that contain menthol
unknown 1 -1 . UN-I4, and UNS7, and has the highest composition of carvone. It would
be inter t ing to ident i fy, fractionate and then test the antiox idant properly of these
unknown compound .
-1.1.3.2 DPPH . £"avenging activity
The chemi try behind this a ay i the reduction reaction that occurs to the DPPH
molecule (2 ,2-d iphenyl- l -picryl hydrazyl ) by antiox idants in the substance. The DPPH
molecule i one of the few stable organic nitrogen radicals and characterized by deep
purple color \ ith maximum absorbance at 5 1 7 nm wavelength . This method assesses the
radical cavenging act ivity of antiox idants again t the free radical DPPH. The reduction
reaction of DPPH and by an antiox idant i hown in Figure 2 1 . Upon reduction, the color
fade a the odd electron of DPPH radical becomes paired with a free radical scavenging
antioxidant and fonn the reduced DPPH-H . The loss in color is proportional to the
antioxidant concentration; the higher the antioxidant concentration the more the color
loss ( the more the DPPH scavenging activity) . The antioxidant concentration was
calculated as ascorbic acid equivalent (AA eq) from a cal ibrat ion curve (Appendix C) and
the antiox idant or antiradical activ ity values were expressed as mm AA eq/ l OOg of
extract .
5 7
DPPH
Fi.!ure 2 1 DPPH reduction b) antioxIdant
60
50
40
30
20
0... 1 0
0.... o
o 3 5 45
Temperature °c
F igure 12 DPPH a �a) re ult for extracts of henna flo\\ ers
- 80 bar
- 1 00 bar
1 20 bar
5 5
The results o f DPPH assay agrees with the results obtained b y FRAP assay,
i ndicating that henna flower extract obtained by SFE exhibit antioxidant acti vity ( Figure
22) . Similar to the results of the FRAP assay, the extract obtained at 45 °C and 1 20 bar
has the h ighest radical scavenging activity whi le the extract obtained at 5 5 °c and 1 00 bar
exhibited the lowest act ivity. The effect of antioxidants on DPPH radical scavenging is
genera l ly due to their hydrogen donat ing abil i ty . This can be attributed to the presence of
58
adjacent ub ti tuted group uch a methoxyl group in an aromatic ring which i a
electron-donat ing group. On the other hand, the pre ence of a carbo yl group ha a
negat i \ e effect on the antiox idant act ivi ty ince i t is an electron-withdrawing group. Such
group exi t in henna Dower extra t as hOWD from the G analysis .
59
5 DATA lVIO D E L I N G
5. 1 Dc cription of the extract ion mcchan i m
It i well knO\ n tbat tbe e traction proce i the re ult of rna tran fer which i
promoted by concentration gradient . Figure 23 pre ent the teps involved in the
'upercritical fluid extract ion proces . At the beginning, supercritical carbon dioxide fi l l
the e traction ve el and equi l ibrates with ample material where free solute are
di o lved in C-C02. Thi equi l ibrium tage i to ensure the constant temperature,
pre ure, and compo ition within the extTaction y tem. In step (a ) the solutes present in
the olid part ic le d i sol e in SC-C02 within particle pores. Tbis step is governed by
olubi l ity of olute in SC-C02 or adsorption/desorption mechanism. Then, the solutes
d iffu e through the part ic le pores to the particle surface a shown in step (b) . In step ( c ),
the olute tran fer from tbe part ic le surface to the bulk phase through a fi lm. Final ly, the
o lute di ffu e within the bulk phase along the extraction vessel ( Step d). The solutes
leaving the extract ion bed are col lected and accumulated by depressurizing the
upercrit ical olution to ambient pressure in the col lection v ia l .
I t is c lear from the abo e explanation that the extraction process is governed by two
phenomena, namely the olubi l ity of solutes in SC-C02 and d iffusion of the solute
within the part icle and the bulk flu id phase.
60
� � ." �
� if + .... .. if � � ."
� �
St�1' � DuluSl" fl " f s, lutes from s" hd t" p,'res
Step \ b ) Dl1'l.i.ts1011 of s lutes wllhm Ule partIcle to the p�rlIde sur(�('e forl11mg ;t fIlm
Step \ C 1 Ddluslon of ,,,lutes frnm the pnrtJcle surface tn the bulk phnse
FIlter � -----,t---�---i i
i
i Fllte�------------
Step I " I Dl li"uSIl'11 of sl) lutes \\ 1111m U1e
bulk along U1e extractlOl1 bed
Figure 23 i\lechal1l l11 of F E process
5.2 Theoretical principle of the extraction process
It is c lear from section 5 . 1 that the extraction process takes place in two pha es
namely; particle phase, and fluid pha e. The propo ed mathematical model of the current
extraction process is based on the law of conservation of mass. Derivation of the model
equation starts by applying ma s balance around a thin shel l perpendicular to the transfer
direction in each phase. The general equation of mass balance is :
(Rate Of ) _ ( Rate Of ) + ( Rate of ) = ( Rate of ) rna in mass out - mass generated or consumed accumulated mass
The fol lowing assumptions were used to simpl ify the model equations:
6 1
( 23 )
1 . The y tern i i othennal and i obaric; therefore, upercri tical fluid propert ie
uch a ; d i ffu i it coefficient , den ity, and i co ity are con tant along the bed.
2. The part icle ha e pherical geometry and ol ute i di tributed uniformly.
3 . Radial concentration gradient are negl cted i n the fluid pha e
4 . o lute concentrat ion gradient in the part ic le i in r coordinate only.
5 . Bed and particle poro i t ie are fi ·ed during the e traction proce s .
6 . Local equ i l ibrium is e tabl i hed a t the interface of flu id and solid phase.
5.2 . 1 Partkh.' Pha c mass t ransfer
Ma tran fer on the part ic le phase occurs through two teps as mentioned
pre iou 1 . When the fluid fi l l the paltic le pores, solute transfers from the sol id phase to
the fluid pha e ins ide the particle pores, due to the concentration gradient ( h igh solute
concentration in the solid pha e compared to that in the pores) . This is usua l ly expressed
a an equi l iblium relation by solubi l ity or ad orption/desorption mechanism. Then the
o lute transfer to the particle surface by d i ffusing through the pores . This step can be
de cribed by molecular d i ffu ion equation. A deta i led description for each step i found
in the coming sections.
5. 2. 1. 1 Tran fer of solute /rom solid phase
In this step the fluid and the sol id are competing in keeping the solute. This kind
of competition is expres ed by adsorption/desorption process. Many researchers
expressed the adsorption/desorption process in the upercrit ical regions using d ifferent
models such as Langmuir-l i ke isotherm and BET type equ i l ibrium equation (J ia et aI . ,
2009b; Papamichail et a I . , 2000; Ruetsch e t a I . , 2003) . Also the adsorption/desorption
62
proce can be e pre ed imply b e ither analogy to interpha e rna tran fer a hown
chematica l ly in Figure 24, or u ing kinetic principle a di cu ed later.
Int�rt .h:e
q,
{ .,1 's,,"'I1J
Ph,l"�
Fum
FluId
t'h ""
Film
( ' ,
19ure 2-+ Interpha"e ma. s tran fer mechanism
Tr.ln .. h : r ('I f solute irl,."lm
the s'''itJ ph lS(' h"'l the
l1uIJ "Jlhm tht! p.lrtH.:k
r,'re
There are t\ 0 pha e in the interpha e mas tran fer mechanism; sol id phase, and fluid
pha e eparated by an interfacial surface. The interphase mass transfer involves three
tran fer teps; the transfer of olute through the ol id phase fi lm to the interfacial surface,
transfer aero the interface into the fluid phase within the pore , and transfer of solute
througb the fluid pha e fi lm to the bulk pha e within the pores. The mathematical
repre entation of this theory acquire two assumptions; ( 1 ) on each side of the interface,
the transfer of solute is governed by the rates of d iffusion through the phases, ( 2 ) there is
no re i tance to the mas transfer across the interface. Consequent ly, the two
concentration at the interface (ql from the sol id side and CP1 from the particle side) are in
equ i l ibrium as a result of the infinite contact time of the two phases. Assuming that the
equi l ibrium relation is l inear ( Eq.24) the rate of mass transfer from sol id phase to
part ic les pore can be written as ( Eq .25) .
