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IGTI 2011 IGTI 2011 June 8 June 8 th th , 2011 , 2011
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Page 1: IGTI 2011 June 8th, 2011 - Turbine Inlet Cooling Associationturbineinletcooling.org/resources/papers/CTIC_WetCompression... · Compressor Efficiency ImprovementCompressor Efficiency

IGTI 2011IGTI 2011

June 8June 8thth, 2011, 2011

Page 2: IGTI 2011 June 8th, 2011 - Turbine Inlet Cooling Associationturbineinletcooling.org/resources/papers/CTIC_WetCompression... · Compressor Efficiency ImprovementCompressor Efficiency

What it Is What it Is NotWET COMPRESSION

What it Is What it Is Not8 to 25% (~12% 7EA) Power Augmentation at any wet bulb temperature above 45 °F

Is not traditional inlet air cooling, like a fogger or a chiller

p

“Complimentary Technology” -used in series w/ inlet cooling & other GT upgrades

Is not a system that limits your other options

upgrades

Technology demonstrated for more than 10 years and >>300,000 fleet hours

Is not a new, untested concept

Applied to a wide range of GT’s aero Is not a limited ApplicationApplied to a wide range of GT’s, aero and frame, for five GT OEMs

Is not a limited Application

Small droplets size, remain entrained in inlet air flow reducing impingement

Is not damaging to compressorinlet air flow, reducing impingement

GT OEMs have been Caldwell’s repeat customers for Wet Compression

Page 3: IGTI 2011 June 8th, 2011 - Turbine Inlet Cooling Associationturbineinletcooling.org/resources/papers/CTIC_WetCompression... · Compressor Efficiency ImprovementCompressor Efficiency

Four-fold effect:Four-fold effect:• Water Inter-cools the CT compressor:

– COMPRESSOR EFFICIENCY DRAMATICALLY IMPROVED– Mass flow enhancement (minor, but measurable)– Lower CDT allows more fuel to be fired

(at constant firing temperature)

• Adiabatic Cooling of inlet air:Cools air to very near WBT @ bell mouth– Cools air to very near WBT @ bell-mouth

– Usually operated with an existing fogger or evap cooler upstream

• Overall net impact ~ 9 - 13 MW on a GE 7EA, simple cycle

Page 4: IGTI 2011 June 8th, 2011 - Turbine Inlet Cooling Associationturbineinletcooling.org/resources/papers/CTIC_WetCompression... · Compressor Efficiency ImprovementCompressor Efficiency

Compressor Efficiency ImprovementCompressor Efficiency Improvement10 100

GE 7EA

789

e 708090

W

GE 7EAcompressor shaft parasitic powerrequirements before and after

standard pressure ratio = 12 70

11 MW

567

per s

tag

506070

ativ

e M

Wstandard pressure ratio 12.70

34

MW

p

3040

cum

ula

012

01020

01 2 3 4 5 6 7 8 9 1011121314151617

stage

0

Page 5: IGTI 2011 June 8th, 2011 - Turbine Inlet Cooling Associationturbineinletcooling.org/resources/papers/CTIC_WetCompression... · Compressor Efficiency ImprovementCompressor Efficiency

T S Diagram of Compressor & CombustorT-S Diagram of Compressor & Combustor

Heat (2 to 3) 3

T 2A

2

( )Constant

firing temp. 2S

Change in CDT (-122 F) is the equivalent of replacing

“electric heating of air”2W

gvs. “fuel heating of air”

Compress (1 to 2)

Blue colored line is new Wet Compression path

S

1(1 to 2) p p

Page 6: IGTI 2011 June 8th, 2011 - Turbine Inlet Cooling Associationturbineinletcooling.org/resources/papers/CTIC_WetCompression... · Compressor Efficiency ImprovementCompressor Efficiency

Wet Compression Effects on StageWet Compression Effects on Stage Operating Pressure

sure

Dry

WetIntercooling reduces front end compressor work

Pres

s

Water and increased HP rotor speed increase mass flow and CDP

Axial Position

Turbine pressure increased in all stages

Compressor HP LP GEN

Two Stage Turbine

Page 7: IGTI 2011 June 8th, 2011 - Turbine Inlet Cooling Associationturbineinletcooling.org/resources/papers/CTIC_WetCompression... · Compressor Efficiency ImprovementCompressor Efficiency

WC Cycle Performance EffectsWC Cycle Performance EffectsDry, Base Load Operation 2560

AirFuel

Estimated CyclePerformance Effects:

