CN101581252B - 控制用于抽吸空气以提供冷却空气的设定点的方法和系统 - Google Patents

控制用于抽吸空气以提供冷却空气的设定点的方法和系统 Download PDF

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Publication number
CN101581252B
CN101581252B CN2009101389251A CN200910138925A CN101581252B CN 101581252 B CN101581252 B CN 101581252B CN 2009101389251 A CN2009101389251 A CN 2009101389251A CN 200910138925 A CN200910138925 A CN 200910138925A CN 101581252 B CN101581252 B CN 101581252B
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China
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air
stage
pressure
compressor
compressed air
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Expired - Fee Related
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CN2009101389251A
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Chinese (zh)
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CN101581252A (zh
Inventor
P·蔡尔德斯
M·迪施
C·纽顿三世
D·W·小鲍尔
K·N·惠林
A·M·特鲁斯代尔
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General Electric Co
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General Electric Co
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C9/00Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/16Control of working fluid flow
    • F02C9/18Control of working fluid flow by bleeding, bypassing or acting on variable working fluid interconnections between turbines or compressors or their stages
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C6/00Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
    • F02C6/04Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output
    • F02C6/06Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output providing compressed gas
    • F02C6/08Gas-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
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, 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
    • F02C7/12Cooling of plants
    • F02C7/16Cooling of plants characterised by cooling medium
    • F02C7/18Cooling of plants characterised by cooling medium the medium being gaseous, e.g. air

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Control Of Positive-Displacement Air Blowers (AREA)
  • Control Of Turbines (AREA)
  • Jet Pumps And Other Pumps (AREA)
CN2009101389251A 2008-05-14 2009-05-12 控制用于抽吸空气以提供冷却空气的设定点的方法和系统 Expired - Fee Related CN101581252B (zh)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US12/120621 2008-05-14
US12/120,621 US8240153B2 (en) 2008-05-14 2008-05-14 Method and system for controlling a set point for extracting air from a compressor to provide turbine cooling air in a gas turbine
US12/120,621 2008-05-14

Publications (2)

Publication Number Publication Date
CN101581252A CN101581252A (zh) 2009-11-18
CN101581252B true CN101581252B (zh) 2013-12-04

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CN2009101389251A Expired - Fee Related CN101581252B (zh) 2008-05-14 2009-05-12 控制用于抽吸空气以提供冷却空气的设定点的方法和系统

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Country Link
US (1) US8240153B2 (https=)
EP (1) EP2119892A3 (https=)
JP (1) JP5039085B2 (https=)
CN (1) CN101581252B (https=)