( 24 )
63
dq = k (C - C ) dt a P P
Where K i the lope of the equi l ibrium curve. ka i th 0 eral l rna
(25 )
tran fer capacity
coefficient, C;, is the concentration in the pore of the part ic le in equi l ibrium \ ith q.
q = KC; (26)
The equi l ibrium relation ( Eq .24) can be u ed to relate Cp to q.
ub t i tuting with Eq. (�6) into Eq. (25 ) , the rate of mas transfer from sol id phase to
particle pore can be calcu lated from :
(27)
Another \ ay to expres the tran fer of solute from solid pha e to pore of the part ic le i
through ad orptionJde orption mechani m using the reaction kinetics principles by
implement ing the fol lowing re ersible react ion with l SI order rate can tants for both
direction :
dq - = k C - kd q dt a p
DefIning K = ka leads to kd
(28 )
64
B th approache ( Interphase rna tran fer and adsorption/desorption) re ul ted in the
arne fonn of the rna tran fer equat ion ( Eq. 27 and 28) , with di fferent phy ical meaning
for their con tant . In thi tudy parameter ka and K were fitted to the experimental data.
5. 2. 1 .2 Diffi"'iol1 withill particle pore.\
olute that i tran [erred from the ol id phase to the pore wi l l d iffu e within the
pores to\>\ ard the urface of the pa11ic le due to a concentration gradient. Molecular mass
tran fer i de cribed by Fick' law and ince the pore ize are not uniform in the particle,
effecti e di ffu ion coefficient i u ed in the flux equation:
(29)
Applying equation 23 (rna s balance) around a spherical she l l of thickness L\r
within a ingle part ic le a shown in Figure 25 ,the fol lowing equation can be obtained :
c/
r = O r = R 1 1 r - - - - - - ., 1 1 1 .... .. - � - .. , " " " " - - 1- "' ,, "
' " I ' 1 I I \ ' : t 1 1"--+1 . �u�
\ Ii ) \ , " 1 I I
' " '
... _ _ .. " ., ' 1 ' ... _ _ _ _ .... " 1 1
1 1 1 1
1 1 1 1.&1
q 'M
F igure 25 . l a tran fer in the particle phase
65
Diy iding both ide b 4rr.1r
Reananging
d 2 2 dCp dq -Ep - r NA = Epr - + r2 - ( 1 - Ep) dr dl dt
ince there i no convecti e mas transfer ( lower flow) in the pores NA = jA
Applying Fick's law of d iffusion jA = -De dCp dr
d dC dC ( ) dq D E - (r2 _P) = E r 2 ---E + r2 1 - E -
e P dr dr P dt P dt
Dividing both s ides by Epr2
S ince both Cp and q are functions of two variables ( r, t) , the ordinary derivatives are
converted to part ia l deri atives and rearranged:
( 3 1 )
Eq. 3 1 can also be written as
66
quation 32 i a partial d ifferential equat ion ith two dimen ion and ha the fol lowing
init ial and boundary condition :
at t = 0 and 0 ::;; r ::;; R :
at r = 0 . oCp = 0 or
5.2.2 Fluid Pha e mass transfer
Diffusion of the solute in the fluid phase is control led by its transfer from the
part ic le phase, which invol e hvo steps; ( 1 ) h'ansfer of solute from surface of the part ic le
to the bulk fluid pha e in the extraction e sel which j repre ented by film diffusion and
( 2 ) tran fer of solute along the extraction vessel , which is governed by molecular and
con ective mass transfer. These steps are schematica l ly demonstrated in Figure 26.
67
Filler t -- 7-, \
t \ \ F tlm dIffusion <'> \ . � , Bulk ddfuslon along ,
t I �rraCUOD bed I
i , , ,
t 1 1 FIlter
Fle-ure 26 FlUId pha e l11a�s tran fer mechani. m
5.2. 2. 1 Film diffu ion
Fi lm d iffu ion is ba ed upon the assumption that the entire resistance to d iffusion
from the part ic le urface to the bulk fluid phase occurs in a tagnant or laminar film of
con tant thicknes 8 a shown in Figure 26. Ma s tran fer takes place as a result of the
concentration gradient between the part ic le surface ( high concentration ) and the fi lm
boundary in the fluid phase ( l0\ concentration ) . The mas transfer flux through the fi lm
can be de cribed as hown in Eg .33
5.2.2.2 Bulk diffusion alo11g tire extraction bed
( 3 3 )
i nce the flu id i flowing within the extraction vessel mass tran fer is the result
of molecular d iffusion plus convecti e mass transfer (bulk flow), which can be described
a :
68
Where {)i i the inter t it ial velocity and can be calculated from the superficial velocity
and the bed poro ity:
Figure 27 sho\l the ma balance along the e tract ion bed.
Applying ma s balance ( Eq.23 ) over a control volume in the extraction bed as hown in
Figure 27 yield :
_____ L -z = L
c /' tout - - - - - - - - - z+{).z
-+ - - - - f - - - - z
I n
_____ r - z = O
FIgure 27 1a - 5 tran fer 1TI the fluid phase
Div id ing both ides by EbA6z
r (N A(z) -N ACZ+IIZ)) + ( l -Eb) k (C _ C) = de Imllz .... O t.z Eb fa pR dt
69
ub tituting the flux by NA = jA + C19i
Recal l ing Equation 33
. - - D de
JA - ax dz
Where
Further reaITangement results
( 34)
( 3 5 )
Equation 3 5 i second order part ia l d ifferential equation for solute concentration i n the
fluid phase a a function of two variables (z, t ) .
Boundary and ini t ia l condition are as fol lows:
at t = 0; all zC = Co = 0
a t z = 0; all tC = 0
de at z = L · t > 0 - = 0 J J dz
Equations 3 2 and 3 5 are the mathematical expressions for the proposed model and were
solved numerica l ly by the finite element method
70
alue of Cpo , and qo ere calculated from their corre ponding defmition which take
into ac ount ; the amount of oil di 01 ed ini t ia l ly in the fluid pha e; amount of o i l in the
ample, and the geometry of th particle and the bed a expre ed in equations 39 and 40.
( 39)
(40)
The fraction of olute ini tial ly d issolved in the fluid phase after the equil ibrium time, fo '
\', a a umed to be O. Equation 36-38 can be olved simultaneously from q(r, t) ,
Cp (r, t) , and C(z, t) profile . Once the fluid pha e concentration profile, C(z, t), i s
obtained the extract mas can be calculated from:
M et) = J; C (z = L, t)8sAdt
Where 19s i the superficial velocity and A is the cross ectional area of the extraction
ve e l . S ince both 8s and A are con tants:
M (t) = 19sA J; C (z = L, t)dt
Superficial v elocity 19s can be calculated from
19 = � S pA
(4 1 )
Where rh and p are the mass flow rate and density of the fluid, respectively, at the
extraction operating condit ions. The fluid is mainly C02 since the extract solubi l ity is low
in CO:! « 3 x l O-3 glgC02) . Therefore, fluid properties are assumed to be the same as for
7 1
pure 02 · The proces can be a umed continuous and at teady tate for CO2, therefore,
rna now rate of CO2 in the e traction e el can be as umed equal to that at the yringe
pump, \ hich i at 25 ° and tem pre ure ( P) . Since vol umetric flow rate ( F ) i
control led and recorded at the ynnge pump. Mas flow rate of CO2 ( m) can be
calculated from it den ity at temperature and pre ure of CO2 of the syringe pump
( 25°C system P) :
Therefore,
Fina l ly extraction yield is calculated from:
Yield (%) = Moo X 100 Msample
(42)
The properties of SC-C02 namely; density and viscosity were obtained from
1ST Chemistry webbook and tabulated in Table 4 . The density values were used for the
calculation of mass flow rate and supercritical velocity.
5.2.2.3 Jfodel parameters
The model equations requITe the knowledge of parameters such as effective
d iffu ion coefficient ( De) fi lm coefficient ( kf) axia l d ispersion coefficient ( Dax) , and
constants of the kinetics model ( Ka, K). The axial dispersion coefficient at each extraction
condition was calculated using the cOlTelation proposed by Tan and Liou in 1 989. Their
i nvestigation revealed that the axial dispersion is affected by the intersti t ial velocity,
72
part Ic le diameter and reduced den ity and vi co ity of upercri tical carbon dio ide. The
orrelation hown in equation 43 and ha about .5% deviation from experimental
resul t .
D = 0 08519 0 914d 0.388p 0. 725 /1 0 676 ax . 1 P r rr (43 )
Wi th Pr = 1!.. and 11 1" = £. Pc I1c
Effecti ve d i ffu ion coefficient
particle pora ity:
u ual ly related to binary d iffusion coefficient and
HO\\'ever, ince henna flower extract contain many unknown compounds, calculation or
e perimental determination of the binary d iffusion coefficient is d ifficult and time
con ummg.
Therefore, De and other parameter ( kf' ka, and K) were adjusted to fit
e perimental extraction data by minimizing the fol lowing objective function, which i the
summation of squared relat ive error.
(43)
Where yiexp is the experimental and y;'cal the calculated extraction yield and i refers to
data points used in the fitting.
