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MAXIMUM STRESS & DEFLECTION RESULTS SUMMARY
ITEM : Methanol Injection Skid (A!"#$%
PROJECT NO. N'A
Description Max Bending stress Result Max Deflection Result
nit psi in !!
SIDE ALL (#% )*+*,! $--."# NAME/ "."#$ "*.** ection 2 t'$ (need%ori&ontal stiffener $#+"56 #*,."* NAME/ '.()* ).", O.7
+ertical stiffener NAME/ NAME/ NAME/ ,N-ME NAME/ NAME/
SIDE ALL ($% REF8 REF8 NAME/ ,RE/0 REF8 REF8
%ori&ontal stiffener REF8 REF8 NAME/ ,RE/0 REF8 REF8
+ertical stiffener REF8 REF8 NAME/ ,RE/0 REF8 REF8
9OTTOM ALL N'A N'A NAME/ ,N1- N'A N'A
%ori&ontal stiffener N'A N'A NAME/ ,N1- N'A N'A
+ertical stiffener N'A N'A NAME/ ,N1- N'A N'A
ROOF ALL N'A N'A NAME/ ,N1- N'A N'A
%ori&ontal stiffener N'A N'A NAME/ ,N1- N'A N'A
+ertical stiffener N'A N'A NAME/ ,N1- N'A N'A
N1!!2
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TA9LE OF CONTENT:A;E
( T3RP*'2 : 4IDE 5-66 7(8 DE4I9N C-6C6-TION ) $ -
2 TR:6,$ < SIDE ALL (#% STIFFENER LOCATION # *
" T3RP*'2 : 4IDE 5-66 7(8 %ORIONT-6 4TI//ENER C-6C6-TION # !
) T3RP*'2 : 4IDE 5-66 7(8 +ERTIC-6 4TI//ENER C-6C6-TION # 5
; T3RP*'2 : 4IDE 5-66 728 DE4I9N C-6C6-TION ) " #,
# TR:6,$ < SIDE ALL ($% STIFFENER LOCATION # ##
< T3RP*'2 : 4IDE 5-66 728 %ORIONT-6 4TI//ENER C-6C6-TION # #$
$ T3RP*'2 : 4IDE 5-66 728 +ERTIC-6 4TI//ENER C-6C6-TION # #)
* T3RP*'2 : BTM 5-66 DE4I9N C-6C6-TION # #-
(' TR:6,$ < 9TM ALL STIFFENER CALCULATION # #*
(( T3RP*'2 : BTM 5-66 %ORIONT-6 4TI//ENER C-6C6-TION # #!
(2 T3RP*'2 : BTM 5-66 +ERTIC-6 4TI//ENER C-6C6-TION # #5
(" T3RP*'2 : ROO/ 5-66 DE4I9N C-6C6-TION # #"
() TR:6,$ < ROOF ALL STIFFENER CALCULATION # #6
(; T3RP*'2 : ROO/ 5-66 %ORIONT-6 4TI//ENER C-6C6-TION # $,
(# T3RP*'2 : ROO/ 5-66 +ERTIC-6 4TI//ENER C-6C6-TION # $#
A::ENDIX
(< # $$
($ 4ECTION-6 4TI//ENER PROPERTIE4 C-6C6-TION 7Botto! 5all8 # $)
(* T-B6E O/ RO-R= /ORM6- $ $- $*
N=>?e4o1 @ae3
4ECTION-6 4TI//ENER PROPERTIE4 C-6C6-TION74ide 5all(>2 and Roof 5all8
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SIDE ALL (#% DESI;N CALCULATION (:a4t #%
TAN7 NO. < T!)$-
:ROBECT < 7RA7EN F:SO
Design
Tan? %eig@tA % $' in 2'"2 !! Pressure arg psig ?P-
Tan? 5idt@A 5 *).)* in 2)'' !! Top '.'; '.=> 9endin 3t4e33+ (qb2)/ t2
4
a
4
4
4
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SIDE ALL (#% DESI;N CALCULATION (:a4t $%
TAN7 NO. < TR:6,$
:ROBECT < E:CIC OF BDA ;AS 9ALANCIN; EACUATION (EA%
Tan? %eig@tA % $' in 2'"2 !!
