JP4230356B2 - ガスタービンエンジン制御システムに加速計画を適用するための方法および装置 - Google Patents

ガスタービンエンジン制御システムに加速計画を適用するための方法および装置 Download PDF

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JP4230356B2
JP4230356B2 JP2003545953A JP2003545953A JP4230356B2 JP 4230356 B2 JP4230356 B2 JP 4230356B2 JP 2003545953 A JP2003545953 A JP 2003545953A JP 2003545953 A JP2003545953 A JP 2003545953A JP 4230356 B2 JP4230356 B2 JP 4230356B2
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Prior art keywords
engine
temperature
plan
surge
pressure compressor
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Expired - Fee Related
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JP2003545953A
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Japanese (ja)
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JP2005509794A (ja
JP2005509794A5 (enExample
Inventor
メイスナー・リチャード
Original Assignee
グッドリッチ・ポンプ・アンド・エンジン・コントロール・システムズ・インコーポレーテッド
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Classifications

    • 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
    • F02C9/26Control of fuel supply
    • F02C9/28Regulating systems responsive to plant or ambient parameters, e.g. temperature, pressure, rotor speed
    • 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
    • F02C9/48Control of fuel supply conjointly with another control of the plant
    • F02C9/50Control of fuel supply conjointly with another control of the plant with control of working fluid flow
    • F02C9/52Control of fuel supply conjointly with another control of the plant with control of working fluid flow by bleeding or by-passing the working fluid
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2270/00Control
    • F05D2270/01Purpose of the control system
    • F05D2270/10Purpose of the control system to cope with, or avoid, compressor flow instabilities
    • F05D2270/101Compressor surge or stall

Landscapes

  • 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)
JP2003545953A 2001-11-15 2002-11-15 ガスタービンエンジン制御システムに加速計画を適用するための方法および装置 Expired - Fee Related JP4230356B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US33538701P 2001-11-15 2001-11-15
PCT/US2002/036769 WO2003044353A1 (en) 2001-11-15 2002-11-15 Method and apparatus for adaptive acceleration schedules in gas turbine engine control systems

Publications (3)

Publication Number Publication Date
JP2005509794A JP2005509794A (ja) 2005-04-14
JP2005509794A5 JP2005509794A5 (enExample) 2006-01-05
JP4230356B2 true JP4230356B2 (ja) 2009-02-25

Family

ID=23311554

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2003545953A Expired - Fee Related JP4230356B2 (ja) 2001-11-15 2002-11-15 ガスタービンエンジン制御システムに加速計画を適用するための方法および装置

Country Status (5)

Country Link
US (1) US6820429B2 (enExample)
EP (1) EP1444428B1 (enExample)
JP (1) JP4230356B2 (enExample)
DE (1) DE60230791D1 (enExample)
WO (1) WO2003044353A1 (enExample)