Families Citing this family (126)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20030097872A1 (en) * 2001-11-29 2003-05-29 Granitz Charles Robert System for reducing oil consumption in gas turbine engines
WO2009120779A2 (en) 2008-03-28 2009-10-01 Exxonmobil Upstream Research Company Low emission power generation and hydrocarbon recovery systems and methods
CN104098070B (zh) 2008-03-28 2016-04-13 埃克森美孚上游研究公司 低排放发电和烃采收系统及方法
EP2146057B1 (en) * 2008-07-16 2011-09-07 Siemens Aktiengesellschaft Fluidically controlled valve for a gas turbine engine and for a combustor
SG195533A1 (en) 2008-10-14 2013-12-30 Exxonmobil Upstream Res Co Methods and systems for controlling the products of combustion
US8267122B2 (en) * 2009-06-30 2012-09-18 Ge Aviation Systems Llc Method and systems for bleed air supply
IT1395820B1 (it) * 2009-09-25 2012-10-26 Nuovo Pignone Spa Sistema di raffreddamento per una turbina a gas e relativo metodo di funzionamento
US8337139B2 (en) * 2009-11-10 2012-12-25 General Electric Company Method and system for reducing the impact on the performance of a turbomachine operating an extraction system
BR112012010294A2 (pt) 2009-11-12 2017-11-07 Exxonmobil Upstream Res Co sistema integrado, e, método para a recuperação de hidrocarboneto de baixa emissão com produção de energia
JP4958967B2 (ja) * 2009-12-15 2012-06-20 川崎重工業株式会社 換気構造を改良したガスタービンエンジン
US8303695B2 (en) * 2010-05-17 2012-11-06 General Electric Company Systems for compressing a gas
AU2011271635B2 (en) 2010-07-02 2015-10-08 Exxonmobil Upstream Research Company Stoichiometric combustion of enriched air with exhaust gas recirculation
TWI564475B (zh) 2010-07-02 2017-01-01 艾克頌美孚上游研究公司 低排放之三循環動力產生系統和方法
AU2011271634B2 (en) 2010-07-02 2016-01-28 Exxonmobil Upstream Research Company Stoichiometric combustion with exhaust gas recirculation and direct contact cooler
SG186158A1 (en) 2010-07-02 2013-01-30 Exxonmobil Upstream Res Co Low emission power generation systems and methods
GB201015029D0 (en) 2010-09-10 2010-10-20 Rolls Royce Plc Gas turbine engine
ITTO20100824A1 (it) * 2010-10-06 2012-04-07 Ansaldo Energia Spa Metodo di controllo per raffreddare uno stadio di turbina in una turbina a gas
US20120167587A1 (en) * 2010-12-30 2012-07-05 Robert Earl Clark Gas turbine engine with bleed air system
TWI593872B (zh) 2011-03-22 2017-08-01 艾克頌美孚上游研究公司 整合系統及產生動力之方法
TWI563166B (en) 2011-03-22 2016-12-21 Exxonmobil Upstream Res Co Integrated generation systems and methods for generating power
TWI563165B (en) 2011-03-22 2016-12-21 Exxonmobil Upstream Res Co Power generation system and method for generating power
TWI564474B (zh) 2011-03-22 2017-01-01 艾克頌美孚上游研究公司 於渦輪系統中控制化學計量燃燒的整合系統和使用彼之產生動力的方法
FR2979136B1 (fr) * 2011-08-16 2014-11-14 Snecma Dispositif d'activation d'une vanne passive d'ejecteur pour pressurisation d'une enceinte de turboreacteur d'aeronef
EP2562369B1 (de) 2011-08-22 2015-01-14 Alstom Technology Ltd Verfahren zum Betrieb einer Gasturbinenanlage sowie Gasturbinenanlage zur Durchführung des Verfahrens
US8973373B2 (en) * 2011-10-31 2015-03-10 General Electric Company Active clearance control system and method for gas turbine
GB201121428D0 (en) 2011-12-14 2012-01-25 Rolls Royce Plc Controller
GB201121426D0 (en) 2011-12-14 2012-01-25 Rolls Royce Plc Controller
US9260974B2 (en) * 2011-12-16 2016-02-16 General Electric Company System and method for active clearance control
WO2013095829A2 (en) 2011-12-20 2013-06-27 Exxonmobil Upstream Research Company Enhanced coal-bed methane production
US9169782B2 (en) * 2012-01-04 2015-10-27 General Electric Company Turbine to operate at part-load
US9322333B2 (en) * 2012-01-06 2016-04-26 General Electric Company System and method for determining a cooling flow parameter downstream from a gas turbine combustor
US9376931B2 (en) 2012-01-27 2016-06-28 General Electric Company Turbomachine passage cleaning system
US10724431B2 (en) * 2012-01-31 2020-07-28 Raytheon Technologies Corporation Buffer system that communicates buffer supply air to one or more portions of a gas turbine engine
