Analysis of TTGh Inlet Air Cooling Techniques Applied to Brazilian Sites 2012

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    LIST OF SYMBOLS AND NOMENCLATURE

    Abbreviations

    ISO International Organization for Standardization

    TIT Turbine Inlet Temperature

    TIC Turbine Inlet Cooling

    Symbols Units

    Cp

    [kJ/kgC]

    COP

    [-]

    LHV [kJ/kg]

    h [kJ/kg]

    HR Heat rate

    m

    P [Pa]

    P [Pa]

    Q

    [kW]

    r [-]

    T Temperature [C]

    Tb [C]

    Tw Wet-bulb temperature [C]

    W

    Power output [MW]

    SFC

    doi: 10.5028/jatm.2012.04032012

    Analysis of Gas Turbine Performance with Inlet Air Cooling

    Techniques Applied to Brazilian Sites

    Ana Paula Santos1, Cludia R. Andrade2,*1

    2

    Abstract:Frrph r whr pwrm hh r pr rr h

    wrmmh rb r h p r r p r-

    r h pwrp b h rb r hhrm wr h

    mprr mprr r rb h pr p r -m-w

    mb mh h p m r rprpr h mprr h r h

    r r hhrrm wr h mr r C h rb

    pwrp h r mh r b rr mprr rmprr Thr r

    w b m rr b r Th r m - m h pr

    pr r m h pr wr r h rb rmprrTh mmp w w h r mh mpr brp h mh

    h mmw hrh h hr h rm h rmh r h

    pr hrmm rb prrm rr h r pwr

    p hrm r rmprr r hm Th r b

    whh m r mpr whh h wh hr m -C Th h

    hr h r mp mpm rr mprr

    r hm h rb w rr mh rw r

    mpr bw hrm mh brp hw h h brp hrpr h

    hh rm r r whwr r O h hrh pr r

    r h w r b wh m p

    Keywords: rb Trb TC pr Chrbrp

    J. Aerosp. Technol. Manag., So Jos dos Campos, Vol.4, No 3, pp. 341-353, Jul.-Sep., 2012 341

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    [-]

    [-]

    [-]

    [-]

    [kgwater

    /kgair

    ]

    Subscripts

    0

    a

    a

    C

    MC

    CL Cooling load

    g in Input

    N Net

    Turbine

    T Total

    h

    w water

    INTRODUCTION

    -

    -

    -

    Jaber a

    -

    -

    and

    J. Aerosp. Technol. Manag., So Jos dos Campos, Vol.4, No 3, pp. 341-353, Jul.-Sep., 2012342

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    GAS TURBINE CYCLE

    -

    Net.W

    0

    06

    050403

    TurbineCompressor

    Air ambient

    CombusonChamber

    P P0 03=

    P04

    P r P04 03$=

    -

    T04

    P

    PT

    TT1

    c

    04

    03

    03

    04

    1

    03h

    = - +c

    c-

    c m= G

    W m C T T ,C a pa avg 04 03$= -o o ^ h

    ma C

    pa

    ag

    -

    P05

    P P PCombustor05 04 D= -

    Q m C T T ,in a pg avg 05 04$ $= -o o ^ h

    Cpg

    ag

    LHV

    /m

    Q LHV f

    Combustor

    in

    h=o o

    Cmbr

    /T T T

    P P1

    1t06 0 5 04

    05 06

    1

    $h= - - c

    c-

    c m= G

    P

    J. Aerosp. Technol. Manag., So Jos dos Campos, Vol.4, No 3, pp. 341-353, Jul.-Sep., 2012 343

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    W m C T T ,t T pg avg 05 06$= -o o ^ h

    mT

    m m mT a f= +o o o

    and Cpg

    ag

    W W WN T C= -o o o

    SFCW

    m3600

    N

    f$

    =o

    o

    HR SFC LHV$=

    SFC LHV

    3600th

    $

    h =

    INLET AIR COOLING SYSTEMS

    -

    Net

    .W

    01

    02

    0

    06

    050403

    Compor

    Cooingym

    Evaporative cooling

    Coolingmedia

    Air cooledAmbient Air

    T Tb Tb Tw03 02 02 02f= - -^ h

    m mw a 02 03$ ~ ~= -o o ^ h

    J. Aerosp. Technol. Manag., So Jos dos Campos, Vol.4, No 3, pp. 341-353, Jul.-Sep., 2012344

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    ma

    02

    03

    -

    Q m C T T ,CL a pa avg 02 03$ $

    = -o

    o ^ h

    ma C

    paag

    Absorption and mechanical chiller systems

    -

    tion cooling.

