Transcript
Page 1: Analysis of Gas Turbine Performance with Inlet Air Cooling … ·  · 2012-10-06Analysis of Gas Turbine Performance with Inlet Air Cooling Techniques Applied to Brazilian Sites Ana

LIST OF SYMBOLS AND NOMENCLATURE

AbbreviationsISO International Organization for StandardizationTIT Turbine Inlet TemperatureTIC Turbine Inlet Cooling

Symbols UnitsCp [kJ/kg°C]

COP [-]

LHV [kJ/kg]h [kJ/kg]HR Heat ratemP [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 SitesAna Paula Santos1, Cláudia R. Andrade2,*1

2

Abstract: F r r ph r wh r p w r m h h r pr r r hw rm m h rb r h p r r p r -

r h p w r p b h rb r h h r m w r hmpr r mp r r r rb h p r p r - m - wmb m h h p m r r pr p r h mp r r h r hr r h h r r m w r h m r r C h rb

p w r p h r m h r b r r mpr r r mp r r Th r rw b m rr b r Th r m - m h p r

p r r m h p r w r r h rb r mp r rTh m mp w w h r m h mpr b rp h m hh m m w hr h h h r h r m h r m h r h

pr h rm m rb p r rm rr h r p w rp h rm r r mp r r r h m Th r b

w h h m r mp r w h h h w h h r m -C Th hhr h r mp mp m r r mp r r

r h m h rb w r r m h r w rmp r b w h r m m h b rp h w h h b rp h r pr h

h h r m r r w h w r r O h h r h p r rr h w r b w h m p

Keywords: rb T rb T C p r Ch r b rp

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

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[-][-][-][-][kgwater/kgair]

Subscripts0

aaCMCCL Cooling load

gin InputN Net

TurbineT Totalh

w water

INTRODUCTION

-

-

-

Jaber a

-

-

and

J. Aerosp. Technol. Manag., São José 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

Combus onChamber

P P0 03=

P04

P r P04 03$=

-

T04

PP

TT

T1c

0403

03

04

1

03h= - +

cc-c m= G

W m C T T,C a pa avg 04 03$= -o o ^ hma Cpa a g

-P05

P P PCombustor05 04 D= -

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

LHV

/m

Q LHVf

Combustor

in

h=o

o

C mb r

/T T T

P P1

1t06 05 04

05 06

1

$h= - -cc-c m= G

P

J. Aerosp. Technol. Manag., São José 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 ^ hm T

m m mT a f= +o o o

and Cpg a g

W W WN T C= -o o o

SFCW

m3600

N

f$= o

o

HR SFC LHV$=

SFC LHV3600

th $h =

INLET AIR COOLING SYSTEMS

-

Net.

W

01

02

006

050403

Comp or

Coo ingy m

Evaporative cooling

Coo

ling

med

ia

Air cooledAmbient Air

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

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

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

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m a 02 03

-

Q m C T T,CL a pa avg 02 03$ $= -o o ^ hm a Cpa a g

Absorption and mechanical chiller systems

-tion cooling.

Ambient air

Chilled water

Air cooled togas 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-

-

WCOPQ

MC

CL=o

o

-

W W W WN t C MC= - -o o o o

J. Aerosp. Technol. Manag., São José 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 ChillingProcess

EnthalpyBtu Per Pound

of Dry Air

EvaporativeCooling Process

SpecificHumidity

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 KHeat ratePower output

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

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-

-

4 8 12 16 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

Pow

erou

tput

[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

31.0Th

e rm

alef

ficie

ncy

[%]

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 KAbsorption chiller: = 18% and 60%Evaporative cooling: = 0.90 and = 18%Evaporative cooling: = 0.90 and = 60%

J. Aerosp. Technol. Manag., São José 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

Pow

er o

utpu

t[M

W]

TIT = 1385 KAbsorption 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

Ther

mal

effic

ienc

y[%

]

TIT = 1385 KAbsorption 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

Pow

erou

tput

[MW

]

TIT = 1385 K= 60 %

COP = 7.0COP = 4.5COP = 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

Pow

erou

tput

[MW

]

TIT = 1385 K= 60 %

COP = 7.0COP = 4.5COP = 2.0

J. Aerosp. Technol. Manag., São José 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

Pow

erou

tput

[MW

]

TIT = 1385 KCOP = 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

Mas

sflo

ww

ate r

[kg/

s]

ma = 141.16 kg/sTET = 1385 °C

= 18%Evaporative cooling: = 0.90Absorption chillerMechanical 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

Cool

ing

load

[MW

]

TIT = 1385 K= 18 %

Mechanical chiller: COP = 4.5Absorption chillerEvaporative cooling: = 0.90

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

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-

-

Table 2.

Site25.0

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

Pow

erou

tput

[MW

]

TIT = 1385 K= 18%

Evaporative cooling:Absorption chillerCompression chiller: COP = 4.5Base 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

The r

mal

e ffic

ienc

y[%

]

TIT = 1385 K= 18 %

Evaporative cooling:Absorption chillerCompression chiller: COP = 4.5Base-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

Am

bien

t tem

pera

ture

[°C

]

70

71

72

73

74

75

76

77

78

79

80

81

DECNOVOCTSEPAUGJULJUNMAYAPRMARFEBJAN

Rel

ativ

e hu

mid

ity [%

]

Months

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

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Op ra r Na i na Si ma ri

-

-

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

Am

bien

t tem

pera

ture

[°C

]

DECNOVOCTSEPAUGJULJUNMAYAPRMARFEBJAN

Months

25

30

35

40

45

50

55

60

65

70

75

80

85

Rel

ativ

e hu

mid

ity [%

]

Evaporative cooling: = 0.90 Absorption chiller Mechanical chiller: COP = 4.5

DECOUTSEPAUGJUL NOV

Months

0

400

800

1,200

1,600

2,000

2,400

2,800

3,200

3,600

4,000

4,400

Incr

emen

tal e

lect

ric e

nerg

y ge

nera

tion

[MW

h]

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

Incr

emen

tal e

lect

ric e

nerg

y ge

nera

tion

[MW

h]

J. Aerosp. Technol. Manag., São José 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

32.0243.2453.00

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

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REFERENCES

-

-

-

a-

a -

a

-

a-

a

-

a

-

-

a

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


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