No Slide Title - The U.S.-China Oil & Gas Industry Forum Turbine and Combined Cycle BasicsGas...
Transcript of No Slide Title - The U.S.-China Oil & Gas Industry Forum Turbine and Combined Cycle BasicsGas...
GE Company ProprietaryConfidential Document
1
Harold E. MillerNPI/SE
June - July, 2002
MS9001FA Gas Turbine 燃气轮机
Technology Overview
Harold E. Miller
经理-新产品技术系统工程部
Mgr. – New Product Introduction Systems EngineeringHouston, TX
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Harold E. MillerNPI/SE
June - July, 2002
可提供的燃机产品 GT Technology Offerings500
满足不同的市场要求Meeting the Needs of a Dynamic MarketMeeting the Needs of a Dynamic Market
MW450
400工业界的全方位产品
Wide Range of Industry Solutions
H-Technology350
300250
F-Technology200150
Cogeneration & Industrial100 E-Technology500
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Harold E. MillerNPI/SE
June - July, 2002
先进的燃气轮机技术Advances in Gas Turbine Technology先进的燃气轮机技术Advances in Gas Turbine Technology
FA技术 -- FA Technology第一台F技术燃机1990年运行 First F Operates at Virginia Power - 19901159台已定货 1159 Operating On Order超过500万运行小时Over 5,000,000 Operating Hours
H技术 -- H System (TM)
60% Efficiency PlatformClosed Loop Steam CoolingSingle Crystal 1st Stage Nozzles and BucketsWorld's Most Efficient, Powerful Power Gen TechnologyStart-up 2002, Baglan Energy Park, Wales
Unprecedented Technology LeadershipUnprecedented Technology Leadership
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Harold E. MillerNPI/SE
June - July, 2002
F/FA 技术精要 Technology OverviewF/FA 技术精要 Technology Overview7FA/9FA
最有经验最可靠的高技术燃气轮机
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Harold E. MillerNPI/SE
June - July, 2002
Fossil Fuel Technology ChoicesFossil Fuel Technology Choices
Technology Power CyclePerformance
LevelPrimary
AdvantagesPrimary
DisadvantagesSteamTurbine
RankineCycle
30% - 40% · Custom Size· Solid Fuels· Dirty Fuels
· Low Efficiency· Rel. High $/KW· Slow Load Change
Packaged PowerPlantLow $/KWMed Fast StartsFast Load Delta
Clean FuelsAmbientDependence
Gas Turbine Brayton Cycle 30% to 40% · · · ·
· · ·
Combined · · 45% - 60% Highest EfficiencyBraytonTopping /RankineBottoming
Clean FuelsAmbientDependenceMed. Start Times
· · Cycle Med. $/KWLimited Fast LoadDelta
· ·
Diesel · · Diesel Cycle 40% - 50% High Maint.Rel. HighEfficiencyPackaged PowerPlantFast StartFast Construction
· Small Size (5MW)·
· ·
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Harold E. MillerNPI/SE
June - July, 2002
F燃机的运行启动统计图 Fleet Experience DemographicsF燃机的运行启动统计图 Fleet Experience Demographics
0
500
1,000
1,500
2,000
2,500
3,000
0 10,000 20,000 30,000 40,000 50,000 60,000 70,000
Fired Hours
Fire
d St
arts
6FA7F/FA9F/FA10 Hours/Start50 Hours/Start
周期性负荷Cycling Duty
调峰Peaking Duty
基荷Base Load
July 2001
11 Years of Operating History
Wide Range of Application Indicates RobustnessWide Range of Application Indicates Robustness
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Harold E. MillerNPI/SE
June - July, 2002
燃机要求 GT Demand
200
150
100
1950's
50
0
燃机
定货
GT
Ord
ers
(GW
)350
300
250
CC GW
SC GW
1960's 1970's 1980's 1990's
Huge Increase in Orders Huge Increase in Orders –– Combined Cycle Combined Cycle Becomes TechnologyBecomes Technology--ofof--ChoiceChoice
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Harold E. MillerNPI/SE
June - July, 2002
影响发电成本的因素Factors That Affect the Cost of Electricity
Fuel Composition
GT CostNox Abatement
ST, G BOP
OPERATIN
G& MAINTE
NANCE COST
S
Plant Price
Financing Cost
AvailabilityOutput Deterioration
Uncertainty - Availability
Fuel Price
Plant EfficiencyEfficiency Deterioration