    Ambient air

    Chilled water

    Air cooled to

    gas turbine inlet

    a

    Q m h h h ,CL a w02 03 03 02 03$ $ ~ ~= - - -o o ^ ^h h6 @

    h02

    and h03

    m mw a 02 03$ ~ ~= -o o ^ h

    -

    a

    -

    a

    -

    -

    WCOP

    QMC

    CL=o o

    -

    W W W W N t C MC= - -o o o o

    J. Aerosp. Technol. Manag., So Jos dos Campos, Vol.4, No 3, pp. 341-353, Jul.-Sep., 2012 345

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    -

    a a

    100% RH

    60% RH

    40% RH

    20% RH

    10% RH

    Inlet Chilling

    Process

    Enthalpy

    Btu Per Pound

    of Dry Air

    Evaporative

    Cooling Process

    Specific

    Humidity

    Dry Bulb Temperature

    40

    35

    30

    25

    20

    15

    4 16 27 38 49.000

    .005

    .010

    .015

    .020

    C

    RESULTS AND DISCUSSIONS

    -

    -

    taining

    11 [-]

    Turbine inlet temperature

    turbine

    100 [mmH2O]

    200 [mmH2O]

    -

    -

    72

    76

    80

    84

    88

    92

    96

    100

    104

    108

    112

    116

    [%]

    4 8 12 16 20 24 28 32 36 40 44 48

    Intake temperature [C]

    ISO Conditions:T = 15 C

    = 60 %

    TIT = 1385 K

    Heat rate

    Power output

    J. Aerosp. Technol. Manag., So Jos dos Campos, Vol.4, No 3, pp. 341-353, Jul.-Sep., 2012346

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    -

    -

    4 8 12 1 6 20 24 28 32 36 40 44 48

    Intake temperature [C]

    2.5

    3.0

    3.5

    4.0

    4.5

    5.0

    5.5

    6.0

    6.5

    7.0

    7.5

    8.0

    T

    [C]

    TIT = 1385 K

    = 60%

    = 0.95

    = 0.90

    = 0.85

    temperature drop.

    4 8 12 16 20 24 28 32 36 40 44 48

    Intake temperature [C]

    27

    28

    29

    30

    31

    32

    33

    34

    35

    36

    37

    38

    39

    40

    41

    42

    Poweroutp

    ut[MW]

    TIT = 1385 K

    = 0.90

    = 18%

    = 60%

    Base-case

    4 8 12 16 20 24 28 32 36 40 44 48

    Intake temperature [C]

    25.5

    26.0

    26.5

    27.0

    27.5

    28.0

    28.5

    29.0

    29.5

    30.0

    30.5

    31.0

    Thermalefficiency[%]

    TIT = 1385 K

    = 0.90

    = 18%

    = 60%

    Base-Case

    4 8 12 16 20 24 28 32 36 40 44 48-4

    0

    4

    8

    12

    16

    20

    24

    28

    32

    36

    40

    T

    [C]

    Intake temperature[C]

    TIT = 1385 K

    Absorption chiller: = 18% and 60%

    Evaporative cooling: = 0.90 and = 18%

    Evaporative cooling: = 0.90 and = 60%

    J. Aerosp. Technol. Manag., So Jos dos Campos, Vol.4, No 3, pp. 341-353, Jul.-Sep., 2012 347

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    -

    a

    4 8 12 16 20 24 28 32 36 40 44 48

    Intake temperature[C]

    27

    28

    29

    30

    31

    32

    33

    34

    35

    36

    37

    38

    39

    40

    Poweroutput[MW]

    TIT = 1385 K

    Absorption chiller: =18%

    Absorption chiller: =60%

    Base-case

    4 8 12 16 20 24 28 32 36 40 44 48

    Intake temperature[C]

    25.5

    26.0

    26.5

    27.0

    27.5

    28.0

    28.5

    29.0

    29.5

    30.0

    30.5

    Thermaleffic

    iency[%]

    TIT = 1385 K

    Absorption chiller: = 18%

    Absorption chiller: = 60%

    Base-case

    4 8 12 16 20 24 28 32 36 40 44 48

    Intake temperature [C]

    30

    31

    32

    33

    34

    35

    36

    37

    38

    39

    Poweroutput[MW]

    TIT = 1385 K

    = 60 %

    COP = 7.0

    COP = 4.5

    COP = 2.0

    4 8 12 16 20 24 28 32 36 40 44 48

    Intake temperature [C]

    30

    31

    32

    33

    34

    35

    36

    37

    38

    39

    Poweroutp

    ut[MW]

    TIT = 1385 K

    = 60 %

    COP = 7.0

    COP = 4.5

    COP = 2.0

    J. Aerosp. Technol. Manag., So Jos dos Campos, Vol.4, No 3, pp. 341-353, Jul.-Sep., 2012348

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    -

    obtained at

    -

    -

    4 8 12 16 20 24 28 32 36 40 44 48

    Intake temperature [C]

    34.5

    35.0

    35.5

    36.0

    36.5

    37.0

    37.5

    38.0

    38.5

    39.0

    Poweroutput[MW]