Tan? 5idt@A 5 *).)* in 2)'' !!
Tan? 6engt@A 6 a0 (@t$% 3.3"8 in
(@t$% )*+*,! psi
-s per Ta?le ##.- Ca3e No.#d
!1s2
?g1!"
7 liFg%7!ax8'.=> 9endin 3t4e33+ (qb2)/ t2
4
a
4
4
4
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SIDE ALL (#% DESI;N CALCULATION RESULTS
TAN7 NO. < TR:6,$
:ROBECT NO. E:CIC OF BDA ;AS 9ALANCIN; EACUATION (EA%
T@erefore A Consider Gorst condition of part ( and part 2
At Center,
Ma0i>=> De1lection >a0 (@t#% >a0 (@t$%
(.
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SIDE ALL (#% STIFFENER LOCATION
TAN7 NO. < TR:6,$
:ROBECT NO. E:CIC OF BDA ;AS 9ALANCIN; EACUATION (EA%
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REACTION FORCE DESI;N CALCULATION
TAN7 NO. < TR:6,$
:ROBECT NO. E:CIC OF BDA ;AS 9ALANCIN; EACUATION (EA%
Calc of nifor! distriuted load 758 t@at act upon @ori&ontal > Lertical stiffener
A is giLen K eloG for!ula
5 R !ax 7Plate 3(8 R !ax 7Plate 328 12
5 Rp( Rp2 12
G@ere R is calc ased on Roar? /or!ulaA Tale ((.) Case No.(a
%EI9%T sd Gall (
( (''' (''' #,,, @)
2 (''' ;'' 5*, @"
" (''' """ *,, @2
) (''' 2;' $*, @(
; (''' 2'' $*,
LEN;TK
# #*,, #*,,
2 #*,,
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SIDE ALL (#% KORIONTAL STIFFENER CALCULATION (Majo4 3ti11ene4%
TAN7 NO. < TA!)$,
SEAATER 9UFFER TAN7
Maxi!u! ending !o!ent occurs at t@e point G@ere dM1dx ' and s@ear force is &eroA
t@at isA at t@e !iddle of t@e ea!.
6 2''' !!
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SIDE ALL (#% ERTICAL STIFFENER CALCULATION
TAN7 NO. < TR:6,$
:ROBECT < S7O :i@eline3 & Facilitie3 Rej=enation :4oject < 9A:9
6 2'"2.' !! $'.'' in
,RE/0 l1in ($''.' !! a0 '.''("'* x 56)
55a
6
5
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SIDE ALL ($% ERTICAL STIFFENER CALCULATION ( >ino4 3ti11ene4%
TAN7 NO. < TA!)$,
SEAATER 9UFFER TAN7
;.
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,.,,,! 61"#' ,.,6!* in O.7
The4e1o4e the 3ie =3ed i3 ade=ate.
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SIDE ALL ($% DESI;N CALCULATION (:a4t #%
TAN7 NO. < TR:6,$
:ROBECT < E:CIC OF BDA ;AS 9ALANCIN; EACUATION (EA%
Tan? %eig@tA % $' in 2'"2 !!
Tan? 5idt@A 5 *).)* in 2)'' !!
Tan? 6engt@A 6 => De1lection+ t12 '.(($ in
3'.'"
>a0 (@t#% 0.03 in
(@t#% -+)"6 psi
-s per Ta?le ##.- Ca3e No.#a
Rectangular plate, all edges simply supported, uniform over entire plate
!1s2
?g1!"
liFg%
N1!2
-(qb4)/Et3
Ma0i>=> 9endin 3t4e33+ (qb2)/ t2
4
a
4
4
4
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SIDE ALL ($% DESI;N CALCULATION (:a4t $%
TAN7 NO. < TR:6,$
:ROBECT < E:CIC OF BDA ;AS 9ALANCIN; EACUATION (EA%
Tan? %eig@tA % ;* in (;'' !!