Uncertainty - Efficiency
Daily Operation Costs
Uncertainty - Repair/Maintenance
Parts Replacement Cost
Parts Replacement Frequency
Outage Duration
Unplanned Outage Frequency
Planned Outage Frequency
PROJECTEDCOST OFELECTRICITY
FUEL COST
建厂成本
CA PITAL COST
7500 Hoursof Operation
per Year
9%Fuel
65%
26%
燃料成本
运行维护成本
计划的发电成本
Capital
O&M
Fuel is 65% of Cost of Power -- Plant Efficiency Drives Product Evolution
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Harold E. MillerNPI/SE
June - July, 2002
Gas Turbine and Combined Cycle BasicsGas Turbine and Combined Cycle Basics1250 322416 8 1pressure ratio:
Tem
pera
ture
(C)
200
400
600
800
1000
1200
1400
15
430
410
Expansion
Compression
Heat Addition(Combustion)
Exchange of Heat(to Environment or HRSG)
gas turbine
condenser
generator
generatorsteam turbines
condensatepump
heat recovery steam generator (HRSG)
Combined Cycle Combined Cycle –– GT & ST GT & ST
Gas Turbine Gas Turbine
Gas TurbineCompresses AirBurns Fuel (Many Types)Expands Gas – Mechanical WorkDrives GeneratorHot Exhaust Gas
Steam CycleTakes Hot Exhaust Gas from GTRaises, Superheats SteamExpands in Steam TurbineDrives Generator1/3 More Power, No Additional Fuel
GE Company ProprietaryConfidential Document
Harold E. MillerNPI/SE
June - July, 200272.27
Effect of Design Parameters on Efficiency and Output
56.00%
56.25%
56.50%
56.75%
57.00%
57.25%
57.50%
Specific W ork
Combined Cycle Efficiency
1260 C
1315 C
1370 C
20.5
17.5 15.0
Firing Tem p
Pressure Ratio
Line of Constant Pressure Ratio
Locus of Pressure Ratiosfor Low est Cost-of-
Electricity
Locus of Pressure Ratiosfor M axim um Com bined
Cycle Efficiency
Optimization for Combined Cycle: Pursue Firing Optimization for Combined Cycle: Pursue Firing Temperature; Moderate Pressure RatioTemperature; Moderate Pressure Ratio
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Harold E. MillerNPI/SE
June - July, 2002
技术和产品的发展Technology and Product Development
控制温度是透平设计的关键 - 比如:Controlling Temperature is Key to Turbine Design -for example . . .
Temperature Increase Effect15° C 0.45% Fuel Savings
but unfortunately . . .
15° C 2:1 Life Reduction
15° C 5.6% NOx Increase
DESIGN GOAL: Provide High Efficiency without Compromising Reliability, Operating Flexibility, Environmental Impact
or Maintenance Cost
DESIGN GOAL: Provide High Efficiency without Compromising Reliability, Operating Flexibility, Environmental Impact
or Maintenance Cost
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Harold E. MillerNPI/SE
June - July, 2002
Turbine Materials and Cooling TechnologyStage 1 Stage 2 Stage 3
• Film Plus Serpentine Cooling• Single-Crystal Rene N5 or
GTX111 Alloy• Thermal Barrier and Oxidation
Resistant Coatings
• STEM Drilled Radial Cooling Holes
• Directionally-Solidified GTD111 or GTD444 Alloy
• Oxidation Resistant Coating
• Cycle Pressure Ratio Selection Avoids Cooling
• Directionally Solidified GTD111 or GTD444
• Chromide Coating
Turbine Technology Turbine Technology –– High Gas Temperature, With Long LifeHigh Gas Temperature, With Long Life
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Harold E. MillerNPI/SE
June - July, 2002
Compressor Aero Combustion Turbine Aero
Analysis Tools Materials
“F”技术-结合飞机发动机技术“F” Technology Incorporates Aircraft Technology
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Harold E. MillerNPI/SE
June - July, 2002
叶片的进化 Evolution of Bucket Design
Original 9FFirst Stage
Bucket
CorrosionResistantCoating
Tip Cooling Holes
Current 9FAFirst Stage
BucketLe
adin
g Ed
ge F
ilm C
oolin
g H
oles
ThermalBarrier &CorrosionCoating New Technology
Next Step?