Families Citing this family (34)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6935120B2 (en) * 2002-05-09 2005-08-30 General Electric Company Approach to extending life of gas turbine engine
US6823675B2 (en) * 2002-11-13 2004-11-30 General Electric Company Adaptive model-based control systems and methods for controlling a gas turbine
US7487029B2 (en) * 2004-05-21 2009-02-03 Pratt & Whitney Canada Method of monitoring gas turbine engine operation
US7377114B1 (en) * 2004-06-02 2008-05-27 Kevin P Pearce Turbine engine pulsed fuel injection utilizing stagger injector operation
US7762084B2 (en) * 2004-11-12 2010-07-27 Rolls-Royce Canada, Ltd. System and method for controlling the working line position in a gas turbine engine compressor
US9273614B2 (en) * 2005-09-12 2016-03-01 Industrial Turbine Company (Uk) Limited Determination of a signal indicative of shaft power
US20070214795A1 (en) * 2006-03-15 2007-09-20 Paul Cooker Continuous real time EGT margin control
US7762078B2 (en) * 2006-09-13 2010-07-27 Aerojet-General Corporation Nozzle with temperature-responsive throat diameter
GB0716329D0 (en) 2007-08-21 2007-10-03 Compair Uk Ltd Improvements in compressors control
GB0813413D0 (en) 2008-07-23 2008-08-27 Rolls Royce Plc A compressor variable stator vane arrangement
US8277208B2 (en) 2009-06-11 2012-10-02 Goodrich Pump & Engine Control Systems, Inc. Split discharge vane pump and fluid metering system therefor
GB0915616D0 (en) * 2009-09-08 2009-10-07 Rolls Royce Plc Surge margin regulation
US8899488B2 (en) 2011-05-31 2014-12-02 United Technologies Corporation RFID tag system
FR2976622B1 (fr) * 2011-06-16 2015-05-01 Turbomeca Architecture double corps de turbomoteur avec compresseur haute pression lie a la turbine basse pression
US10436208B2 (en) 2011-06-27 2019-10-08 Energy Control Technologies, Inc. Surge estimator
CA2804462C (en) 2012-07-12 2021-05-25 Pratt & Whitney Canada Corp. Aircraft power outtake management
US8720258B2 (en) * 2012-09-28 2014-05-13 United Technologies Corporation Model based engine inlet condition estimation
US10571316B2 (en) * 2012-11-09 2020-02-25 Safran Aircraft Engines Method and system for determining the flow rate of air collected from an aircraft engine
US20140130510A1 (en) * 2012-11-09 2014-05-15 Honeywell International Inc. Systems and methods for directing cooling flow into the surge plenum of an exhaust eductor cooling system
US9255525B2 (en) * 2012-11-30 2016-02-09 General Electric Company System and method for gas turbine operation
US9228501B2 (en) * 2012-12-14 2016-01-05 Solar Turbines Incorporated Bleed valve override schedule on off-load transients
US9459671B2 (en) 2013-02-25 2016-10-04 General Electric Company Systems and methods for use in adapting the operation of a gas turbine
US9605559B2 (en) 2015-02-02 2017-03-28 General Electric Company Wash timing based on turbine operating parameters
US9938906B2 (en) 2015-06-01 2018-04-10 Solar Turbines Incorporated Combustion stability logic during off-load transients
JP6639338B2 (ja) * 2016-07-11 2020-02-05 三菱日立パワーシステムズ株式会社 ガスタービン及びガスタービンの運転方法
FR3059734A1 (fr) * 2016-12-06 2018-06-08 Airbus Operations Gmbh Procede et dispositif de controle des prelevements sur une turbomachine limitant le risque de pompage par echange d'informations entre un gestionnaire d'energie et un systeme de controle de la turbomachine
CN110886656B (zh) * 2018-09-11 2024-06-18 普拉特-惠特尼加拿大公司 用于为发动机启动设定加速度计划的方法与系统
CN110886658A (zh) * 2018-09-11 2020-03-17 普拉特 - 惠特尼加拿大公司 用于检测高涡轮温度操作的方法和系统
CN109611217B (zh) * 2018-11-07 2020-12-11 大连理工大学 一种航空发动机过渡态控制规律优化的设计方法
FR3104542B1 (fr) * 2019-12-13 2021-12-03 Safran Power Units Groupe auxiliaire de puissance comprenant un générateur de gaz à entrainement direct avec un générateur électrique et un boîtier d’accessoires
US12025060B2 (en) * 2021-05-19 2024-07-02 Pratt & Whitney Canada Corp. Method and system for operating an engine to prevent high power engine surges
GB202201987D0 (en) * 2022-02-15 2022-03-30 Rolls Royce Plc Engine system and method of operating the same
GB202201986D0 (en) 2022-02-15 2022-03-30 Rolls Royce Plc Engine system and method of operating the same
US20250139318A1 (en) * 2023-10-30 2025-05-01 Honeywell International Inc. System and Method for Turbine Engine Parameter Synthesis

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2743578A (en) * 1950-11-24 1956-05-01 Bendix Aviat Corp Turbojet engine control system
CA942408A (en) * 1971-04-28 1974-02-19 William L. Webb Integrated control for a turbopropulsion system
US4117668A (en) * 1975-11-19 1978-10-03 United Technologies Corporation Stall detector for gas turbine engine
US4490791A (en) 1982-04-19 1984-12-25 Chandler Evans Inc. Adaptive gas turbine acceleration control
GR78259B (enExample) * 1982-06-21 1984-09-26 United Technologies Corp
US4603546A (en) * 1985-07-16 1986-08-05 Rolls-Royce Limited Control systems for gas turbine aeroengines
US5226287A (en) * 1991-07-19 1993-07-13 General Electric Company Compressor stall recovery apparatus
US5732546A (en) * 1996-07-19 1998-03-31 General Electric Company Transient turbine overtemperature control
US6141951A (en) 1998-08-18 2000-11-07 United Technologies Corporation Control system for modulating bleed in response to engine usage
US6226974B1 (en) 1999-06-25 2001-05-08 General Electric Co. Method of operation of industrial gas turbine for optimal performance
US6513333B2 (en) * 2000-05-25 2003-02-04 Honda Giken Kogyo Kabushiki Kaisha Surge detection system of gas turbine aeroengine
JP2002138857A (ja) * 2000-11-01 2002-05-17 Honda Motor Co Ltd ガスタービンエンジンの加減速制御装置

Also Published As

Publication number Publication date
JP2005509794A (ja) 2005-04-14
WO2003044353A1 (en) 2003-05-30
US6820429B2 (en) 2004-11-23
US20030131605A1 (en) 2003-07-17
DE60230791D1 (de) 2009-02-26
EP1444428A1 (en) 2004-08-11
EP1444428B1 (en) 2009-01-07

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