11 PELTON WHEEL CHARACTERISTICS.doc

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    Grading Sheet~~~~~~~~~~~~~~ 

    MIME 3470—Thermal Science Laboratory

    ~~~~~~~~~~~~~~ 

    Laboratory №.

    !ELT"# $%EEL

    !E&'"&M(#)E )%(&()TE&ISTI)S

    St*dent+, #ame+ Section №!"I#TS S)"&E T"T(L

    !&ESE#T(TI"#—(--licable to oth MS $ord and Mathcad Section+

    GE#E&(L (!!E(&(#)E/ "&G(#I(TI"#/ E#GLIS%/ 1 G&(MM(&  2

    "&E&E (T(/ )(L)L(TI"#S 1 &ESLTS—M(T%)(

      )(L)L(TI"#S 30  )"MI#E !L"T 52

    IS)SSI"# "' &ESLTS

    $%(T (&E T$" 'E(T&ES "SE&6E '&"M )"MI#E !L"T 2  $%8 IS T%E )9ET E:IT (#GLE SM(LL (# #"#E&" 2  $%(T IS !&!"SE "' )T"T (T )9ET !E&I!%E&8 2  $%(T IS T%E M(:IMM TILI(TI"# '()T"& $%E#

    α5 ; 0 2  $%8 MST ( T&I#E $

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    MIME 3470—Thermal Science Laboratory

    ~~~~~~~~~~~~~~ 

    Laboratory №.

    !ELT"# $%EEL 

    !E&'"&M(#)E )%(&()TE&ISTI)S~~~~~~~~~~~~~~ 

    L( !(&T#E&S= #(ME  #(ME

    #(ME #(ME

    #(ME #(MESE)TI"# №

    E:!E&IME#T TIME

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     be en#isioned as flow throuh rotatin no&&les. $he  pressures withinthe  mo#in  no&&le  produce  wor".  $he  flow  must  be  encased  to

    contain the water   pressure (or  suction)' in order  that the fluid cannotexpand  freely  in  all  directions.  Alternately'   the  #anes  must  be  fully

    submered in the water  flow as with a ships  propeller.

    ost water turbines in use are reaction turbines—e#en asimple spinnin lawn sprin"ler. $hey are used in low and medium

    head applications. $wo popular types of reaction turbines are the

    rancis and the >aplan turbines.n  1?!@'  enoit  ourneyron  de#eloped  a  hih  efficiency   (?0)

    outward flow water  turbine. =ater  was directed tanentially throuh

    the  turbine  runner   causin  it  to  spin.  Bean%Cictor   Poncelet  desinedan  inward%flow turbine  in about 1?!0 that used  the same  principles.

    -. . 8owd obtained a D.-. patent in 1?

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    the product of two factors' the first factor bein referred to as theutilization  factor   or diagram  efficiency  is  t!e  ratio of   t!e  ideal 

    work  output  to t!e energy available  for  conversion into work . $he#alue of the utili&ation factor may be found from the ideal #elocity

    diarams and the enery e9uations. Dnder ideal conditions' it

    should be possible to use all of the a#ailable "inetic enery of theli9uid at the turbine inlet and also the enery obtained in the rotor 

    due to pressure drop (i.e.' reaction effort). -ince the former 

    9uantity is c g V    !!

    1  

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    the tor9ue enerated. or a Prony bra"e radius of  brake  ' that

    tor9ue is

    !1  #  #  brake   ==τ

    $he forces  # 1 and  # ! are determined from sprin%loaded scales

    (see iure E).

    e. or    a  i#en  flow  rate'  one  wants  to  first  determine  the  Pelton

    wheel  rpm  with  no  Prony  bra"e  load'  rpmmaC'  and  that  Prony

     bra"e load ( # 1 and # !) that  Fust stops the  Pelton wheel'  rpm ;

    0. pm is measured usin a laser tachometer.$he Pelton%wheel  buc"et #elocity' U ' with no Prony  bra"e

    load can  be considered a ood approximation  to the actual  Fet

    #elocity'  V 1.  -ince  the  tor9ue'  τ'  is  &ero  for   this  condition'

    horsepower is also &ero ( $%  ; τω).

    =ith  the  wheel  Fust  stopped  with  the  Prony  bra"e'  thehorsepower should also be &ero.

    $here is space on the data sheet for  10 rpms for  each flow

    condition.  n  the  procedure  Fust  abo#e'  the  first  and  last  rpmsare defined.  ,ow' di#ide the maximum rpm  by 10 to determine

    the  rpm  inter#al  such  that  the  remainin  ?  data  points  can  be

    determined. easure the Prony bra"e loads for each rpm.

    'ig*re 4—!*m- !erDormance Te+t &ig and !elton $heel

    )(L)L(TI"#S

    A athcad is supplied below.

    Dse the #ariable names already

    supplied in the obFect. At the bottom of this obFect is in the

    re9uired format the student is tosupply a summary of the @0%

    rpm condition. $his alon with

    the re9uired plot should be morethan sufficient to e#aluate the

    students wor". Kne should be

    able to put all their athcadcalculations on one sheet as

    shown in iure 5.

    $he re9uired plot is as shownin iure @. $he data used to enerate this plot is 9uestionable so

    the actual shape of the cur#es is subFect to chane.

    Pump and Motor CharacteristicsImpeller OD: 5” № of Impeller Blades: 6Type of Impeller: Open Type of Blades: Backward CurvinTor!ue "rm #en$%: 5” &o$or 'peed (ane: )*+))) rpm

    VolumetricMeasuringTank

    Sump Tank

    Weight Hanger→

     Torque Arm↑

    Pump(see below

    Motor

    Pelton Wheel

    !ucketsPelton Wheel

    !uckets

    Pron" !rakePron" !rake

    PumpMotor

    Controller  

    PumpMotor

    Controller  

    Spring#$oaded

    Scale

    Spring#$oadedScale

    'ig*re 2—ECam-le "ne

    !age )alc*lation Sheet

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    'ig*re F — Sam-le !lot oD )alc*lation+

    #ote= The data *+ed Dor thi+ -lot i+ *e+tionable

    Also answer the 9uestions found in the i+c*++ion oD &e+*lt+ and

    supply a )oncl*+ion?+@.

    &E'E&E#)ES

    1.  %rinciples of &urbomac!inery' J.N. -hepherd' acillian

    Publishin 4o.' nc' ,ew Lor"' 15@.!. =i"ipedia' http2//en.wi"ipedia.or/wi"i/=aterOturbine 

    http2//en.wi"ipedia.or/wi"i/PeltonOwheel http2//en.wi"ipedia.or/wi"i/rancisOturbine 

    http2//en.wi"ipedia.or/wi"i/>aplanOturbine 

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    ,-- .,

      := /0- .,

      := ,1+ .,

      := ,-+ .,

      := /0+ .,

      :=

    2ol1

     := 2ol+

     :=2ol

    - :=

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     := $-

     := $+

     :=

    ∆31

     := ∆3-

     := ∆3+

     :=

    'U&&"(4 O, T(I"# 1 6)7: m8do$ "c$1

    k=m8do$ "c$

    219"c$1

    f$=219"c$ 219T%1

    f$=219T%

    T "c$1 .,

    f$ lf  ⋅

    =T "c$ 30 "c$1 .,

    f$ %p⋅

    =30 "c$ U1 .,

    f$

    =U

    D"T": T(I"# I/D;

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    IS)SSI"# "' &ESLTS

    =hat two features can be obser#ed from the plot of the resultsR

     'nswer)

    =hy are the buc"ets desined so that α! (see iure

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    (!!E#I:—(T( S%EET

    Time