73
6 l\l O D E L I � G R E S U LTS
The model equation ( 36-3 ) and e traction yield (Eq.42) were 01 ed u mg
Excel i ual Ba ic Appl ications-Mocro ( BA-Macro) . Furthennore, Powel l
minimization method u ing ubroutine avai lable wa used for fitting the model
parameter to the experimental extract ion data u mg objective function (Eq.44) . The
B -Macro code i hown in Appendix D. The calculation for the adju table parameter
at each condit ion u ing Powel l ' minimization method usual ly took 1 -2 days OD a
per onal computer ( DELL In piron 1 564, AE) .
The model \! a appl ied to each experimenta l condition and the results are hown in
figure 28-30 howing the effect of temperature and pressure. Results howed good
agreement between calculated extract ion yield by the mathematical model and the
experimental data.
The di fference ben een experimental and calculated extraction curve, R2
was
calculated for each condition using equation (44) .
2 ,\, (yexp _ yeal) 2 _ <J[ [ [
R - L yexp _yexp [ [ (44)
alue of R2
ranged from 0.96 to 0.99 as seen in Table 6 . The best agreement between
experimental and calculated extraction curve was found at 45 °C and 80 bar with R2
of
0.998 whi le the worst agreement was at 55 °C and 80 bar with R2
of 0.96.
Four fitting parameters (De l kf l kal and K) were used and their values were
adj usted to the experimental data using Powel l ' minimization method. Values of these
parameters obtained from the model are given in Table 6 at their corresponding conditions
74
along \'vith the optimum objective function and R2 alue . The fitting method re ealed
that the objective function (JObj ) wa en it ive to De and kr while K and Ka were not
affecting the objective function igni ficantly.
0.6
0 .5
0 4 -----OJ) '--" ...... � 0 3 .... ..... ><
LU O.2
0. 1
0
p= 0 bar
0 1 00 200 300 400
CO2 (g) 500 600 700
30
2 5
2 0 �
1 0
5
o
800
o �
5 5 ·C Experimental data • 45 ·C Experimental d ata • 35 ·C Experimental data 5 5 ·C model d ata - 45 ·C model data - 35 ·C model data
FIgure ]" Extraction cun e_ at 80 bar
75
0.7
0 6
0.5
§04 ti "" .... ] 0.3
0.2
0 . 1
0 0
35
P= I OO bar 30
25
20
1 5 ........ 0 � 1 0�
>= 5
0 1 00 200 300 500 600 700 800
55 °C Expenmental data • 45 °C Experimental data • 35 °C Experimental data 55 °C model data - 45 °C model data - 35 °C model data
Figure 3 t traction ('un e� at 1 00 bar
0.7
0.6
0.5 ,--... on ",:: 04 () C;l ..... ><: 0.3
UJ 0.2
0 . 1
0 0
P= 1 20 r
1 00 200 300
5 5 O( Experimental d ata 55 O( Model data
400 CO� (g)
500 600
• 4 5 O( Experi mental data - 4 5 O( Model data
F igure 30 Extraction cun es at 1 20 bar
76
35
30
2 5
2 0 :: ........, ::2
1 5 .� >-
10
5
0
700 800
• 35 O( Experi mental data _ 35 °( Model data
Table 6 dju table model paramder.
lperature °c Pre ure bar Dc X I O I �, m}! kr 1 0H. n
3 5 80 9.50 6.0
3 5 1 00 5 24 7 .88
35 1 20 0.496 0.702
45 0 1 6.3 9.42
45 1 00 20.3 1 0.9
45 1 20 0.6 5 1 2 .2
55 0 2 1 .9 1 3 .7
55 1 00 9.47 1 6 .4
55 1 20 25 .5 5.0 1
77
K, m ' vOId/m) .p Ka. - 1 m3 vOld/m' .p. OBJF R! 1 4 1 . 2 320.8 1 . 60 0.97 1 27
90.3 5 1 9 .3 0.992 0.9939
3 ,49 1 .046 1 .30 0.985 1 9
1 50 .3 1 97. 1 1 . 35 0.99838
1 39.6 45.9 1 0.403 0.97439
69.0 320.02 1 .08 0.96052
1 79.8 1 98.5 1 . 38 0.962 1 6
1 39.9 1 22 .2 1 .4 1 0.9797 1
34.05 5 1 9. 1 0.826 0.98388
7 C o n c l u s i o n a n d reco m m e n d a t i o n s
Volat i le component of henna flower \ ere e tracted u ing supercritical fluid
extraction technique over temperature and pressure range of 3 5-55 °c and 80- 1 20 bar,
respectively. traction operating condition showed ign ificant effects on the solubil ity
of extract in C-C02 and e traction yield. An extraction yield 3 1 % was obtained at 45
°c and 1 20 bar. The rna imum olubil i ty of 2 .9 mgexlraC/g CO2 wa observed at 55 °C and
1 20 bar. Other e traction parameters including; e tract cool ing temperature, and SC-C02
flow rate were al 0 fow1d to have effects on the extraction yield.
Compo itional analysis of extracts obtained at different conditions revea led the
pre ence of many compounds in the extracts. Over 1 00 compounds, 79 of which were not
ident i fied \ ere detected by Gc. Henna flower extracts did not exhibit any antibacterial
act ivity again t S. aureus and E. coli ince no inhibition zone was detected when
perforn1 ing disc d iffusion test. Tbe FRAP and DPPH tests revealed that extracts of henna
flower contain antioxidants. This assay has a great interest in nutraceutical and
phannaceutical fields.
The proposed mathematical model could fit the experimental extract ion curve
ery wel l at a l l conditions. The model was derived according to mass transfer principles
where two mass balance equations (one for the part ic le phase and one for the fl uid pbase)
governed the extraction phenomenon. The parameters· fi lm coefficient, effective
diffusivity coefficients, adsorption and equi l ibrium constants were adj ustable parameters
and fi tted to match the experimental result by Powel l ' s minimization method an objective
function defined as the minimum sum of squared relative errors. The model can be used
for a feasibil i ty study of a large scale process or selection of better conditions that yield
78
higher e tract quality. Moreo er, tbe propo ed mod I can be te ted to model
supercritical e traction of other plant materi al .
79
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88
9 A P P E N D I C E S
A p p e n d i x A
E x p e ri m e n ta l data of F E o f volati l e c o m po n e n ts fro m flower of h e n n a
Thi ection include the value of extTaction yields for each run that were
obtained experimental l y and mathematica l ly at each extract ion condition.