Gen Comp TurbExhaust

CT Power 11.8%CT Heat Rate -1.0%CT Fuel Flow 10.7%

AirFuel

Wet Compression - 1% Overspray

+8%

CT Exhaust Flow 0.0%CT Exhaust Energy ?%

St P d ti 2 0%

Gen Comp Turb

Air

Exhaust

1% H2OSteam Production 2.0%STG Power 2.0%

Duct Burner Flow ?%Gen Comp Turb

Pwr +9%Flow +1%Enthalpy +1%Energy + 2%

Duct Burner Flow ?%

Page 8: IGTI 2011 June 8th, 2011 - Turbine Inlet Cooling Associationturbineinletcooling.org/resources/papers/CTIC_WetCompression... · Compressor Efficiency ImprovementCompressor Efficiency

WC NOx Emission EffectsWC NOx Emission EffectsDry Base Load Operation Estimated Emission Effects:

• CT NOx reduced 10 to 20 percent in conventional diffusion flame combustion systems on a dry volumetric PPM basis

Air

Exhaust

Fuel

corrected to 15% oxygen• Mass emission rates are reduced

by approximately half as much since oxygen content is reduced

Gen Comp TurbExhaust

NOx 42 ppmvdNOx 74 lb/hrDry O2 14.2%

Wet Compression - 1% Overspray

AirFuel

1% H O

+8%

since oxygen content is reduced with wet compression.

• Dry low NOx emissions levels are affected by combustion

t d i d

Dry O2 14.2%

Gen Comp TurbExhaust

1% H2O

Flow +1%

system dynamics and may require tuning to hold NOx PPM constant or slightly increase emission rates. Mass emissions will increase due to the oxygenPwr +9% NOx 38 ppmvd

NOx 71 lb/hrDry O2 13.8%

will increase due to the oxygen correction.

Page 9: IGTI 2011 June 8th, 2011 - Turbine Inlet Cooling Associationturbineinletcooling.org/resources/papers/CTIC_WetCompression... · Compressor Efficiency ImprovementCompressor Efficiency

Environmental Benefits: 7EAEnvironmental Benefits: 7EA

• Improves SC HR ~4%. Emissions Before with WC delta207EA, duct-fired, pre-fit w/ evap cooling

• Reduces NOx PPM– on conventional diffusion

(WI / SI) burners; and NOx as NO2 65 73 7.4 CO 110 110 0.0

Gas Turbine Emissions (total for 2 units) - burning gas fuel

– requires integration with dry-low NOx burners

UHC as CH4 19 20 0.6

NOx as NO2 33 37 3.6 CO 18 18 0 0

Duct Burner Emissions (total for 2 units) - burning gas fuel

CO 18 18 0.0 UHC as CH4 11 11 0.4

Plant Total EmissionsNOx as NO2 20 22 2.2 NOx as NO2 2.2

CO 128 128 0.0 NH3 27 27 0.8

• Overall NOx usually limited by SCR system• Increase in “Criteria Pollutants” << 40 TPH trigger for NSR

Page 10: IGTI 2011 June 8th, 2011 - Turbine Inlet Cooling Associationturbineinletcooling.org/resources/papers/CTIC_WetCompression... · Compressor Efficiency ImprovementCompressor Efficiency

Wet Compression Nozzle LocationWet Compression Nozzle Location

existing fogging nozzle location or evap cooler system

silencing panels

Wet Compression SystemNozzle Rack Location

Page 11: IGTI 2011 June 8th, 2011 - Turbine Inlet Cooling Associationturbineinletcooling.org/resources/papers/CTIC_WetCompression... · Compressor Efficiency ImprovementCompressor Efficiency

Array Manifold 7EA

Page 12: IGTI 2011 June 8th, 2011 - Turbine Inlet Cooling Associationturbineinletcooling.org/resources/papers/CTIC_WetCompression... · Compressor Efficiency ImprovementCompressor Efficiency

Manifold Installation

Page 13: IGTI 2011 June 8th, 2011 - Turbine Inlet Cooling Associationturbineinletcooling.org/resources/papers/CTIC_WetCompression... · Compressor Efficiency ImprovementCompressor Efficiency

WCT Nozzle Spray Pattern

Page 14: IGTI 2011 June 8th, 2011 - Turbine Inlet Cooling Associationturbineinletcooling.org/resources/papers/CTIC_WetCompression... · Compressor Efficiency ImprovementCompressor Efficiency

Cardinal Cogen - GE Frame 6B

No Wet Compression With Wet Compression

Ambient dry bulb 58°F 59°F

Ambient wet bulb 52°F 52°F

Compressor Inlet Air Temp 57.9°F 52°F

Compressor Discharge Pressure 153 psig 158 psigCompressor Discharge Pressure 153 psig 158 psig