Tan? 5idt@A 5 ;*.'# in (;'' !!
Tan? 6engt@A 6 a0 (@t$% 0.01 in
(@t$% #+#5" psi
-s per Ta?le ##.- Ca3e No.#e
Rectangular plate, all edges simply supported, it! load increasing uniformly along idt!
!1s2
?g1!"
7 liFg%7!ax8'.=> 9endin 3t4e33+ (qb2)/ t2
4
a
4
4
4
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SIDE ALL ($% DESI;N CALCULATION RESULTS
TAN7 NO. < TR:6,$
:ROBECT NO. E:CIC OF BDA ;AS 9ALANCIN; EACUATION (EA%
T@erefore A Consider Gorst condition of part ( and part 2
At Center,
Ma0i>=> De1lection >a0 (@t#% >a0 (@t$%
'.'" '.'(
,.,- in
G@ere t12 '.(($ in
+ince +um of #a$ %eflection 5 t'2 6 .
(@t#%
(@t$%
)A"$* (A(
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SIDE ALL ($% STIFFENER LOCATION
TAN7 NO. < TR:6,$
:ROBECT NO. E:CIC OF BDA ;AS 9ALANCIN; EACUATION (EA%
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SIDE ALL ($% KORIONTAL STIFFENER CALCULATION (>ino4 3ti11ene4%
TAN7 NO. < TR:6,$
:ROBECT < E:CIC OF BDA ;AS 9ALANCIN; EACUATION (EA%
Maxi!u! ending !o!ent occurs at t@e point G@ere dM1dx ' and s@ear force is &eroA
t@at isA at t@e !iddle of t@e ea!.
6 2*'." !! ((.)" in
#;.2) l1in #''.' !! 2".# in
6oad F $.5!$ psi
unit load 5 F x psi
!*.$- l1in
use /B ;' x $
((.)" in
9endin Mo>ent
As per /ale 8.1 Case 2e of Roars )niform load on entire span*
-t x 612 ;.a0
M>a0
' 3ti11ene4
alloGale
!ax
7;56)8
55a
6
5
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SIDE ALL ($% ERTICAL STIFFENER CALCULATION
TAN7 NO. < REF8
:ROBECT < REF8
6 ,RE/0 !! ,RE/0 in
,RE/0 l1in ,RE/0 !! ,RE/0 in
6oad F REF8 psi
unit load 5 F x psi
REF8 l1in
use /B ;' x $
,RE/0 in
9endin Mo>ent
As per /ale 8.1 Case 2d of Roars )niformly increasing load* -t x '.;)$6 ,RE/0 in
Maxi!u! !o!entA
NAME/ l3in 7 6 ,RE/0 in 8
C@ec?ing 4ection Modulus of 4tiffener reFuired
M1I
%enceA 7I1K8 reFuired M1K
,N-ME
,N-ME
-lloGale 4ection Modulus of 4tiffener reFuired
7I1K8 reFuired NAME/
U3in F9 *, 0 "
I1K 7stiffener8 ,.-,* ,N-ME 7I1K8 reFuired
The4e1o4e+ Ma0 ?endin 3t4e33
!ax psi ,N-ME
De1lection
As per /ale 8.1 Case 2d of Roars )niformly increasing load*
-t x '.;2;6 ,N-ME in
EI
NAME/ ,RE/0 REF8 in REF8
REF8
M!ax '.'2(;56
2
/K
in"
in"
H>a0
M>a0
' 3ti11ene4
alloGale
>a0 '.''("'* x 56)
55a
6
5
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SECTIONAL STIFFENER :RO:ERTIES CALCULATION
TAN7 NO.
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