• Similar CoolingTechnology – more film
• Upgrade to SingleCrystal Material
• Improved TBC
• 3D Aero
Evolutionary Change within the same Proven Design PracticeEvolutionary Change within the same Proven Design Practice
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Harold E. MillerNPI/SE
June - July, 2002PG9311FA 到 PG9351FA 的进化PG9311FA to PG9351FA Evolution
9351FA Incorporates Features to Improve Performance, Reliability, & Availability
9351FA Incorporates Features to Improve Performance, Reliability, & Availability
Stage 1 Nozzle, Bucket, Shroud• Thermal Barrier Coating• Reduced Cooling Air
Double Walled Cone• Improved Sealing• Reduced Flow
Tapered StrutsRobust CompressorRotor
Honeycomb HPPS• Tie Bolt & Marriage Flange Cooling• 4-Segment Inner Barrel (roundness)
3300 Series Bentley Probes#1 & #2 Bearings
False Flanges (Roundness)• Compressor Case• Compr Discharge Case• Turbine Shell
Hot Gas PathImproved SealingStage 2 Bucket
• Scalloped Shroud• Mod Cooling
Hole Pattern
Monitoring/Diagnostics• Added Combustor Tuning Kit
<25 PPM DLN 2.0+ Combustor• 430mm Hast-X Liner• Class C TBC (8-12K CI)• Flexible Seals
Since PG9311FA, New Features have been Incorporated in PG9351FA
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Harold E. MillerNPI/SE
June - July, 2002效率对减少排放污染的影响Efficiency Contributes to Emissions Reduction
Technology Advances & Reduced Emissions
(Basis: Same Exhaust Concentrations - 25 ppmvd NOx; 9 ppmvd CO)
00.10.20.30.40.5
NOx CO
Emis
sion
s (k
g/M
Wh)
240250260270280290
CO2
Emis
sion
s (k
g/M
Wh)
E 1100C
FA 1300C
Firing Temp. Class
“F” Technology Enhances Environmental Performance
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Harold E. MillerNPI/SE
June - July, 2002干式低NOx (DLN)是如何工作的How Dry Low NOx (DLN) Works
Fuel-Rich and Fuel-Lean Operation Result in Lower Flame Temperature and Lower NOx Formation Rates.
Fuel-Lean Operation Results in Lower Smoke.
DLN Combustion Relies on Lean Operation
Flam
e Tem
pera
ture
(K)
0
50
100
150
200
250
300
350
400
Rate
of T
herm
al NO
x Pro
duct
ion
d NO
/ dt(
PPMV
/MS)
Temperature
NOx
CO
NO. 2 Oil, 10 AtmAir Preheat 590 K
richlean
2500
2000
1500
1000
500
00.25 0.5 0.75 1 1.25 1.5 1.75
Equivalence Ratio
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Harold E. MillerNPI/SE
June - July, 2002
Low NOx Combustion
Allowable burning rangefor lean-premixed com-bustor to stay withinflammable region and meet NOx goal
Rich flammability limit
Stochiometricfuel/air ratioNOx design goal
NO
x le
vel (
log
sca
le)
Air / Fuel RatioLean flammability limit
Range added withcatalytic combustion
Low NOx CombustionManagement of Reaction-Zone Fuel-Air Mixture -
NOx Control – Limited Combustion Operation Envelope72.10
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Harold E. MillerNPI/SE
June - July, 2002DLN燃烧室DLN Combustors
flame
cross-section
pre-mixing zone - no flamewhen operating properly
fuel enters fuel nozzles
to transitionpiece
end view
pre-mixed combinationof fuel and air burn fuel first enters air stream,
begins mixing
To Produce Stable Combustion at Low Fuel-Air Ratios, Fuel and Air are Mixed Together Upstream of the Flame Zone
Velocity in Pre-Mixing Chambers must be Uniformly High So Stable Combustion is Possible ONLY in Flame Zone
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Harold E. MillerNPI/SE
June - July, 2002
电厂概况 Power Plant OverviewShowcase Plants
Gennevilliers Power Plant First Unit Installed 1991
AES Medway, U.K. First Combined Cycle GE High Power Density Steam Turbine
Delesto 2, The Netherlands’ Largest Cogen Plant Relies on Stag 109FA
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Harold E. MillerNPI/SE
June - July, 2002
GE燃气轮机的“第一”GE Gas Turbine "Firsts"GE燃气轮机的“第一”GE Gas Turbine "Firsts"
1949 – Gas Turbine Power Generation Application,Oklahoma Gas & Electric1961 – Package Power Plant,South Carolina Electric & Gas1974 – Large Combined Cycle Plant,Salt River Project1984 – Integrated Gasification Combined Cycle Plant,Cool Water Project1988 – Introduction of Advanced F TechnologyGas Turbines1991 – LM6000 Aeroderivative Breaks 40% EfficiencyBarrier in Simple Cycle1995 – Introduction of H Technology Gas TurbinesWith 60% Efficiency Platform
Unmatched Leader in Gas Turbine Technology for Half a CenturyUnmatched Leader in Gas Turbine Technology for Half a Century