35 °C and 80 bar
20
1 3 5 °C and 80 bar ....... 1 6 �. ... 1 4
,........ p � � '-' 1 0 '"0 a:> >= • Experimental 6
4 - Mathematical
2 Modeling
0 0 200 400 600 800
CO, (g)
89
CO2 g
0 3 . 8832
9,-85556 1 1 .6496 1 5 5328 1 9 .4 1 6 38 .832 58.248 77.664 97.08
1 1 6 .496 1 35 .9 1 2 1 55.328 1 82 . 5 1 1 94 . 1 6
2 1 6.683 232 .992 252 .408 27 1 .824 29 1 .24
3 1 0.656 330.072 349.488 368 .904 388.32
407.736 427. 1 52 446.568 468.3 1 4
485.4 504.8 1 6 524.232 543 .648 563 .064 582.48
60 1 .896 62 1 .3 1 2 640.728 660. 1 44 679.56
698.976
0'0 Yc,p 0
0.94 1 1 9 0.74 1 99 I 1 0552 1 . 1 3042 1 .90728 2 02679 2.684 1 3 3 . 1 77 1 3 4 1 1 334 4 .52 1 69 5 .3 1 846 6.33435 6.78253 6.97 1 76 7.58926 7.9727 1 8 .38 1 06 8.83422 9.49 1 56 9.60 1 1 2 1 0 .4029 1 0.5473
1 1 . 1 1 1 .5034 1 2 .4645 1 2 .7 1 35 1 3 .3858 1 4 .0929 1 5 . 1 1 88 J 5 .288 1 1 5 .6964 1 6. 1 596 1 6.7472 1 7 .4643 1 7.8577 1 8 . 1 2 [ 6 1 8 . 1 863 1 8 .2909 1 8 .3656 1 8 .4802
0/0 Y cal
0 0. 1 30 1 2 0.5 1 273 0.62474 0.85989 1 .086 1 1 2. 1 1 6 1 7 3 .02577 3 .85056 4.6 1 004 5 .3 1 666 5.97904 6.60353 7 ,42322 7 .75727 8 .3770 I 8.806 1 4 9.29743 9.769 1 8 1 0.223
1 0.660 1 1 1 .08 1 8 1 I .489 1 1 I . 883
1 2.2642 1 2.6336 1 2.99 1 7 1 3 .3393 1 3 .7 1 67 J 4.0048 1 4.3237 1 4 .634 1 4.936
1 5 .230 1 1 5.5 1 67 1 5 .796
1 6.0684 1 6.3342 1 6.5935 1 6 .8466 1 7 .0938
90
35 °C and 1 00 bar
25
20
5
o o
CO� (g) 0
4.088 1 5
8. 1 763
1 3 .8997
20.4408
4 1 .699 1
6·U928
8 1 .763
1 02.204
1 22.645
1 43 .085
1 63.526
1 83.967
204.408
224.848
245.289
263.277
286. 1 7 1
306.6 1 1
327.052
347.493
367.934
3 88.374
4 1 0.45
429.256
449.697
470. 1 3 7
490.578
5 1 2.409
532.277
553 . 1 27
572.34 1
592.782
6 1 3.223
633.663
654. 1 04
674.545
694.986
3 5 0 and 1 00 bar
0 0 l'C\n 0
0.633 1
0.9322
1 .05683
1 .3659
2.44267
3 . 3 1 007
4 . 2 1 236
5.00997
6.2 1 1 3 7
7. 1 336
7.936 1 9
8.44965
9 56 1 32
1 0. 3 29
1 0.987
1 2.293 1
1 2 .5972
1 3 .5593
1 4.2722
1 4.7856
1 5 .4287
1 6.30 1 1
1 6.9191
1 7.5025
1 8.290 1
1 9. 1 874
1 9.332
1 9.8355
20.3 1 9
20.4786
20.5284
20.8225
20.9472
2 1 .05 1 8
2 L296 1
2 1 .3659
2 1 .4307
200
0 0 Ycal 0
0. 1 584 1
0.45262
0.85095
1 .28566
2.59 1 1 9
3 .86637
4.75634
5.75564
6.6991 1
7.5945 1
8.447 1 8
9.26 1 66
1 0.04 1 5
1 0.7898
1 1 .5089
1 2 . 1 1 93
1 2&68 1
1 3 .5 1 1 6
1 4 . 1 33
1 4.7337
1 5. 3 1 47
1 5 .877 1
1 6.4646
1 6.9496
1 7 .46 1 3
1 7.9578
1 8.4395
1 8.9384
1 9.379 1
1 9 .8283
20.2308
20.6473
2 1 .0522
2 1 .4459
2 1 .8287
22.20 1 1
22.5633
400 CO� ( g)
• Experimental
- Mathematica 1 m deling
600 800
9 1
35 °C a n d 1 20 b a r
2 5
20
;0- 1 5 � -0 V >- 1 0
5
o
CO�g 0
4.22735
9.300 1 7
1 2.682 1
1 6.9094
2 1 . 1 368
42.2735
63.4 1 03
84.547
1 04.838
1 26.82 1
1 47.957
1 69.094
1 92.767
2 1 1 .368
232.504
253.64 1
273.932
295.9 1 5
3 1 7.05 1
338 . 1 88
3 59.325
380.462
40 1 .598
422.735
443.872
465.009
486. 1 45
507.282
526.728
542.792
549.556
570.692
5 9 1 .829
6 1 2.966
634. 1 03
o
3 5 °C and 1 20 bar
200
0 0 Y<'<I' 0 0 Yea I 0 0
1 .06 1 07 0. 1 99 1 5
1 . 1 8063 0.63856
1 .4 1 477 0.9 1 757
1 .52436 1 .25305
1 63894 1 .57622
2.665 1 4 3 .05587
345223 ·U7269
4.5 1 828 5.57233
5 80353 6.63693
6 . 8 1 977 7 . 7 1 074
7.91 073 8.67678
8.75262 9.5862 1
9.9980 1 1 0.5456
1 0.6556 1 1 .26
1 1 4078 1 2 .0338
1 2 .2596 1 2 .7707
1 3 . 1 1 65 1 3 .446
1 4.0879 1 4 . 1 449
1 4 .9 1 48 1 4.787 1
1 5 .8862 1 5 .4022
1 6.7729 1 5 .99 1 8
1 7 .6796 1 6 .5576
1 8 .46 1 7 1 7 . 1 008
1 93982 1 7 .6228
1 9.8864 1 8 . 1 247
:W.255 1 1 8 .6075
20.6685 1 9 .0722
2 1 .062 1 1 9 .5 1 96
2 1 .27 1 3 1 9.9 1 66
2 1 .4307 20.2346
2 1 .62 20.3658
2 1 .62 20.766
2 1 .6599 2 1 . 1 5 1 8
2 1 .7695 2 1 .5238
2 1 .7595 2 1 .8826
400
CO� ( g)
• Experimental
- Mathematical Model ing
600
92
800
45 0 a n d 80 ba r
30
25 45 0 and o bar
�20 " 0 � � 1 5 �
>- 1 0 • Experimental
5 athematical odel ing
0 0 200 t-JO
C 1 (g) 600 800
CO� g 0 0 Y c," 0 0 y,.11 0 0 0
3,8832 0.70247 0. 1 3 1 2 7
9.3 1 968 0.86688 0.475 1 8
1 1 .6496 I 1 5584 0.62009
1 6.3094 1 .27043 0.90564
1 9 .4 1 6 1 .36509 1 .09322
3 8.832 2 .48 1 07 2.215 1 8
58,248 3 . 1 636 1 3.30 1 7 1
77.664 4 05042 4.33378
97.08 4.77282 5.3'2772
1 1 6 .496 5 .5002 6.28778
1 3 3 5�2 6.342 1 7 7 . 1 07 1 1
1 58.43 5 7.43822 8.25969
1 74.744 8. 1 7557 8.99257
1 95 .7 1 3 9.0823 9.90925
2 1 3 .576 9.87445 1 0.6686
2E992 1 0.7065 1 1 .4726
252.408 1 1 .3242 1 2 .2553
2 7 1 .824 1 2 .08 1 5 1 3 .0 1 76
2 9 1 .24 1 2 .8 1 89 1 3.7604
3 1 0.656 1 3 .6309 1 4 .4843
330.072 1 4.3882 1 5 . 1 9
349.488 1 5 .255 1 1 5 .878 1
3 7 1 .234 1 6.22 1 6 1 6.6287
388.32 1 7. 1 682 1 7.2038
407.736 1 8. 1 397 1 7.8424
427. 1 52 1 8.7625 1 84654
446.568 1 9 .42 5 1 1 9.0733
465.984 20.008 1 9.6664
485.4 20.48 1 3 20.2452
504.8 1 6 2 1 .2983 20.8 1 0 1
524.232 22.0506 2 1 .36 1 3
543.648 22.7232 2 1 .8994
563.064 2 3 .3 2 1 224245
5 82.48 23 .6299 22.937
601 .896 23 .9886 23 .4372
62 1 .3 1 2 24. 1 63 23.9255
640 728 24.3922 24.402 1
660. 1 44 24.427 1 24.8673
679.56 24437 25.3 2 1 4
698.976 24.407 1 25.7646
93
45 °C a n d 1 00 b a r
35
30 45 °C and 1 00 bar
2 5
--;;- ')0 ::..- --0 � 1 5 >-
1 0
5
0 0 200
CO� (g) 00 Yo," 0 0
8 . 1 763 0.7 1 325 1 2.2645 0.932 7 1 1 6.3526 I 1 3223 20.4408 1 . 1 82 1 40.88 1 5 2.26944 6 1 .3223 3.63 1 1 86.6688 4.6 1 37 204.408 1 0.2649 2 1 5 .037 1 0.9033 245.289 1 1 .45 1 9 265.73 1 3. 1 528
277. 1 77 1 4. 1 453 306.6 1 1 1 6.0 1 58 327.052 1 7.2876 347.493 1 7. 8 1 63 367.934 1 8 .385 388.374 1 9.3376 408.8 1 5 20.4 429.256 2 1 .2878 449.697 21. 1 457 470. \ 3 7 23 . 1 483 490.578 24. 1 259 506. 1 1 3 24.9339 529.824 25 .4576
55 1 .9 26.3604 572.34 1 27.83 1 8 592.782 28.8294 6 1 3.223 28.8543 633 .663 28.949 1 654. 1 04 28.939 1 674.545 29.5925 694.986 29.83 1 9
...... • , ..
