JP6183994B2 - トルクコンバータシステムを有するガスタービン圧縮機入口加圧 - Google Patents

トルクコンバータシステムを有するガスタービン圧縮機入口加圧 Download PDF

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Publication number
JP6183994B2
JP6183994B2 JP2013111429A JP2013111429A JP6183994B2 JP 6183994 B2 JP6183994 B2 JP 6183994B2 JP 2013111429 A JP2013111429 A JP 2013111429A JP 2013111429 A JP2013111429 A JP 2013111429A JP 6183994 B2 JP6183994 B2 JP 6183994B2
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JP
Japan
Prior art keywords
gas turbine
torque converter
flow rate
subsystem
fan
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
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JP2013111429A
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English (en)
Japanese (ja)
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JP2013249836A (ja
JP2013249836A5 (enExample
Inventor
サンジ・エカナヤケ
アルストン・アイ・シピオ
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General Electric Co
Original Assignee
General Electric Co
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Publication date
Application filed by General Electric Co filed Critical General Electric Co
Publication of JP2013249836A publication Critical patent/JP2013249836A/ja
Publication of JP2013249836A5 publication Critical patent/JP2013249836A5/ja
Application granted granted Critical
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Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
    • F02C6/04—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output
    • F02C6/10—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output supplying working fluid to a user, e.g. a chemical process, which returns working fluid to a turbine of the plant
    • F02C6/12—Turbochargers, i.e. plants for augmenting mechanical power output of internal-combustion piston engines by increase of charge pressure
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
    • F02C3/107—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor with two or more rotors connected by power transmission
    • F02C3/113—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor with two or more rotors connected by power transmission with variable power transmission between rotors
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
    • F02C6/04—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output
    • F02C6/06—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output providing compressed gas
    • F02C6/08—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output providing compressed gas the gas being bled from the gas-turbine compressor
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
    • F02C6/18—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use using the waste heat of gas-turbine plants outside the plants themselves, e.g. gas-turbine power heat plants
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/36—Power transmission arrangements between the different shafts of the gas turbine plant, or between the gas-turbine plant and the power user
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/16—Control of working fluid flow
    • F02C9/18—Control of working fluid flow by bleeding, bypassing or acting on variable working fluid interconnections between turbines or compressors or their stages
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00—Function
    • F05D2260/20—Heat transfer, e.g. cooling
    • F05D2260/211—Heat transfer, e.g. cooling by intercooling, e.g. during a compression cycle
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00—Function
    • F05D2260/40—Transmission of power
    • F05D2260/402—Transmission of power through friction drives
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00—Function
    • F05D2260/40—Transmission of power
    • F05D2260/406—Transmission of power through hydraulic systems
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E20/00—Combustion technologies with mitigation potential
    • Y02E20/14—Combined heat and power generation [CHP]
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E20/00—Combustion technologies with mitigation potential
    • Y02E20/16—Combined cycle power plant [CCPP], or combined cycle gas turbine [CCGT]

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Fluid Mechanics (AREA)
  • Physics & Mathematics (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • General Chemical & Material Sciences (AREA)
  • Control Of Turbines (AREA)
  • Control Of Positive-Displacement Air Blowers (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Supercharger (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)
JP2013111429A 2012-05-31 2013-05-28 トルクコンバータシステムを有するガスタービン圧縮機入口加圧 Expired - Fee Related JP6183994B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US13/485,273 2012-05-31
US13/485,273 US9239007B2 (en) 2012-05-31 2012-05-31 Gas turbine compressor inlet pressurization having a torque converter system

Publications (3)

Publication Number Publication Date
JP2013249836A JP2013249836A (ja) 2013-12-12
JP2013249836A5 JP2013249836A5 (enExample) 2016-07-14
JP6183994B2 true JP6183994B2 (ja) 2017-08-23

Family

ID=48538988

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2013111429A Expired - Fee Related JP6183994B2 (ja) 2012-05-31 2013-05-28 トルクコンバータシステムを有するガスタービン圧縮機入口加圧

Country Status (5)

Country Link
US (1) US9239007B2 (enExample)
EP (1) EP2669491A3 (enExample)
JP (1) JP6183994B2 (enExample)
CN (1) CN103452667B (enExample)
RU (1) RU2013125140A (enExample)