US20130192251A1 (en) 2012-01-31 2013-08-01 Peter M. Munsell Buffer system that communicates buffer supply air to one or more portions of a gas turbine engine
US9353682B2 (en) 2012-04-12 2016-05-31 General Electric Company Methods, systems and apparatus relating to combustion turbine power plants with exhaust gas recirculation
US9784185B2 (en) 2012-04-26 2017-10-10 General Electric Company System and method for cooling a gas turbine with an exhaust gas provided by the gas turbine
CN104736817B (zh) * 2012-04-26 2017-10-24 通用电气公司 再循环用于燃气涡轮发动机中多个流动路径中的排气的系统和方法
US10273880B2 (en) 2012-04-26 2019-04-30 General Electric Company System and method of recirculating exhaust gas for use in a plurality of flow paths in a gas turbine engine
KR101933585B1 (ko) * 2012-07-25 2018-12-28 한화에어로스페이스 주식회사 가스 터빈 장치
US9003762B2 (en) * 2012-10-02 2015-04-14 General Electric Company Turbine exhaust plume mitigation system
US9708977B2 (en) 2012-12-28 2017-07-18 General Electric Company System and method for reheat in gas turbine with exhaust gas recirculation
US10215412B2 (en) 2012-11-02 2019-02-26 General Electric Company System and method for load control with diffusion combustion in a stoichiometric exhaust gas recirculation gas turbine system
US9599070B2 (en) 2012-11-02 2017-03-21 General Electric Company System and method for oxidant compression in a stoichiometric exhaust gas recirculation gas turbine system
US9631815B2 (en) 2012-12-28 2017-04-25 General Electric Company System and method for a turbine combustor
US9869279B2 (en) 2012-11-02 2018-01-16 General Electric Company System and method for a multi-wall turbine combustor
US10107495B2 (en) 2012-11-02 2018-10-23 General Electric Company Gas turbine combustor control system for stoichiometric combustion in the presence of a diluent
US10161312B2 (en) 2012-11-02 2018-12-25 General Electric Company System and method for diffusion combustion with fuel-diluent mixing in a stoichiometric exhaust gas recirculation gas turbine system
US9803865B2 (en) 2012-12-28 2017-10-31 General Electric Company System and method for a turbine combustor
US9611756B2 (en) 2012-11-02 2017-04-04 General Electric Company System and method for protecting components in a gas turbine engine with exhaust gas recirculation
US9574496B2 (en) 2012-12-28 2017-02-21 General Electric Company System and method for a turbine combustor
US9175783B2 (en) * 2012-11-16 2015-11-03 Ford Global Technologies, Llc Vacuum-actuated wastegate
US9562475B2 (en) * 2012-12-19 2017-02-07 Siemens Aktiengesellschaft Vane carrier temperature control system in a gas turbine engine
US10208677B2 (en) 2012-12-31 2019-02-19 General Electric Company Gas turbine load control system
US9581081B2 (en) 2013-01-13 2017-02-28 General Electric Company System and method for protecting components in a gas turbine engine with exhaust gas recirculation
ITMI20130089A1 (it) * 2013-01-23 2014-07-24 Ansaldo Energia Spa Impianto a turbina a gas per la produzione di energia elettrica e metodo per operare detto impianto
US9512759B2 (en) 2013-02-06 2016-12-06 General Electric Company System and method for catalyst heat utilization for gas turbine with exhaust gas recirculation
US9938861B2 (en) 2013-02-21 2018-04-10 Exxonmobil Upstream Research Company Fuel combusting method
TW201502356A (zh) 2013-02-21 2015-01-16 Exxonmobil Upstream Res Co 氣渦輪機排氣中氧之減少
WO2014133406A1 (en) 2013-02-28 2014-09-04 General Electric Company System and method for a turbine combustor
US9618261B2 (en) 2013-03-08 2017-04-11 Exxonmobil Upstream Research Company Power generation and LNG production
US20140250945A1 (en) 2013-03-08 2014-09-11 Richard A. Huntington Carbon Dioxide Recovery
TW201500635A (zh) 2013-03-08 2015-01-01 Exxonmobil Upstream Res Co 處理廢氣以供用於提高油回收
JP6143895B2 (ja) 2013-03-08 2017-06-07 エクソンモービル アップストリーム リサーチ カンパニー 発電及びメタンハイドレートからのメタン回収
US9482236B2 (en) 2013-03-13 2016-11-01 Rolls-Royce Corporation Modulated cooling flow scheduling for both SFC improvement and stall margin increase
