8 Combustion Bejan

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    Thermodynamicsof

    Steady Flow Combustion

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    SteadyFlowCombus2on

    Combus2onstoichiometry Applica2on of the 1st law and nd law tocombus2onprocesses

    Combined1standndlaw ndlawefficiency

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    Combus2onStoichiometry

    Combus'onburningorrapidoxida2onofHCfuels GenericformofHCfuelsCaHb CommonOxidantAtmosphericair 0.1O+0.79N (for1moleofair) O+3.76N (for1moleofO)

    CompleteCombus,on

    CaHb + Air

    CO+HO IncompleteCombus,on

    CaHb + AirCO+CO+HO

    3

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    Combus2onStoichiometry

    StoichiometricRela2on

    Wheretheistheminimumno.ofmolesofOper

    moleofCaHb effec2ngthecompletecombus2onofCaHb

    Defining4

    CH

    + O

    2+3.76 N

    2( )CO2 + H2O+N2wheretheunknownstoichiometriccoefficients are= =

    2=+

    4= 3.76 +

    4"#$ %

    &'

    4

    +

    Actual air flow rate1

    Theorectical air flow rate = >

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    Combus2onStoichiometry

    Whereisdefinedastheexcessair

    IfIncompletecombus,on IfpureOisused:

    5

    ( )

    ( )

    2 2

    2 2 2 2

    3.76

    4

    3.76 12 4 4

    C H O N

    CO H O N O

    + + +

    + + + + +

    ( )1

    1<

    Thereac2onissaidtobewith400%theore2calairorwith

    300%excessair

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    1stLawAnalysis

    Open,Steadyflowsystem

    Let,themolalflowrateoffuel

    6

    Reactants ProductsHr HP

    Q

    W

    ControlVolumeCombus2onChamber

    0 = Q W+ nrihri

    i=1

    m

    npihpii=1

    n

    nr1=

    nfuel

    0 =

    Q

    nfuel

    Q

    W

    nfuel

    W

    + rih

    ri

    i=1

    m

    Hr

    pihpi

    i=1

    n

    Hp

    0 =QW+HrHp

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    1stLawAnalysis

    Case:W=0andtempofproductsandreactantsare

    T0,P0

    quan22esevaluatedatreferenceToandPo.

    Q

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    1stLawAnalysis

    Enthalpyofforma'on

    Combus2onofCHwith(-1)excessair

    Q:Enthalpyofcombus2onofCH.

    8

    ( )

    ( )

    , 0 Elementary substances 0

    , For Compounds

    o

    o o f

    o

    o o f

    h T P h

    h T P h

    = =

    =

    Hr= h

    f CH

    o

    + 0O

    2

    + 0

    N2

    H

    p=h

    f CO2

    o+

    2h

    f H2O

    o+0+0

    Heat transfer per mole of fuelQ =hf CO

    2

    o+

    2h

    f H2O

    o

    hf C

    H

    o

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    1stLawAnalysis

    Hea2ngvalueoffuel=|Q|=HrHp

    IfHydrogenappearsasHO(vapor)LHV IfHydrogenappearsasHO(liquid)HHV

    9

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    1stLawAnalysis

    Case:Reactants&ProductsareatdifferentToandPo

    LetTandPrepresentthetemperatureandpressureof the one par,cular cons,tuent in the stream of

    reactantsorproductsandletbeitsenthalpy:

    10

    0

    r p

    ri pi o o

    Q W H H

    but h and h are not at T and P

    = +

    ( ),h T P

    h T,P( )= h To ,Po( )+ h T,P( ) h To ,Po( )

    h

    h T,P( ) = hfo+h where h is the enthalpy change

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    1stLawAnalysis

    At low pressures, cons2tuents obey the ideal gasmodel:

    Inconclusion,thepermoleoffuelenthalpyis:

    Fig 7.7 in the textbook shows that isprac2callylinearintemp.

    11

    ( ) ( ) 0oh h T only h T = =

    ( ) ( )1 1

    m no o

    r ri f p pi f ri pii i

    H h h H h h = =

    = + = +

    h T( )

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    1stLawAnalysis

    Case: W = 0 and Q = 0 (Adiaba2c). Adiaba2c Flame

    Temperature

    heretheproductsreachextremelyhightemperatures.