•• • +
• Experimental
- Mathematical Model ing
400
CO2 (g)
600
0 0 YC.l1 0
0.2842 0.53 1 5 1 0.77855 1 .02352 2.2 1 752 3 .36835 4.74577 1 0.5836
1 1 .072 1 2 .4308 1 3 .3238 1 3.8 1 52 1 5 .05 1 6 1 5.8875 1 6.7055 1 7.5059 1 8.2893 1 9.0559 1 9.8063 20.5407 2 1 .2595 2 1 .963 1 22.4879 23 .2726 23.9858 24.63 1 8
25.264 25 .8829 26.4888 27.08 1 8 27.6623 28.2306
94
800
45 °C a n d 1 20 b a r
35 45 0 and 1 20 bar
30
25
"? ')0 � -:2 � 1 5 >-
1 0 • Experimental
5 - Mathematical
0 Modeling
0 200 400 600 00 °2 (g)
CO� g 0 0 YCX" 0 0 Yc,1 0 0 0
5.9 1 829 1 .297 1 5 0.49515
8.4547 1 1 4748 0.804
1 2.682 1 1 .87088 1 .29932
1 6.9094 1 .94512 1 .77279
2 1 . 1 368 2.0:W55 1 . 22804
42.2735 3 .38256 4.30077
63.4 1 03 4 84434 6. 1 1902
84.547 6.24616 7.78 1 03
1 05.684 7.88266 9.29422
1 39.503 1 0.41 7 1 1 1 .484
1 69.094 1 1 .7242 1 3 .1093
201222 1 2 4726 1 4 .9 1 6 1
1 1 1 .368 1 4.2836 1 5 .4133
131.504 1 5 .5508 1 6.435 8
253.64 1 1 7. 1 622 1 7 .3928
274.778 1 7.8408 1 8 .299
295.9 1 5 1 8 .983 1 1 9. 1 581
3 1 7.05 1 20. 1 107 1 9.9738
338. 1 88 2 1 .9 1 1 8 10.7488
359.325 1 3 .1389 1 1 .4859
380.462 25 .3 1 43 12. 1 874
3 9 1 .453 15.6935 11.5389
412.735 26. 1 824 13 .492 1
443.872 17.0904 24 0989
465.009 28.2618 14.6775
486. 1 45 28.9862 25.2294
507.281 29.2556 15.756 1
538.564 30.2934 26.49 1 8
549.556 30.6476 26.7385
570.691 30.881 1 27. 1 966
59 1 .829 30.8 5 7 1 27.6339
6 1 2 .966 30.882 1 28.05 1 6
634. 1 03 30.872 1 28.4505
655.239 30.882 1 28.83 1 6
676.376 30.882 1 19. 1 955
95
55 °C a n d 80 ba r
35
30 5 5 °C and 0 bar
25
� 20 -0 u
1 5 >-1 0
5
0 0 1 00 200 300
CO� (g) ° 0 '{C-X" 0 0 YCd! 0 0 0
3 .8832 0.60709 0. 1 5 1 38
7.7664 0 90565 0.42975
1 1 .6496 1 .249 0.70395
1 5 .5328 1 37838 0.97362
1 9 .4 1 6 1 .54757 1 .23936
38.832 2.4582 2.52052
58.248 3 .8863 5 3 .73863
77.664 4.60788 4.90589
99.4099 5.98627 6. 1 6 1 47
1 1 6.496 6.60828 7. 1 1 38
1 3 5.9 1 2 7.479 1 8. 1 627
1 55.328 8.44447 9. 1 7877
1 74 744 9.6636 1 1 0. 1 642
1 94. 1 6 1 0.4399 1 1 . 1 208
2 1 3 .576 1 1 .3406 1 2 .05
232.992 1 2 .3 1 09 1 2 .9533
256.29 1 1 3.6246 1 4. 0044
2 7 1824 1 4.5253 1 4.6862
29 1 .24 1 5 .5603 1 5 .5 1 77
3 1 0.656 1 6.3266 1 6 .3272
3 30.072 1 7 .5707 1 7 . 1 1 54
349.488 1 8.302 1 1 7 .8828
368.904 1 9.3 1 73 1 8 .6303
3 88.32 20. 1 732 1 9.3584
4 1 0.066 20.7454 20. 1 5 1 5
4')9.482 2 1 .3376 20.8403
446.568 2 1 .9098 2 1 .43 1 7
465.984 22.3726 22.0876
485.4 22.6363 22.7267
504. 8 1 6 23.0693 23.3495
524.232 2 3 . 1 389 23 .9563
543.648 23.3 1 8 1 24.5476
568.5 23.3479 25.2826
59·t 1 3 23 .4972 26.0 1 54
684.22 ')3 . 5569 28.4023
698.976 23.527 1 28.7667
7 1 8.392 23 .5768 29.2355
400 500 O2 (g)
96
...
• xperimental
- Mathematical Model ing
600 700 800
55 °C a n d 1 00 b a r
3 0
2 5
20 � <> ;:... "0 � 1 5
>-1 0
5
a a
COe (g) 0
4.088 1 5
8 . 1 763
1 2 .2645
1 6.3526
20.4408
40.88 1 5
6 1 .3223
�1 .763
1 02 . 204
1 1 4.468
1 43 .085
1 63 5�6
I§3.967
2 1 2 5§4
224.848
230.572
265.73
286. 1 7 1
306.6 1 1
3 27.052
347.493
367 934
3 88.374
408. 8 1 5
429.256
449.697
470. 1 3 7
490.578
5 1 8.377
53 1 .46
55 1 .9
592.782
6 1 3.223
633.663
654. 1 04
674.545
694.986
7 1 5.426
55 0 and 1 00 bar
200
0 0 Ynn 0
0.78854
0.93826
1 .44732
1 .68688
2 . 1 7597
3 .20407
3 .64825
5 .43495
5 .80925
6.73 754
7.65085
8.559 1 7
9.79688
1 1 . 1 643
1 1 .823 1
1 2 .8462
1 3 .505
1 4.568
1 5 .9455
1 7 .0 1 85
1 7 .9668
1 9. 1 645
1 9 .7535
20.74 1 6
1 1 .9694
13. 1 97 1
23.8309
�5 .0786
26. 1 666
26.6307
27.0799
27. 1 348
27.7936
27.7736
27.7886
27.8036
27.7886
27.7786
° 0 Yeal
400 CO� (g)
0
0. 1 9453
0.55 1 02
0.89976
1 .23798
1 .567 1 1
3 . 1 0737
4.5 1 565
5. 82469
7.053 1 2
7.75677
9.3 1 396
1 0.362
1 1 .3626
1 2.69 1 9
1 3 .2382
1 3 .4886
1 4.9676
1 5 .7838
1 6.5703
1 7 .329
1 8 .06 1 4
1 8.7689
1 9 .4528
20. 1 1 4 1
20.754
2 1 .3735
2 1 .9733
21.5543
23.3 1 58
23 .663 1
24. 1 92 1
25.2017
25.6853
26. 1 536
26.608
27.0489
274769
27.8923
• xperimental
atheematical odel ing
600
97
800
55 °C a n d 1 20 bar
30
25
20
1 0
5
o o
C02 g 0
3 . 1 829
5 .00 1 7
6.8205
9.094
1 1 .3675
2 1 .8256
34. 1 02 5
45 .47
56.8375
68.205
78.2084
92.7588
1 02.3075
1 1 4.5844
1 25 .4972
1 36.4 1
1 47.7775
1 59 . 1 45
1 70.5 1 25
1 8 1 .88
1 93 .2475
55 ° and 1 20 bar
50
0'0 y �'P
0
1 .327677
1 .7070 1 3
2 .066384
2 .600449
3 .03968 1
4.69678 1
6.443723
8.485 1 5 1
1 0.47667
1: 2 .09384
1 4. 1 3027
1 6.22 1 6 1
1 8. 1 1 829
20.20464
22 .226 1
23 .66858
24.6868
25 . 1 6596
2 5 .4 1 552
2 5 . 5 1 036
25.50537
0 0 Yea I
1 00 CO2 (g) 1 50
0
0.54 1 789
1 .003844
1 .457 1 06
2 . 0 1 3066
2 .55856 1
4 .954 1 33
7 .564377
9 .8 1 1 672
1 1 .9 1 03 7
1 3.87 1 2
1 5 .490 1 2
1 7 .679 1 3
1 9.0 1 59
20.62656
2 1 .96263
23 .2 1 459
24 .43499
25 .57547
26.64 1 27
27.63728
28 .56806
• Experimental
- Mathematical Model ing
200
98
250
A p p e n d i x B
G a C h ro m a togra phy res u l ts of h e n n a flower ext racts
Thi ection pre ent the chromatogram of extract at ach condition obtained by Gc. The
chr matogram are hO\ n in th fol lowing figure :
> E
1 8000
1 3000
000
3 000
-2(J�0 5
1 8000
1 3000
> E 8000
3000
-2(J�0 5
35 °C and 80 bar
Time ( min)
35 °C and 1 00 bar
1 5 2 5 3 5 45 55
Time ( min)
99
65 75 85 95 1 05
I 000 35 °C and 1 20 bar
1 3000
> E 000
3000
-2000 5 1 5 25 35 45 55 65 75 85 95 1 05 Time (mi n)
45 °C and 80 bar
I 000
1 3000
> E 8000
3000
-2000 5 1 5 25 3 5 45 55 65 75 85 95 1 05
Time ( min)
1 00
45 °C a n d 1 00 b a r
000
000
> E 000
3000 j -2060 5 1 5 25 3 5 4 5 55 65 75 85 95 1 05
Time ( m i n )
I 000 45 °C and 1 20 bar
1 3000
> E 000
3000 J -2060 5 1 05
Time (min)
1 0 1
> E
1 000
1 3000
000
3000
1 000
1 3000
� 000
3000
-2000
1 000
1 6000
1 4000
1 2000
1 0000 > 8000 � c
6000
4000
2000
-2000
5 1 5 25
5 I S 25
5 1 5 2 5
55 °C a n d 80 b a r
3 5 4 5 55 65 75 85 95 1 05 Time ( m i n )
55 °C a n d 1 00 bar
35 45 55 65 75 85 95 1 05
Time ( m i n )
55 °C and 1 20 bar
1 05
Time ( min)
1 02
A p p e n d i x C
Thi ect lOn pre ent the calibration urve obtained for FRAP and DPPH a ay .