US9447702B2 (en) 2013-06-21 2016-09-20 Sankar K. Mohan Cooling system and cooling method for use with closed loop systems
US9835089B2 (en) 2013-06-28 2017-12-05 General Electric Company System and method for a fuel nozzle
TWI654368B (zh) 2013-06-28 2019-03-21 美商艾克頌美孚上游研究公司 用於控制在廢氣再循環氣渦輪機系統中的廢氣流之系統、方法與媒體
US9631542B2 (en) 2013-06-28 2017-04-25 General Electric Company System and method for exhausting combustion gases from gas turbine engines
US9617914B2 (en) 2013-06-28 2017-04-11 General Electric Company Systems and methods for monitoring gas turbine systems having exhaust gas recirculation
US10227927B2 (en) 2013-07-17 2019-03-12 United Technologies Corporation Supply duct for cooling air from gas turbine compressor
US9587510B2 (en) 2013-07-30 2017-03-07 General Electric Company System and method for a gas turbine engine sensor
US9903588B2 (en) 2013-07-30 2018-02-27 General Electric Company System and method for barrier in passage of combustor of gas turbine engine with exhaust gas recirculation
US9951658B2 (en) 2013-07-31 2018-04-24 General Electric Company System and method for an oxidant heating system
EP2857656A1 (en) * 2013-10-01 2015-04-08 Alstom Technology Ltd Gas turbine with cooling air cooling system and method for operation of a gas turbine at low part load
US9752458B2 (en) 2013-12-04 2017-09-05 General Electric Company System and method for a gas turbine engine
US10030588B2 (en) 2013-12-04 2018-07-24 General Electric Company Gas turbine combustor diagnostic system and method
CN103697281A (zh) * 2013-12-27 2014-04-02 北京华清燃气轮机与煤气化联合循环工程技术有限公司 燃气轮机低压引气管路和高压引气管路之间的节流结构
US10227920B2 (en) 2014-01-15 2019-03-12 General Electric Company Gas turbine oxidant separation system
US9915200B2 (en) 2014-01-21 2018-03-13 General Electric Company System and method for controlling the combustion process in a gas turbine operating with exhaust gas recirculation
US9863267B2 (en) 2014-01-21 2018-01-09 General Electric Company System and method of control for a gas turbine engine
US10079564B2 (en) 2014-01-27 2018-09-18 General Electric Company System and method for a stoichiometric exhaust gas recirculation gas turbine system
US9580180B2 (en) 2014-03-07 2017-02-28 Honeywell International Inc. Low-pressure bleed air aircraft environmental control system
US9644542B2 (en) * 2014-05-12 2017-05-09 General Electric Company Turbine cooling system using an enhanced compressor air flow
US10047633B2 (en) 2014-05-16 2018-08-14 General Electric Company Bearing housing
EP3146184B1 (en) * 2014-05-21 2018-03-07 Siemens Energy, Inc. Method of providing a cooling flow from a compressor to a turbine in a gas turbine engine
EP2957746B1 (en) * 2014-06-17 2021-04-28 Raytheon Technologies Corporation High pressure turbine cooling
US9885290B2 (en) 2014-06-30 2018-02-06 General Electric Company Erosion suppression system and method in an exhaust gas recirculation gas turbine system
US10655542B2 (en) 2014-06-30 2020-05-19 General Electric Company Method and system for startup of gas turbine system drive trains with exhaust gas recirculation
US10060359B2 (en) 2014-06-30 2018-08-28 General Electric Company Method and system for combustion control for gas turbine system with exhaust gas recirculation
US10767562B2 (en) * 2014-12-10 2020-09-08 Pratt & Whitney Canada Corp. Modulated cooled P3 air for impeller
US9869247B2 (en) 2014-12-31 2018-01-16 General Electric Company Systems and methods of estimating a combustion equivalence ratio in a gas turbine with exhaust gas recirculation
US9819292B2 (en) 2014-12-31 2017-11-14 General Electric Company Systems and methods to respond to grid overfrequency events for a stoichiometric exhaust recirculation gas turbine
US10788212B2 (en) 2015-01-12 2020-09-29 General Electric Company System and method for an oxidant passageway in a gas turbine system with exhaust gas recirculation
US10094566B2 (en) 2015-02-04 2018-10-09 General Electric Company Systems and methods for high volumetric oxidant flow in gas turbine engine with exhaust gas recirculation