Compressor Discharge Temp 664°F 614°F

Gas Flow 6.1 lb/sec 6.6 lb/sec

Theoretical Firing Temp 2023 °F 2023 °F

Turbine Exhaust Temp 1029 °F 1017 °F

Turbine Power Output 35 3 MW 38 6 MWTurbine Power Output 35.3 MW 38.6 MW

Page 15: IGTI 2011 June 8th, 2011 - Turbine Inlet Cooling Associationturbineinletcooling.org/resources/papers/CTIC_WetCompression... · Compressor Efficiency ImprovementCompressor Efficiency

Duct Work Treatment 6B

Page 16: IGTI 2011 June 8th, 2011 - Turbine Inlet Cooling Associationturbineinletcooling.org/resources/papers/CTIC_WetCompression... · Compressor Efficiency ImprovementCompressor Efficiency

Wet Compression Arrays 6B

Page 17: IGTI 2011 June 8th, 2011 - Turbine Inlet Cooling Associationturbineinletcooling.org/resources/papers/CTIC_WetCompression... · Compressor Efficiency ImprovementCompressor Efficiency

WCT Skid On Test

Page 18: IGTI 2011 June 8th, 2011 - Turbine Inlet Cooling Associationturbineinletcooling.org/resources/papers/CTIC_WetCompression... · Compressor Efficiency ImprovementCompressor Efficiency

Rolls Royce ISI SKID

Page 19: IGTI 2011 June 8th, 2011 - Turbine Inlet Cooling Associationturbineinletcooling.org/resources/papers/CTIC_WetCompression... · Compressor Efficiency ImprovementCompressor Efficiency

Table 1: Performance Comparison of Various Combustion Turbines

Combustion Turbine

SiemensW501FC

SiemensV84.2

GE LM2500

PE

GE Frame 6B

SWPCW501D5A

Alstom GT-24

GE Frame7EA

PE

Overspray, % 1.3 1.0 2 1 2 1.2 1.5%

CompressorDischargeTemperature

90 50 Data notavailable

50 100 48 90

TemperatureReduction, °F

Fuel FlowIncrease, %

N.D. N.D. 4 8.2 13.2 5.5 11.5%

Change in Base No Change No Change No Change No Change No Change No Change No ChangeLoad FiringTemperature, ºF

CT Power Increase

17 5.2 1.6 3.3 15 15.5 9 Increase, MW

Steam Turbine Power

Increase, MW

Simple Cycle

Simple Cycle

-.5 0.3 (est.) 2 (est.) 1.8(est.) Simple Cycle

CT H t R t N D 2 0 1 2 2 1 05%CT Heat Rate Improvement, %

N.D. 2 0 1 2 2 1.05%

NOx Info -10% N.D. -14% DLN DLN No Change -54%

Page 20: IGTI 2011 June 8th, 2011 - Turbine Inlet Cooling Associationturbineinletcooling.org/resources/papers/CTIC_WetCompression... · Compressor Efficiency ImprovementCompressor Efficiency

Wet Compression ExperienceWet Compression Experience

• Patented Wet Compression Technology• Patented Wet Compression Technology– licensed from Dow Chemical– 10 years of continuous improvement

• > 300,000 hours of operating experience on more than 60 CTs

Engine 1st Installed Engine 1st Installed Engine 1st InstalledW501A 1995 GE 6B 2002 GT 24 2002

W501D5A 1997 LM2500 2003 GT 26 2004W501D5 1999 GE 7EA 2008 RR T60 2009

V94 2001V94 2001W501F 2004

8 units andgrowing

Page 21: IGTI 2011 June 8th, 2011 - Turbine Inlet Cooling Associationturbineinletcooling.org/resources/papers/CTIC_WetCompression... · Compressor Efficiency ImprovementCompressor Efficiency

Wet Compression SummaryWet Compression Summary

• Significant efficiency improvement• Significant efficiency improvement• << 1 year payback• Ambient Independent: consistent predictable power• Ambient Independent: consistent, predictable power

augmentation• Short outage, low-impact installation• > 300,000 hours of operating experience• Safe and Reliable – no impact to Reliability, Availability,

Maintainability (RAM)

Page 22: IGTI 2011 June 8th, 2011 - Turbine Inlet Cooling Associationturbineinletcooling.org/resources/papers/CTIC_WetCompression... · Compressor Efficiency ImprovementCompressor Efficiency

Wet Compression CustomersWet Compression Customers

Projects installed in: USA South America AfricaProjects installed in: USA, South America, Africa, Europe, Asia, Australia


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