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GE Power Systems Technologies to Reduce GT Emissions Technologies to Reduce GT Emissions Rich Rapagnani Global Marketing & Development March 18, 2003 Rich Rapagnani Global Marketing & Development March 18, 2003

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Page 1: PDF 3.4 MB

GE Power Systems

Technologies toReduce GT EmissionsTechnologies toReduce GT Emissions

Rich RapagnaniGlobal Marketing & DevelopmentMarch 18, 2003

Rich RapagnaniGlobal Marketing & DevelopmentMarch 18, 2003

Page 2: PDF 3.4 MB

GE Power Systems

Technologies toReduce GT Emissions

Dry Low NOx Combustion Systems

Advanced DLN Systems

Catalytic Combustion

Technologies toReduce GT Emissions

Dry Low NOx Combustion Systems

Advanced DLN Systems

Catalytic Combustion

Page 3: PDF 3.4 MB

NO

x (T

ons)

/ M

W-Y

ear

DLN 2Advanced Cooling/Sealing

High Temperature Materials3D-Aero Premixers

Active Control

DLN 2Advanced Cooling/Sealing

High Temperature Materials3D-Aero Premixers

Active Control

• 3D Reactive Flow Modeling• Thermal Barrier Coatings• Active Radial Fuel Staging• Harsh Environment Sensors

Technology Enablers

1985 1990 20001995

Converting 33% of E Fleet= 25 Million Cars

Dry Low NOxLean Premix Combustion

Fuel Staging

Dry Low NOxLean Premix Combustion

Fuel Staging

25 PPM

Water InjectedWater Injected

42 PPM

9 PPMGE World Leader

1.5 Tons / MW Yr

10 Tons / MW Yr

GT Emissions Technology Advancements

Page 4: PDF 3.4 MB

• All Dependent on Temperature, Mixing & Time History• NOx Results From High Temperature (>2800F) times Time• CO Results From Insufficient Temperature (<1850) & Time

to Complete Reaction• UHC Similar to CO Except Lower Temperature and Times• Smoke Results From Local Fuel Rich Burning Zones ->

Carbon Particle Formation-> Quickly Moving to a Cooler Zone– Mainly a Problem With Distillate Fuel

• Low NOx, CO and UHC Over Wide Machine Operating Range isa Complex Development Challenge– As New Machine Temps and Pressures Have Increased,

Improved Solutions Have Been Required

NOx, CO, UHC, Smoke

Emissions As a Function Of Combustor Design

Page 5: PDF 3.4 MB

NOx

Stability & Premix Mode

Load Range

CO

DynamicsReliabilityComponentLife

Cannot Alter One Parameter Without Affecting Others

DLN Design Technology - A Four Sided Box

Page 6: PDF 3.4 MB

Thermal NOx • Formed from the oxidation of the free nitrogen in the combustion air or fuel

• Mainly a function of the stoichiometric adiabatic flame temperature of the fuel

• Sensitive to numerous combustion operational parameters

Organic NOx• Formed from the oxidation of organically bound nitrogen in the fuel, “fuel-bound

nitrogen (FBN)”

• Oxidation of FBN is very efficient : contribution important for fuels that contain significant amounts of FBN such as crude or residual oils.

• Sensitive to turbine firing temperature

• Water/Steam injection increases organic NOx for liquid fuels

Nitrogen Oxides (NOx) FormationTwo Types of NOx :

Page 7: PDF 3.4 MB

The following relationships exist between diffusion flame combustor operation conditions and thermal NOx production:

• NOx increases/decreases exponentially with increasing/decreasing flame temperature

• NOx increases exponentially with combustion inlet air temperature

• NOx increases approximately as the square root of the combustor inlet pressure

• NOx increases with increasing residence time in the flame zone

• NOx decreases exponentially with increasing water/steam injection or increasing specific humidity with increasing residence time in the flame zone

Thermal NOx Production

Page 8: PDF 3.4 MB

Ambient Pressure Effect on NOX

Relative Humidity Effect on NOX

Ambient Temperature Effect on NOX

GT25075

NOx versus Ambient Variations

Page 9: PDF 3.4 MB

Fundamentals of GT DLN Combustion Systems

• Fuel and Air Mixed Before Combustion (Premixed)

• Combustion Eq. Ratio Between 0.45 and 0.55for NOx, CO and Combustion Stability

• Premix Load Range Dependent on Compressor IGV Range (Airflow)

Bigger Range W/ Inlet Bleed Heat Option

• Excess Air (Dilution Air) Injected Late To Achieve Low CO (“E” Cycle and Earlier Machines)

• Highly Coordinated Control System Required to Maintain NOx Levels Over Wide Load Range and Ambient Conditions

Page 10: PDF 3.4 MB

F/A Ratio, Equivalence Ratio & NOx

Overall Eq Ratio below 0.5,all GT’s

FlameTempdegF

NOx ProductionRate

PPM/msec

Gas Fuel650 F Air Preheat

Page 11: PDF 3.4 MB

All Sizes 15 – 25

Total Large Frame GTs w/DLN: > 1200

345

Frame Size NOx (ppm)

7E/7EA/6B

7F/FA

9

9

Total 9 ppm Units:

No. of Units

360 + 29 in Const

306 + 201 in Const

896

GE Gas Turbine DLN Experience

Page 12: PDF 3.4 MB

Advanced DLN-1 Combustion System

• Being Developed for 7E/EA, 9E & 6B

• Multiple Operating Modes For Ignition thru Base Load

• Sub-9 ppm NOx on Gas Fuel

• Single Digit CO Emissions

• 42 ppm NOx on Distillate Fuel w/Water Injection

• Extendor Package Included

• Potential for Power Augmentation w/Steam Injection

Page 13: PDF 3.4 MB

0

0.5

1

1.5

2

2.5

0 10 20 30 40 50 60

ppm

LB/M

W-H

r

0

100

200

300

400

500

600

700

800

0 10 20 30 40 50 60

ppm

Tons

/Yr (

7EA

; 800

0 hr

s)