    TIT = 1385 K

    COP = 4.5

    = 18%

    = 60%

    4 8 12 16 20 24 28 32 36 40 44 48

    Intake temperature [C]

    -0.1

    0.0

    0.1

    0.2

    0.3

    0.4

    0.5

    0.6

    0.7

    0.8

    0.9

    1.0

    1.1

    1.2

    Massflow

    wa

    ter[kg/s]

    ma

    = 141.16 kg/s

    TET = 1385 C

    = 18%

    Evaporative cooling: = 0.90

    Absorption chiller

    Mechanical chiller: COP = 4.5

    4 8 12 16 20 24 28 32 36 40 44 48

    Intake temperature [C]

    -0.5

    0.0

    0.5

    1.0

    1.5

    2.0

    2.5

    3.0

    3.5

    4.0

    4.5

    5.0

    5.5

    6.0

    6.5

    Coolingloa

    d[MW]

    TIT = 1385 K

    = 18 %

    Mechanical chiller: COP = 4.5

    Absorption chiller

    Evaporative cooling: = 0.90

    J. Aerosp. Technol. Manag., So Jos dos Campos, Vol.4, No 3, pp. 341-353, Jul.-Sep., 2012 349

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    -

    -

    Table 2.

    Site 25.0

    Latitude []

    Longitude [] - 41.34

    101.25

    -

    4 8 12 16 20 24 28 32 36 40 44 48

    Intake temperature [C]

    26

    28

    30

    32

    34

    36

    38

    40

    42

    Poweroutput[MW]

    TIT = 1385 K

    = 18%

    Evaporative cooling:

    Absorption chiller

    Compression chiller: COP = 4.5

    Base case

    = 0.90

    4 8 12 16 20 24 28 32 36 40 44 48

    Intake temperature [C]

    25.5

    26.0

    26.5

    27.0

    27.5

    28.0

    28.5

    29.0

    29.5

    30.0

    30.5

    31.0

    Thermaleffic

    iency[%]

    TIT = 1385 K

    = 18 %

    Evaporative cooling:

    Absorption chiller

    Compression chiller: COP = 4.5

    Base-case

    = 0.90

    27.0

    27.5

    28.0

    28.5

    29.0

    29.5

    30.0

    30.5

    31.0

    31.5

    32.0

    32.5

    33.0

    33.5

    34.0

    Months

    DECOCTSEPAUGJULJUNMAYAPR NOVMARFEBJAN

    Ambienttemperature[C]

    70

    71

    72

    73

    74

    75

    76

    77

    78

    79

    80

    81

    DECNOVOCTSEPAUGJULJUNMAYAPRMARFEBJAN

    Relativehu

    midity[%]

    Months

    J. Aerosp. Technol. Manag., So Jos dos Campos, Vol.4, No 3, pp. 341-353, Jul.-Sep., 2012350

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    Oprar NainaSimari

    -

    -

    a a

    29.0

    29.5

    30.0

    30.5

    31.0

    31.5

    32.0

    32.5

    33.0

    33.5

    34.0

    34.5

    35.0

    Months

    DECOCTSEPAUGJULJUNMAYAPR NOVMARFEBJAN

    Ambienttemperature[C]

    DECNOVOCTSEPAUGJULJUNMAYAPRMARFEBJAN

    Months

    25

    30

    35

    40

    45

    50

    55

    60

    65

    70

    75

    80

    85

    Relativehu

    midity[%]

    Evaporative cooling: = 0.90

    Absorption chiller

    Mechanical chiller: COP = 4.5

    DECOUTSEPAUGJUL NOV0

    400

    800

    1,200

    1,600

    2,000

    2,400

    2,800

    3,200

    3,600

    4,000

    4,400

    Incremen

    talelectricenergygeneration[MWh]

    0

    400

    800

    1,200

    1,600

    2,000

    2,400

    2,800

    3,200

    3,600

    4,000

    4,400

    4,800

    5,200

    Mounths

    DECOUTSEPAUGJUL NOV

    Evaporative cooling: = 0.90

    Absorption chiller

    Mechanical chiller: COP = 4.5

    Incrementalelectricenerg

    ygeneration[MWh]

    J. Aerosp. Technol. Manag., So Jos dos Campos, Vol.4, No 3, pp. 341-353, Jul.-Sep., 2012 351

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    -

    -

    CONCLUSIONS

    T0

    -

    ACKNOWLEDGMENTS

    Table 3. I

    43.28

    32.02

    43.24

    53.00

    J. Aerosp. Technol. Manag., So Jos dos Campos, Vol.4, No 3, pp. 341-353, Jul.-Sep., 2012352

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    REFERENCES

    -

    -

    -

    a

    -

    a -

    a

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    a

    -

    a

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    a

    -

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    a

    J. Aerosp. Technol. Manag., So Jos dos Campos, Vol.4, No 3, pp. 341-353, Jul.-Sep., 2012 353