US10316746B2 (en) 2015-02-04 2019-06-11 General Electric Company Turbine system with exhaust gas recirculation, separation and extraction
US10253690B2 (en) 2015-02-04 2019-04-09 General Electric Company Turbine system with exhaust gas recirculation, separation and extraction
US10267270B2 (en) 2015-02-06 2019-04-23 General Electric Company Systems and methods for carbon black production with a gas turbine engine having exhaust gas recirculation
US10145269B2 (en) 2015-03-04 2018-12-04 General Electric Company System and method for cooling discharge flow
US10480792B2 (en) 2015-03-06 2019-11-19 General Electric Company Fuel staging in a gas turbine engine
US9863285B2 (en) 2015-03-19 2018-01-09 General Electric Company Power generation system having compressor creating excess gas flow for supplemental gas turbine system
US10024197B2 (en) 2015-03-19 2018-07-17 General Electric Company Power generation system having compressor creating excess air flow and turbo-expander using same
US20160273401A1 (en) * 2015-03-19 2016-09-22 General Electric Company Power generation system having compressor creating excess air flow and eductor for process air demand
JP5897180B2 (ja) * 2015-04-03 2016-03-30 三菱日立パワーシステムズ株式会社 ガスタービン
US9850819B2 (en) * 2015-04-24 2017-12-26 United Technologies Corporation Intercooled cooling air with dual pass heat exchanger
US10830148B2 (en) 2015-04-24 2020-11-10 Raytheon Technologies Corporation Intercooled cooling air with dual pass heat exchanger
KR101790146B1 (ko) * 2015-07-14 2017-10-25 두산중공업 주식회사 외부 케이싱으로 우회하는 냉각공기 공급유로가 마련된 냉각시스템을 포함하는 가스터빈.
US10502137B2 (en) * 2015-10-19 2019-12-10 General Electric Company Gas turbine with a valve cooling system
US10480342B2 (en) * 2016-01-19 2019-11-19 Rolls-Royce Corporation Gas turbine engine with health monitoring system
JP6801968B2 (ja) * 2016-02-15 2020-12-16 三菱パワー株式会社 ガスタービンの制御装置および制御方法、並びにガスタービン
GB2547674A (en) * 2016-02-25 2017-08-30 Rolls Royce Plc Gas turbine engine
CN105736080B (zh) * 2016-04-29 2017-12-05 华电郑州机械设计研究院有限公司 一种新型火电厂小汽轮机轴封抽汽系统
US20180057171A1 (en) * 2016-08-23 2018-03-01 Ge Aviation Systems, Llc Advanced method and aircraft for pre-cooling an environmental control system using a three wheel turbo-machine
US10731568B2 (en) 2016-11-23 2020-08-04 General Electric Company Systems and methods for reducing airflow imbalances in turbines
GB201619960D0 (en) 2016-11-25 2017-01-11 Rolls Royce Plc Gas turbine engine
US11739697B2 (en) 2017-05-22 2023-08-29 Raytheon Technologies Corporation Bleed flow safety system
US10473037B2 (en) 2017-05-22 2019-11-12 United Technologies Corporation Passively-driven bleed source switching
US12392289B2 (en) 2017-05-22 2025-08-19 Rtx Corporation Active bleed flow modulation
US11578668B2 (en) 2017-05-30 2023-02-14 Raytheon Technologies Corporation Gas turbine engine control based on characteristic of cooled air
FR3072414B1 (fr) * 2017-10-16 2019-11-01 Safran Aircraft Engines Dispositif et procede de refroidissement d'une turbine basse pression dans une turbomachine
DE102018125748A1 (de) * 2018-10-17 2020-04-23 Rolls-Royce Deutschland Ltd & Co Kg Ausfallerkennungssystem eines Kühlluftzufuhrsystems und Ausfallerkennungsverfahren für ein Kühlluftzufuhrsystemeiner Hochdruckturbine
US11047313B2 (en) * 2018-12-10 2021-06-29 Bell Helicopter Textron Inc. System and method for selectively modulating the flow of bleed air used for high pressure turbine stage cooling in a power turbine engine
FR3107088B1 (fr) * 2020-02-10 2022-12-09 Safran Dispositif et procédé d’arrêt de machine électrique pour une turbomachine
US11738833B1 (en) 2020-03-31 2023-08-29 Bombardier Recreational Products Inc. Fender system for a watercraft
US11828223B2 (en) * 2021-05-28 2023-11-28 Honeywell International Inc. Variable jet pump
US12234840B2 (en) 2022-06-07 2025-02-25 Honeywell International Inc. Jet pump system
US20250146441A1 (en) * 2023-11-02 2025-05-08 Rtx Corporation Turbine cooling air pressure boost system