Families Citing this family (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20160376908A1 (en) * 2015-06-29 2016-12-29 General Electric Company Power generation system exhaust cooling
US9850794B2 (en) 2015-06-29 2017-12-26 General Electric Company Power generation system exhaust cooling
US9856768B2 (en) 2015-06-29 2018-01-02 General Electric Company Power generation system exhaust cooling
US10060316B2 (en) 2015-06-29 2018-08-28 General Electric Company Power generation system exhaust cooling
US9938874B2 (en) 2015-06-29 2018-04-10 General Electric Company Power generation system exhaust cooling
US9840953B2 (en) 2015-06-29 2017-12-12 General Electric Company Power generation system exhaust cooling
US10030558B2 (en) * 2015-06-29 2018-07-24 General Electric Company Power generation system exhaust cooling
US10215070B2 (en) * 2015-06-29 2019-02-26 General Electric Company Power generation system exhaust cooling
US9752502B2 (en) * 2015-06-29 2017-09-05 General Electric Company Power generation system exhaust cooling
US10077694B2 (en) * 2015-06-29 2018-09-18 General Electric Company Power generation system exhaust cooling
US9850818B2 (en) 2015-06-29 2017-12-26 General Electric Company Power generation system exhaust cooling
US9752503B2 (en) * 2015-06-29 2017-09-05 General Electric Company Power generation system exhaust cooling
US10087801B2 (en) 2015-06-29 2018-10-02 General Electric Company Power generation system exhaust cooling
GB201518929D0 (en) * 2015-10-27 2015-12-09 Rolls Royce Plc Gas turbine engine
US20170204786A1 (en) * 2016-01-15 2017-07-20 General Electric Company System and method for injecting tempering air for hot scr catalyst
GB2547674A (en) * 2016-02-25 2017-08-30 Rolls Royce Plc Gas turbine engine
US10316759B2 (en) 2016-05-31 2019-06-11 General Electric Company Power generation system exhaust cooling
KR101795947B1 (ko) * 2016-07-07 2017-11-09 한국서부발전 주식회사 가스 터빈의 토크 컨버터 제어 장치
EP3301279A1 (en) * 2016-09-28 2018-04-04 Siemens Aktiengesellschaft A rotating device for controlling a mass flow in a compressor of a gas turbine
GB201619960D0 (en) 2016-11-25 2017-01-11 Rolls Royce Plc Gas turbine engine
US11814187B2 (en) * 2020-12-21 2023-11-14 General Electric Company Hybrid electric propulsor equipped with a hydraulic coupling

Family Cites Families (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1029635A (fr) * 1950-11-14 1953-06-04 Snecma Perfectionnement aux turbo-réacteurs à deux flux
US3792586A (en) * 1973-01-22 1974-02-19 Avco Corp Bearing assembly systems
US3932058A (en) * 1974-06-07 1976-01-13 United Technologies Corporation Control system for variable pitch fan propulsor
US4651521A (en) * 1985-11-21 1987-03-24 Avco Corporation Convertible turbo-fan, turbo-shaft aircraft propulsion system
JPS64326A (en) * 1987-06-23 1989-01-05 Hitachi Ltd Nox abating type gas turbine plant
US5778675A (en) * 1997-06-20 1998-07-14 Electric Power Research Institute, Inc. Method of power generation and load management with hybrid mode of operation of a combustion turbine derivative power plant
US6230480B1 (en) 1998-08-31 2001-05-15 Rollins, Iii William Scott High power density combined cycle power plant
US7065953B1 (en) 1999-06-10 2006-06-27 Enhanced Turbine Output Holding Supercharging system for gas turbines
US6308512B1 (en) 1999-06-10 2001-10-30 Enhanced Turbine Output Holding, Llc Supercharging system for gas turbines
US6442942B1 (en) 1999-06-10 2002-09-03 Enhanced Turbine Output Holding, Llc Supercharging system for gas turbines
KR100874508B1 (ko) * 1999-06-10 2008-12-18 인핸스드 터빈 아웃풋 홀딩, 엘엘씨 개스 터빈용 과급 시스템
US6718771B1 (en) 1999-09-03 2004-04-13 Enhanced Turbine Output Holding Llc Gas turbine operative at high ambient temperatures
US6442941B1 (en) * 2000-09-11 2002-09-03 General Electric Company Compressor discharge bleed air circuit in gas turbine plants and related method
US6530224B1 (en) 2001-03-28 2003-03-11 General Electric Company Gas turbine compressor inlet pressurization system and method for power augmentation
US6880343B2 (en) 2001-12-06 2005-04-19 William L. Kopko Supercharged gas turbine with improved control
US20030182944A1 (en) * 2002-04-02 2003-10-02 Hoffman John S. Highly supercharged gas-turbine generating system
US7788898B2 (en) * 2006-12-06 2010-09-07 General Electric Company Variable coupling of turbofan engine spools via open differential gear set or simple planetary gear set for improved power extraction and engine operability, with torque coupling for added flexibility
US7791235B2 (en) * 2006-12-22 2010-09-07 General Electric Company Variable magnetic coupling of rotating machinery
US7950237B2 (en) * 2007-06-25 2011-05-31 United Technologies Corporation Managing spool bearing load using variable area flow nozzle
US8181442B2 (en) * 2008-05-05 2012-05-22 Pratt & Whitney Canada Corp. Gas turbine aircraft engine with power variability
US8291716B2 (en) * 2008-10-08 2012-10-23 The Invention Science Fund I Llc Hybrid propulsive engine including at least one independently rotatable turbine stator
US20100287944A1 (en) * 2009-05-13 2010-11-18 General Electric Company Availability improvements to heavy fuel fired gas turbines

Also Published As

Publication number Publication date
US20130318984A1 (en) 2013-12-05
JP2013249836A (ja) 2013-12-12
EP2669491A3 (en) 2018-04-04
CN103452667A (zh) 2013-12-18
CN103452667B (zh) 2016-09-07
US9239007B2 (en) 2016-01-19
RU2013125140A (ru) 2014-12-10
EP2669491A2 (en) 2013-12-04

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