The cal ibration curve a prepared by plotting concentrat ion of A corbie Acid ranging
from 0 to 1 00 ppm er u their ab orbance at 539 run a hown in Figure 3 1 and the
cal ibration equation \ a found to be:
E 1.5 0.. 0.. 1
"0 'v 0.5 1'0
I.J :c 0 ... 0 I.J 0 2 0 4 0 60 VI
-0. 5 80 c:t Absorbance at 539 nm
Figure 3 1 Cal ibration cun e for F RA P assay
R2 = 0.981
100 120
Concentration (ppm) = 0.0 1 2 1 Abs - 0.0342
1 . 8
1 .6 R2 = 0.9587
E 1.4 c:
i' 1 . 2 .-I U"I
1 ... •
1'0 QI 0.8 I.J c:
0.6 1'0 .0 ...
0 . 4 0 VI .0
0.2 c:t • 0
-0. 2 0 2 0 4 0 60 80 100 120
Ascorbic Acid concentration (ppm)
FIgure 32 Cal ibration cun e for DPPH assay
Absorbance = - 0.0 1 5 6 concentration (ppm) + 1 .5474
1 03
A p p e n d i x D
Sol ut ion to t h e model eq u a tions
I n the part icle phase:
Recal l ing equation 32 and 2
let n and k present the time and radius domains respectively,
acp _ cp k,nH -Cp k,n at t!.t
acp _ cp k+1 ,n -cp k- l,n ar 2t!.r
a2 cp _ cp k+ l.n -2Cp k,n + Cp k- l,n ar2 t!.r2
Starting with Equation 28 :
aq q k.nH - q k,n at t!.t
q k.n H - q k,n = k (C _ q kn) t!.t a p k.n K
Rearranging yields
q k,n+t = q k.n (1 - t,t;) + t,tka Cp k.n
1 04
( 32 )
(28)
( 36)
Equati n 32 can be rearranged and con erted to finite element a fol low
Cp k.nH-Cp k.n = ZDe (Cp k+ l.n -cp k-l .n) + D cp k + l.n - ZCp k.n + Cp k- l.n _ ( l -Ep) q k,nH-q k,n M kllr Zl1r e l1r2 Ep l1t
Rearranging results
_ 2De ( ) IHDe ( ) (l-Ep) ( ) Cp k.n+t -cp k.n + kllr2
cp k+ l.n - cp k-l,n + t;;2 cp k+ l.n - 2Cp k,n + cp k-l,n -£- q k,n+t - q k,n p
Sub tituting itb q k,n+ t from equat ion 36 :
c = (1 _ 2�tDe _ ( I - £p) fj.tk ) c + (�tD. _ MDe) C + (MOe + MOe) C + ( l -Ep) fj. t ka q p k.nH M2 £p
a p k,n M2 kl1r2 p k- l,n kllrz l1r2 p k+l.n £p K k,n
Defining
M - �tD Mz - (I-Ep) fj.tk 1 - �r2 ' - <p a
(37)
The fol lowing criteria should be taken into account to en ure real istic physical results :
a) (1 - 2M1 - M2» o
Hence,
1 05
k > l
The init ial and boundary condition
at k = 0 . acp = 0 = cp k+ l.n -Cp k- l.n , ar 2�r
hence Cp k+ 1.n = Cp k- l .n
aq = 0 = q k+ l n -q k.n ar �r
there/ore, q k+ l.n = q k.n
at k = R ;
. D Cp R+ l,n -Cp R,n - k (c C ) . , - e �r - fa pR.n - m,n
I n th e fluid phase:
Recal l ing Equation 3 5 :
( 3 5 )
1 06
let m presents the z domain
oC _ Cm.n+ I - Cm,n at M
oC Cm + 1 n - Cm -l,n az 2 6z
a2 c _ Cm+ 1 n - 2 Cm.n + Cm - l , n az2 6z2
ub tituting into Equation 3 5 :
D ( Cm + l .n - 2 Cm.n + Cm - I ,n ) _ {J . ( Cm + l ,n - Cm-l,n) + (l-Cb) k a(C _ C ) = Cm,n + l - Cm,n ax f1z2 l 2f1z Cb f pR,n m,n M
Rearranging yields:
(Dn> 0, ) ( l -Cb) k 2Dax ) (Dax 0, ) (I -'b) Cm " + 1 = --:;- - - f1tCm+1 " + 1 - -- f aM - -2 I!.t Cm " + 2 + - I!.tCm- 1 n + -- kraI!.tCpR n . 6z· 26z ' 'b 6z ' l!.z 26z " b '
fi ' M Dax M {)l d M De m mg 3 = - 4 = - - an 5 f1z2 ' 2f1z '
The fol lowing criteri a should be val id for real istic results :
a) M3 + M4 > 0, D� - � > 0 /j,z" 2/j,z
therefore
b) (1 - MsM - 2M3M) > 0
1 M < --Ms + 2M3
1 07
In i t ia l and boundary condition
at n = 0; C = 0
at m = 0 ; C = 0
at m = L ;
ac = 0 = az
Cm+l .n-Cm.n l!.z
hence, Cm+ 1,11 = Cm,l1
1 08
E x cel V i s u a l Basic A p p l icat ion M ac ro (V BA - M acro) Code
Thi ection include the code that \ a written in Excel YBA-Macro for mathematical
model ing of FE from henna flower .
The code i a fol low
Pub l l C pcom ( 5 0 ) , x i com ( 5 0 ) , n c om Fu n c t l on FUNC ( x ) Dim c ( 1 0 0 1 ) , c 1 ( 1 0 0 1 ) , Y ( 1 0 0 0 0 0 0 0 ) , t ( 1 0 0 0 0 0 0 0 ) , q 1 ( 1 5 1 ) , c p 1 ( 1 5 1 ) , c p ( l 5 1 ) , q ( l 5 1 ) , texp ( 1 0 0 ) , ye xp ( 1 0 0 ) , yca l ( 1 0 0 ) Dim n t A s Long , n z A s Long , n r A s I n tege r
fo = Wo r ks h e e t s ( " v � s u a l ba s i c " ) . Range ( " c 3 6 " ) . Va l ue M i n f = Wor k s hee t s ( " v l s ua l ba s l c " ) . Range ( " c 3 7 " ) . V a l ue 0 1 2 = Wo r k s hee t s ( " v i s u a l b a s i c " ) . Ran ge ( " c S 7 " ) . Va l ue Oax = Wo r k s he e t s ( " v i s u a l b a s i c " ) . Range ( " c 6 1 " ) . Va l u e ep = W o r k s h e e t s ( " v l s u a l ba s i c " ) . Range ( " c 8 " ) . Va l ue F = Wo r k s he e t s ( " v :. s u a l b a s i c " ) . Range ( " c2 6 " ) . Va l ue dens i t y = Wo r k s he e t s ( " v i s u a l ba s l c " ) . Range ( " c 4 1 " ) . Va l u e Msamp l e = W o r k s h e e t s ( " v i s u a l b a s l c " ) . Range ( " c 3 0 " ) . Va l ue ibn = W o r k s h e e t s ( " v i s u a l b a s ic " ) . Ran ge ( " n 4 3 " ) . Va l ue Ndat = ibn
De = Abs ( x ( l ) ) * 0 . 0 0 0 0 0 0 0 0 0 0 0 1 k f = Abs ( x ( 2 ) * 0 . 0 0 0 0 0 0 0 1 k = Ab s ( x ( 3 ) ) ka = Abs ( x ( 4 ) )
o To ibn Fo r l b = t e xp ( ib ) yexp ( i b ) Next i b
Wo r ks hee t s ( " v i s u a l ba s i c " ) . Ce 1 I s ( S + i b , 1 5 ) . Value Wo r k s hee t s ( " v i s u a l ba s i c " ) . Ce l l s ( S + ib , 1 7 ) . Va 1 u e
i b 1
dp 0 . 0 0 0 5 0 4 rp dp / 2 # r = r p
L 0 . 0 5 D 0 . 0 1 6 p i 1 = 3 . 1 4 1 5 9 2 6 5 4 a = p i l * ( D A 2 ) / 4 # u s = F / ( den s i t y * a ) p o ro s i t y = 0 . 5 u i u s / po r o s i t y Mo 0 . 0 0 0 6 1 9
co 0 qo ( 1 - f o ) * M o / ( a * L * ( 1 - p o r o s i t y ) * ( 1 - e p )
1 09
Cpo = fo * Mo / ( a * � * ( 1 - poro s i t y ) * e p )
t f 6 0 0 0 0 n r 2 0 d r r / n r
Wo r K shee t s ( " v l s u a l b a s i c " ) . Range ( " A 1 0 0 : B I O I " ) . C l e a rContents Wo r K s h e e t s ( " v i s u a l b a s i c " ) . Range ( " OC 1 1 8 : 0E 3 0 0 0 " ) . C l e a rContents