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6550253B2 (en) * 2001-09-12 2003-04-22 General Electric Company Apparatus and methods for controlling flow in turbomachinery
EP1442203B1 (de) * 2001-11-02 2006-05-24 ALSTOM Technology Ltd Verfahren zur steuerung der kühlluftmassenströme einer gasturbogruppe
CN1991142A (zh) * 2005-12-19 2007-07-04 通用电气公司 涡轮机叶轮空间温度控制
US7328098B1 (en) * 2007-04-03 2008-02-05 United Technologies Corporation Determining bleed valve failures in gas turbine engines

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2002535122A (ja) 1999-01-20 2002-10-22 マイクロリス・コーポレーション 流れコントローラ
GB0224625D0 (en) * 2002-10-23 2002-12-04 Honeywell Normalair Garrett Method of balancing the supply of bleed air from a plurality of engines
US7536865B2 (en) * 2005-02-09 2009-05-26 Honeywell International Inc. Method and system for balancing bleed flows from gas turbine engines
US7536864B2 (en) 2005-12-07 2009-05-26 General Electric Company Variable motive nozzle ejector for use with turbine engines
US8136361B2 (en) 2006-05-04 2012-03-20 General Electric Company Methods and apparatus for assembling a low noise ejector motive nozzle

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6550253B2 (en) * 2001-09-12 2003-04-22 General Electric Company Apparatus and methods for controlling flow in turbomachinery
EP1442203B1 (de) * 2001-11-02 2006-05-24 ALSTOM Technology Ltd Verfahren zur steuerung der kühlluftmassenströme einer gasturbogruppe
CN1991142A (zh) * 2005-12-19 2007-07-04 通用电气公司 涡轮机叶轮空间温度控制
US7328098B1 (en) * 2007-04-03 2008-02-05 United Technologies Corporation Determining bleed valve failures in gas turbine engines

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Publication number Publication date
US20120117977A1 (en) 2012-05-17
US8240153B2 (en) 2012-08-14
CN101581252A (zh) 2009-11-18
EP2119892A2 (en) 2009-11-18
JP5039085B2 (ja) 2012-10-03
JP2009275702A (ja) 2009-11-26
EP2119892A3 (en) 2017-11-29

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