    System external to combus2on chamber receivesjoulespermoleoffuelLHV

    SystemisinsulatedCannotdisposeLHV1

    r pH H=

    Hea2ngValue

    Combus2on Products,To,Po

    Products

    Taf,Po

    Reactants

    To,Po

    Adiaba2candzeroworkcontrolsurface

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    1stLawAnalysis

    LHVheats themixtureof products to theAdiaba,cFlameTemperature(Taf)

    TafisobtainedfromHr(To,Po)=Hp(Taf,Po) Tafistheore2callyhighestvaluebecause:

    nocombus2onchamberisperfectlyinsulated atTafoneoftheproductscanundergochemicaldissocia2on

    E.g.COCO+O

    13

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    14

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    1stLawAnalysis

    Dissocia2onendsTnewproducts=Toriginalproducts

    Tafd

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    ndLawAnalysis

    Representsentropyinterac2ons

    16

    ControlVolume(C.C)Reactants

    Sr

    Products

    SPTi

    Qi

    /Ti

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    ndLawAnalysis

    Thepermoleoffuelstatement

    C.C.actsasproducerofentropy Adiaba2ccombus2on: Inthe Incombus2onprocesses

    17

    Sgen

    =

    Qi

    Tii

    Sr + Sp 0

    0gen p r

    S S S=

    0lim 0 ( )T s s s T = =

    ( , )s s T P=

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    ndLawAnalysis

    AtP=Po(atm)

    isduetopressurechangeatconstanttemperature

    Inmanycasestemperaturesareveryhighandpar2alpressurePsarelowtojus2fytheidealgasmodel

    18

    ( ) ( ), oos T P s T=

    s T,P( ) = s o T( )+ s T,P( ) s T,Po( )s

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    ndLawAnalysis

    Assumingallcons2tuentsareidealgases:

    If the cons2tuents appear in liquid form, ICsubstancemodelisused

    19

    1

    1

    ln

    ln

    m

    r ri o

    i o ri

    n

    p pi o

    i o pi

    PS s R

    P

    PS s R

    P

    =

    =

    =

    =

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    MaximumPowerOutput

    How chemical reac2ons are used to producemechanicalpower?

    1stLaw ndLaw

    0

    W

    Products

    Hp,Sp,Bp

    Reactants

    Hr,Sr,Br Combus2onchamber

    andpowerplant

    Steadyflowapparatus

    TemperaturereservoirToQo

    To

    0o r p

    Q W H H =

    +

    0o

    gen r p

    o

    QS S S

    T= +

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    MaximumPowerOutput

    Combined1standndlaw

    Workoutputpermoleoffuel

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    MaximumPowerOutput

    SpecialCase:inletandoutletmixturesareatTo,Po

    whereisthepar2almolalGibbsfreeenergy

    Worklost(ToSgen)isdueto: combus2onprocesses powerplantbetweencombus2onchamberandambient

    ( ) ( ), ,

    1 1

    , ,

    1 1

    m n

    rev ri o pi oo ri o pii i

    m n

    rev ri o ri pi o pi

    i i

    W h T s h T s

    W

    = =

    = =

    =

    =

    ( )oo

    h T s

    rev r p

    rev

    W G G

    W W

    =

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    MaximumPowerOutput

    Case:PowerplantreplacedbyCarnotengine

    Irreversibility(WrevW)isduetoC.C.alone

    3

    W

    QL

    Carnotcycle

    Powerplant

    Sameas-Qo

    QH=HrHp

    Tf

    ReservoirTo

    Combus2onChamber

    (To,Po)Reactants

    Hr,Br

    (To,Po)Products

    Hp,Bp

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    MaximumPowerOutput

    Effec2veflametemperatureoftheC.C.

    ndlawefficiency

    4

    Wexergy

    = H

    rH

    p( )heattransfer

    1T

    o

    Tf

    "

    #$$

    %

    &''

    1r p o

    II

    rev r p f

    H H TW

    W B B T

    = =