d zmax = 2# * Oax / u i d z = d zmax - ( dzmax / 1 0 ) n z = CLng ( L / d z ) s t epdr : dt.max 1 = 1 # / ( 2 # * Oax / ( d z " 2 # ) + 3 # * k f * ( 1 # - p o ro s i t y ) / ( rp * p o ro s l t y ) )
dtma x 2 = 1 # / ( ( 2 * De / ( ep * ( dr A 2 » + ( 1 - e p ) * ka / e p » d ma x 3 = k / k a : f dtmax 1 < dtma x 2 A n d dtmax 1 < dtma x 3 Then dtmax = dtma x 1 E l s e I f dtma x 2 dtma x 1 A n d dtmax2 < dtma x 3 The n dtmax dtmax2 E l s e d max dtmax3 End I f dtma x = dtma x - ( dtmax / 1 0 ) dt = dtmax I f d t > 3 Then dt. = 3 End I f
n t = C L n g ( t f / dt ) drmin ( ( 2 * De * dt ) / ( ep * ( 1 - ( ( 1 - e p ) * d t * k a / e p » » " 0 . 5
d rma x De / k f I f d r < drmi n Then d r = dr�in + ( drmin / 1 0 ) Wo r k s he e t s ( " v i s u a l b a s i c " ) . Ce l l s ( 1 0 0 , 3 ) . Va l u e Go To s tepdr E n d I f I f d r > drmax Then dr = d rmax - ( drmax / 1 0 ) W o r k s h ee t s ( " v i s u a l b a s i c " ) . C e l l s ( 1 0 0 , 4 ) . Va l u e Go To s ""C.epdr E n d r :
I f ( d z > = 2 # * Oax / u i ) Then W o r k s h e e t s ( " v i s u a l ba s l c " ) . Ce l l s ( 1 0 0 , 1 ) . V a l u e
E n d I f
" d r i s sma l l "
" dr i s l a rge "
" d z i s l a rge "
I f ( dt > = 1 # / ( 2 # * Oax / ( d z " 2 # ) + 3 # * k f * ( 1 # - poros i t y ) / ( rp x p o r o s i t y » ) Then
W o r ks he e t s ( " v i s u a l ba s i c " } . Ce l l s ( 1 0 1 , 1 } . Va l ue = " dt is l a r ge " E n d I f I f ( dt >= 1 # / ( ( 2 * De / ( ep * ( d r A 2 } ) + ( 1 - e p ) * k a / e p } } ) Then
W o r k s h e e t s ( " v i s u a l b a s i c " ) . Ce l l s ( 1 0 1 , 2 ) . Va l u e = " dt is l a r ge " E n d I f
1 1 0
Ml Dax / ( dz A 2 ) M2 - U l / ( 2 Ji . dz ) M3 3 * k f * ( 1 - p o r o s i t y ) M4 De * dt M5 ( 1 - e p )
e l ( 0 ) 0 # t ( 0 ) 0 Y ( O ) = 0
/ ( dr .. dt
Fo r ] = 1 To nz + 1 c i ( j ) = eo
Next J
Fo r J r = 0 To n r q I ( j r ) = qo cp I ( j r ) = Cpo
ext j r
" 2 ) * k a / e p
/ ( r * poros i t y )
c p I ( n r + 1 ) c p I ( n r ) - d r * k f * ( cp I ( n r ) - c I ( O » / De
M I O 0 # Y I O 0 #
y e a I ( O ) 0 #
Fo r i = 0 To n t c ( 0 ) c l ( 0 ) e ( I ) = c ( O ) + dz * u i * c ( O ) / Dax
F o r ] = 0 To nz q ( O ) = ( 1 * - ( dt * ka / k » * q I ( O ) + dt * k a * c p l ( O ) q ( l ) = q ( O ) cp ( I ) = ( M 4 / 1 # + M4 ) * e p I ( 2 ) + ( 1 # - 2 # * M4 - MS ) * c p l ( l )
+ ( M 4 - M4 I H ) * c p l ( 0 ) + M S * ql ( 1 ) / k cp ( O ) = cp ( I )
Fo r j r = 2 To n r q ( J r ) = ( 1 # - d t * ka / k ) * q l ( j r ) + d t * k a * c p l ( j r ) cp ( J r ) = ( M 4 / j r + M4 ) * c p l ( j r + 1 ) + ( 1 # - 2 # * M4 - MS )
* c p l ( j r ) + ( M 4 - M4 / j r ) * cpl ( j r - 1 ) + M S * q l ( j r ) / k Next J r I f ( J < 2 ) Then Go To s tep z l e ( j ) = d t. * ( M l + M2 ) * e l ( j + 1 ) + ( 1 # - 2 # * M l * dt - M 3 *
dt ) * e l ( j ) + dt * ( M l - M2 ) * c l ( j - 1 ) + M3 * dt * e p l ( n r + 1 )
s t ep z I : ep ( n r + 1 )
Next j c ( n z + 1 ) c ( n z )
ep ( n r ) - d r * k f * ( cp ( n r ) - c ( j » / De
area dt * ( e ( n z ) + e l ( n z » / 2 # M = M I 0 + a r e a * u s * a Y ( i ) M * 1 0 0 # / M s amp l e t ( i ) = 1 * d t
1 1 1
For ] = 0 To n z + 1 c 1 ( j ) c ( j ) MI 0 = M
e x t J For J r = 0 To n r
c p l ( j r ) = cp ( j r ) q 1 { J r ) = q ( j r )
Next j r c p 1 ( n r + 1 ) = cp ( n r + 1 )
I f 1. > 0 Then I f t ( � - 1 ) < = texp ( i b ) * 60 And t ( i ) > texp ( ib ) * 60 Then
yca l ( i b ) = « t exp ( i b ) * 60 - t ( i - 1 » ) / ( t ( i ) - t ( i - 1 » ) * ( Y ( i ) - Y ( i - 1 » + Y ( i - 1 )
l b = i b + 1 End : f E n d I f
Next i OBJF = 0 # F o r i b = 1 T o ibn - 1 OBJF = OBJF + « yc a l ( i b ) - yexp ( ib » / yexp ( i b » A 2 Next i b W o r k s h e e t s ( " vi s u a l bas l c " ) . Ce l l s ( S , 2 1 ) . Va l ue = OBJF W o r k s h e e t s ( " vi s u a l b a s i c " ) . C e l l s ( 6 , 1 0 ) . Va l u e = OBJF Wo r k s he e t s ( " vl s u a l bas i c " ) . Range ( " i 6 " ) . V a l ue x ( l ) Work shee t s ( " vi s u a l bas i c " ) . Range ( " i 7 " ) . Va l ue x ( 2 ) Wo r k sh e e t s ( " v i s u a l bas i c " ) . Range ( " i 8 " ) . Va l ue x ( 3 ) Wo r k sh e e t s ( " v i s u a l bas i c " ) . Range ( " i 9 " ) . V a l ue x ( 4 )
FUNC = OBJF End Fun c t i on Sub Opt imi z a t i on ( )
N o r M = 4 Oim X P ( 4 ) , xi ( 4 , 4 ) FTOL = 0 . 0 0 0 0 0 1 np = D I M
F o r i = 1 T o N O I M F o r ] = 1 To N o r M
X i ( l , J ) = 0 # Next j
Next i F o r 1 = 1 To N o r M
x i ( i , i ) = 1 # ex i
Oe = W o r ks h e e t s ( " v i s u a l b a s i c " ) . Range ( " c 6 4 " ) . Va l ue k f = W o r k s h e e t s ( " v i s u a l b a s i c " ) . Range ( " c 6 6 " ) . Va l ue k = Wo r k s hee t s ( " v i s u a l bas i c " ) . Range ( " c 6 7 " ) . Va l u e ka = Wor k s h e e t s ( " v i s u a l b a s i c " ) . Range ( " c 6 8 " ) . Va l ue
X P ( 1 ) De
X P ( 2 ) k f
X P ( 3 ) k
X P ( 4 ) ka
Ca l l powe l l ( X P , X l , N O I M , np , FTOL , i t e r , f r e t )
1 1 2
Wo r ksheets ( " v _ s u a l ba s l c " ) . Range ( " i 6 : k 9 " ) . C l e a rCon e n t s Wo r k shee t s ( " v � s u a l b a s � c " ) . Range ( " 1 6 " ) . V a l u e X P ( l ) Worksheets ( " v _ s u a l bas _ c " ) . Range ( " i 7 " ) . V a l ue X P ( 2 ) Wo r k sheets ( " v i s u a l bas .L c " ) . Range ( " i 8 " ) . Va l ue X P ( 3 ) Wo r k sheets ( " v i s u a l b a s _ c " ) . Range ( " i 9 " ) . V a l u e X P ( 4 ) Wo rksheets ( " v l s u a l ba s l c " ) . Range ( " J 6 " ) . Va l u e FUNC ( X P ) Wo r k sheets ( " v i s u a l bas l c " ) . Range ( " j 7 " ) . Va l ue f r e t Wo r kshee ts ( " v� s u a l ba s l c " ) . Range ( " k6 " ) . Va l ue l te r