NOx Pounds per MW-Hr :E-Class Simple Cycle (~ 10,700 HR)

NOx Tons per Year : E-Class SimpleCycle (~ 10,700 HR), 7EA, 8000 hours

GT NOx Production: Lbs per MW-Hr; Tons per Year

Page 14: PDF 3.4 MB

0

0.05

0.1

0.15

0.2

0.25

0 10 20 30 40 50 60

ppm

LB/M

MB

tu

(1 ppm ~ .004 lb/Mbtu; 15 t/y)

NOx Production: Lbs per Million BTU (LHV) E-Class Simple Cycle (~ 10,700 HR)

Page 15: PDF 3.4 MB

MS 6B System Similar But Smaller

MS 7001 E/EA Combustion System Cross Section

Page 16: PDF 3.4 MB

MS 6B, 7E/EA & 9E EmissionsNatural Gas Fuel (load points w/IBH)

1009080706050403020100

350

300

250

200

150

100

50

0

ISO Ambient Conditions

NOx

CO

0 10 20 30 40 50 60 70 80 90 100

CO (p

pmvd

)

% Gas Turbine Load

NOx @

15%

O2 (

P Pm

v d)

Premix NOx levels down to <9 ppm based on liner tuning

Page 17: PDF 3.4 MB

Advanced DLN-1 Combustion System

• Retrofittable for Existing Units

• Short Outage Required

• No Plant Mods Necessary

• No Added O&M Costs

• No Performance Degradation

• Maintenance Cost Offset

• Potential to Eliminate Outages w/Extendor Package

Page 18: PDF 3.4 MB

GE Power Systems

GE/Catalytic GE10

Technology Overview

GE/Catalytic GE10

Technology Overview

Page 19: PDF 3.4 MB

Catalytic GE10 Market Assessment

• Power must be available at the point of use80% of US population resides in urban areas: Gas turbines difficult to site

in urban areas without ultra low NOx controls

• GE10 has the ability to site at the point of use, avoiding transmission and distribution constraintsSmall enough footprint to be sited in urban areasLarge enough to serve a significant portion of urban load

• GE10 can satisfy both regulatory and neighborhood air quality concerns in urban load centersNIMBY (Not In My Back Yard) effect can delay and stop projects

Program launched based upon the most stringent emissions requirements

Page 20: PDF 3.4 MB

Catalytic CombustionTraditional combustor

fuel

High temperature inflame produces NOx

ConventionalTem

pera

ture

NoNo--NOxNOx production vs. Cleanproduction vs. Clean--upup

Xonon module®®

fuel

fuel

Xonon module

Catalytic

®®

Page 21: PDF 3.4 MB

Compressor Discharge415C/779F

System Elements

PreburnerIncreases air temperature from CD to

catalyst ignition temperature (≈5/10% of total fuel)

Fuel Injector Gas fuel injection(≈90/95% of total fuel), with mixing resulting in F/A homogeneity 6% at catalyst inlet

Catalyst Heterogeneous combustion, Tinlet ≈ 842F(450°C),≈50% fuel burned, Texit ≈1652F (900°C)

Burn Out ZoneHomogeneous combustion, ≈50% fuel burned,Texit ≈ 2089F (1143°C), low NOx production

Byp

ass

Bypass air (up to 25%) compensates catalyst efficiency reduction with aging by reducing flow velocity in the catalyst and by increasing the F/A ratio in the catalyst + CO limitation during turndown

Turbine Inlet1090C/1994F

Temperature

Page 22: PDF 3.4 MB

Program Schedule

Kicked off2Q 2000

First CombustionSystem test

3Q 2001

From Power Gen market to Mech drive applicationFrom Power Gen market to Mech drive application

Componentsoptimization

1Q 2002

Catalyst test3Q 2002

Single shaft Engine test

1Q 2003

Dual shaft Engine test

1Q 2004

Mech Drivedevelopment

2- 4Q 2003

NPISix Sigma

tollgate process

Full scale full load combustion system

test rig

Page 23: PDF 3.4 MB

Target Performance• 3ppm NOx @ ISO full load

• 9ppm CO and UHC @ ISO full load

• Dry System

• Combustion System pressure drop < 5.0% (for comparable DLE+SCR performance)

• Hot Part Life: 24,000 hrs (same as DLE)

• Combustion Inspection: 8,000 hrs (same as DLE)

• Retrofitability on current GE10

Addressed MarketSingle shaft for Power Generation applications, Mechanical drive is following

Fuel composition limited as following:

Component Maximum, vol% Minimum, vol%Methane 100 90Ethane 10 0Propane 1.8 0Butanes+ 0.6 0

Fuel hydrocarbon components limits (inert-free basis) without adptive controls

Note: Fuels that do not meet this specification may still be acceptable prior GE&CESI evaluation

Page 24: PDF 3.4 MB

GE Technology Integration

GE Medical Systems GE Nuclear

Energy Products

Technologies to Continually Improve Reliability & Cost of ElectrTechnologies to Continually Improve Reliability & Cost of Electricityicity

GE Aircraft Engines

Corporate Research & Development

Energy Services

Investment & Acquisitions $450MM

Page 25: PDF 3.4 MB

GE Power Systems

Technologies toReduce GT Emissions

Dry Low NOx Combustion Systems

Advanced DLN Systems

Catalytic Combustion

Technologies toReduce GT Emissions

Dry Low NOx Combustion Systems

Advanced DLN Systems

Catalytic Combustion

Page 26: PDF 3.4 MB