End Sub Sub powe l l ( P , X l , N, np , FTOL , i te r , f re t )
MAX = 2 0 I TMAX = 2 0 0 D l m pt ( 2 0 ) , p t t ( 2 0 ) , x i t ( 2 0 ) f r e t = FUNC ( P ) Fo r J = 1 To N
pt ( j ) = P ( j ) Next j l te r = 0
s t e p l : i te r = i t e r + 1
fp = f re t l b i g = 0 de l = 0 # F o r i = 1 T o N
Fo r j = 1 To N x i t ( j ) = x i ( j , i )
Next j fptt = f re t Ca l l I l nm i n ( P , x i t , N , f re t ) I f ( Ab s ( fp t t - f re t ) > d e l ) Then
de l = Ab s ( fp t t - f re t ) i b l g = 1
End I f e x t 1
I f ( 2 # * Abs ( fp - f ret ) <= FTOL * ( Ab s ( fp ) + Abs ( f ret ) ) ) Then GoTo f i n i s h
I f ( i t e r = I TMAX ) Then GoTo f i n i s h2 F o r J = 1 To N
p t t ( j ) = 2 # * P ( j ) - pt ( j ) x i t ( j ) = P ( J ) - p t ( j ) pt ( j ) = P ( j )
Next ] fptt = FUNC ( p t t ) I f ( fp t t >= f p ) Then GoTo s t e p l t = 2 * ( fp - 2 # * f r e t + fptt ) * ( fp - f re t - de l ) A 2 # - de l *
( fp - fptt ) A 2 # I f ( t > = 0 4 ) Then GoTo s t e p l Ca l l 1 1 nm i n ( P , x i t , N , f re t ) For J = 1 T o N
x i ( j , i b i g ) = x i ( j , N ) x i ( j , N ) = x i t ( j )
Next j GoTo s t e p l
f i n i s h 2 : Wo r k s he e t s ( " v i s u a l b a s i c " ) . Range ( " 1 6 " ) . Va l ue
ma x l mum i te r a t i on s "
1 1 3
" powe l l exceeding
. ni s h : End Sub Sub l � nmln ( P , X l , N, f r e t )
MAX = 5 0 t o l = 0 . 0 0 0 1 ncom = N For ] = 1 To N
p e om ( j ) = P ( ] ) x i eom ( ] ) = x i ( ] )
Nex j ax = 0 # x x = 1 # Ca l l mnb ra k ( ax , X X , bx , fa , fx , f b ) f r e t = b re n t ( a x , x x , b x , t o l , xmi n ) For j = 1 T o N
X l ( j ) = xm i n * X l ( j ) P ( j ) = P ( j ) + xi ( j )
e x t j End Sub Sub mnbra k ( a x , bx , e x , fa , f b , f e )
GOLD = 1 . 6 1 8 0 3 4
s t ep l :
- r ) )
G L I M I T = 1 0 0 # T I NY = 1 E - 2 0 f a = f 1 dl m ( a x ) f b = f l di m ( b x ) I f ( fb > f a ) Then
dum = ax ax = bx bx = dum dum = fb f b = f a fa = dum
E n d I f ex b x + GOLD * ( bx - a x ) f e = f l dim ( e x )
I f ( fb > = f e ) Then r = ( b x - a x ) * ( fb - f e ) q = ( b x - e x ) * ( fb - fa ) ma xqr = App l i e a t i on . Wor ks hee t F u n e t i o n . Max ( Ab s ( q - r ) , T I NY ) u = bx - « bx - ex ) * q - ( bx - ax ) * r ) / ( 2 # * s i gn ( maxqr , q
u l irn = b x + G L I M I T * ( ex - b x ) I f « bx - u ) * ( u - e x ) > 0 # ) Then
fu = f l dim ( u ) I f ( fu < f e ) Then
ax bx fa f b bx u fb fu GoTo f i n i s h
E l s e I f ( f u > f b ) Then e x = u fe = f u GoTo f i n i s h
E n d I f u = e x + GOLD * ( ex - bx )
1 1 4
fu = f l dim ( u ) E l se I f « ex - u ) * l u - u l im ) > O A ) Then
fu = f l dim ( u ) I f ( fu < f e ) Then
bx = ex e x = u u = ex + GOLD * ( e x - bx ) fb f e f e = f u fu = f l dim ( u )
End I f E l se I f « u - u l im ) * ( u l im - e x ) > = 0 # ) Then
u = u l im fu = f l d im ( u )
E l s e u = ex + GOLD * ( e x - bx ) fu = f l dim ( u )
E n d I f ax bx bx e x ex = u fa f b fb f e f e fu GoTo s te p l
E n d I f f i n i s h :
E n d Sub Fun c t i on b re n t ( a x , bx , e x , t o l , xmi n ) I TMAX = 1 0 0 CGOLD = 0 . 3 8 1 9 6 6 Z E P S = 0 . 0 0 0 0 0 0 0 0 0 1
a = App l i e a t i on . Wo r ksheetFune t i on . M i n ( a x , e x ) b = App l i ea t i on . Wo r ksheetFune t i on . Max ( a x , e x )
v bx w = v x = v E 0 # f x = f l dim ( x ) f v l = fx fw = f x F o r i t e r = 1 To I TMAX
xm = 0 . 5 * ( a + b ) L o l l = t o l * Abs ( x ) + Z E P S t o l 2 = 2 # * t o l l I f ( Ab s ( x - xm ) < = ( to l 2 - 0 . 5 * ( b - a ) ) ) Then GoTo s t e p 3 I f ( Ab s ( E ) > t o l l ) Then
r = ( x w ) * ( f x - f v l ) q I x v ) * ( f x - f w )
P ( x v ) * q - ( x - w ) * r
q 2 # * ( q - r ) I f ( q > 0 # ) Then P = - P q = Abs ( q ) e t emp = E E = D I f ( Ab s ( P ) >= Abs ( 0 . 5 * q * etemp ) O r P < = q * ( a - x ) O r P
>= q * ( b - x ) ) Then GoTo s t e p l
1 1 5
o = P / q u = x + 0 I f ( u - a < t o l 2 Or b - u < t o l 2 ) Then 0 GoTo s tep2
s t e p 1 :
s t e p 2 :
End I f
::: f ( x >= xm) Then E = a - x
E l s e E b x
End I f 0 = CGOLO * E
I f ( Ab s ( D ) >= t o l l ) Then u = x + 0
E l s e u = x + s i gn ( t o l l , 0 )
E n d ::: f fu = f l d im ( u ) I f ( f u < = fx ) Then
I f ( u >= x ) Then a = x
E l s e b = x
E n d I f v = w fvl = fw w = x fw = f x x = u f x = fu
E l s e I f ( u < x ) Then
a = u E l s e
b = u E n d I f I f ( fu < = fw O r w
v = w x ) Then
fv l = fw w = u fw = f u
E l s e I f ( fu < = fvl Or v v = u f v l = fu
E n d I f End I f
N e x t i t e r GoTo f l n i s h 2
s t e p 3 : xm i n = x b r e n t = f x
f i n i sh2 :
x Or v w ) Then
Wo r k s h e e t s ( " v l s u a l bas i c " ) . Range ( " 1 7 " ) . Va l u e maX l mum i t e r a "C l on s " E n d Func t i on
Fu n c t i on f I di m ( x )
1 1 6
s i gn ( to l l , xm - x l
" b r e n t exceeding
Dlm x t ( 5 0 ) MAX = 5 0
1 To ncom Fo r j = x t ( j )
Next J f l dim =
pcom ( j ) + x * x i c om ( j )
FUNC ( x t )
E !1 d Fu n c t i on Fu n c t � on s lg n ( a , b )
I f ( b > = 0 # ) The n s � gn Ab s ( a )
E l s e s � g n
E n d I f End F u n c t l o n
- Ab s ( a )
1 1 7
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