DE69427384T2 - Drehmomentregelung für einen Gasturbinenstarter - Google Patents
Drehmomentregelung für einen GasturbinenstarterInfo
- Publication number
- DE69427384T2 DE69427384T2 DE69427384T DE69427384T DE69427384T2 DE 69427384 T2 DE69427384 T2 DE 69427384T2 DE 69427384 T DE69427384 T DE 69427384T DE 69427384 T DE69427384 T DE 69427384T DE 69427384 T2 DE69427384 T2 DE 69427384T2
- Authority
- DE
- Germany
- Prior art keywords
- gas turbine
- torque control
- turbine starter
- starter
- torque
- 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 - Lifetime
Links
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
- 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
- F02C7/26—Starting; Ignition
- F02C7/268—Starting drives for the rotor, acting directly on the rotor of the gas turbine to be started
- F02C7/275—Mechanical 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
- F05D2270/00—Control
- F05D2270/01—Purpose of the control system
- F05D2270/04—Purpose of the control system to control acceleration (u)
-
- 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
- F05D2270/00—Control
- F05D2270/30—Control parameters, e.g. input parameters
- F05D2270/304—Spool rotational speed
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Control Of Turbines (AREA)
- Control Of Eletrric Generators (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US3362693A | 1993-03-16 | 1993-03-16 |
Publications (2)
Publication Number | Publication Date |
---|---|
DE69427384D1 DE69427384D1 (de) | 2001-07-12 |
DE69427384T2 true DE69427384T2 (de) | 2002-05-23 |
Family
ID=21871481
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE69427384T Expired - Lifetime DE69427384T2 (de) | 1993-03-16 | 1994-03-14 | Drehmomentregelung für einen Gasturbinenstarter |
Country Status (3)
Country | Link |
---|---|
US (1) | US6035626A (de) |
EP (1) | EP0623741B1 (de) |
DE (1) | DE69427384T2 (de) |
Families Citing this family (63)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5430362A (en) * | 1993-05-12 | 1995-07-04 | Sundstrand Corporation | Engine starting system utilizing multiple controlled acceleration rates |
JP3546735B2 (ja) * | 1999-01-18 | 2004-07-28 | 日産自動車株式会社 | エンジンの始動制御装置 |
DE10047502A1 (de) * | 2000-09-26 | 2002-04-11 | Bosch Gmbh Robert | Verfahren und Vorrichtung zur Steuerung der Drehzahl einer Antriebseinheit |
GB2374904A (en) * | 2001-04-26 | 2002-10-30 | Bowman Power Systems Ltd | Controlling temperature in gas turbine apparatus during startup or shutdown |
JP2004537679A (ja) * | 2001-07-27 | 2004-12-16 | エリオット・エナジー・システムズ・インコーポレイテッド | タービン発電機の点火および始動方法 |
EP1427928A1 (de) * | 2001-08-27 | 2004-06-16 | Elliott Energy Systems, Inc. | Verfahren zum zünden einer gasturbine |
SE520475C2 (sv) * | 2001-11-19 | 2003-07-15 | Volvo Aero Corp | Gasturbinaggregat |
US6628024B1 (en) * | 2002-07-30 | 2003-09-30 | Honeywell International, Inc. | Hermetically sealed feed-through assembly for gas turbine engine starter generators and related methods |
US6819999B2 (en) * | 2002-09-13 | 2004-11-16 | Elliott Energy Systems, Inc. | Multiple control loop acceleration of turboalternator previous to self-sustaining speed |
US6791204B2 (en) * | 2002-09-20 | 2004-09-14 | Honeywell International Inc. | Torque generation for salient-pole synchronous machine for start-up of a prime mover |
US6847194B2 (en) * | 2002-09-20 | 2005-01-25 | Honeywell International Inc. | Electric start for a prime mover |
US6941760B1 (en) | 2003-03-19 | 2005-09-13 | Hamilton Sundstrand Corporation | Start system for expendable gas turbine engine |
US6931862B2 (en) * | 2003-04-30 | 2005-08-23 | Hamilton Sundstrand Corporation | Combustor system for an expendable gas turbine engine |
US6960900B2 (en) * | 2003-11-28 | 2005-11-01 | General Electric Company | Method and apparatus for starting a gas turbine using a polyphase electric power generator |
US6940251B1 (en) | 2004-04-30 | 2005-09-06 | Honeywell International Inc. | Decoupling of cross coupling for floating reference frame controllers for sensorless control of synchronous machines |
US7204090B2 (en) * | 2004-06-17 | 2007-04-17 | Pratt & Whitney Canada Corp. | Modulated current gas turbine engine starting system |
US7332884B2 (en) | 2004-07-16 | 2008-02-19 | Hamilton Sundstrand Corporation | Electric motor control strategies |
US7093447B2 (en) * | 2004-08-25 | 2006-08-22 | Hamilton Sundstrand Corporation | Auxiliary power unit with an oil-free compressor |
US7434406B2 (en) * | 2005-05-10 | 2008-10-14 | Honeywell International Inc. | Drive for using a direct driven generator to start a counter-rotating multi-spool gas turbine engine |
US7690205B2 (en) * | 2005-09-20 | 2010-04-06 | Honeywell International Inc. | Gas turbine engine cold start mechanization |
US7448220B2 (en) * | 2005-10-19 | 2008-11-11 | Hamilton Sundstrand Corporation | Torque control for starting system |
US7802757B2 (en) | 2005-11-09 | 2010-09-28 | Pratt & Whitney Canada Corp. | Method and system for taxiing an aircraft |
FR2905985B1 (fr) * | 2006-09-19 | 2008-12-12 | Hispano Suiza Sa | Integration d'un module demarreur/generateur dans une boite de transmission d'une turbine a gaz |
KR101091912B1 (ko) | 2006-04-17 | 2011-12-08 | 삼성테크윈 주식회사 | 시동 모터의 전류 값을 채용한 가스 터빈 엔진의 시동 제어방법 |
US7840333B2 (en) * | 2007-03-30 | 2010-11-23 | Hamilton Sundstrand Corporation | Event-driven starter controller |
US7926287B2 (en) * | 2007-05-08 | 2011-04-19 | Pratt & Whitney Canada Corp. | Method of operating a gas turbine engine |
US8467949B2 (en) * | 2009-05-29 | 2013-06-18 | Honeywell International Inc. | Methods and systems for turbine line replaceable unit fault detection and isolation during engine startup |
FR2947006B1 (fr) * | 2009-06-17 | 2014-10-17 | Eurocopter France | Dispositif et procede pour le demarrage d'un moteur a turbine equipant un helicoptere,mettant en oeuvre une source d'energie electrique comprenant des organes d'appoint a decharge |
US8384328B2 (en) * | 2009-08-21 | 2013-02-26 | Honeywell International Inc. | Control methodology for an AC starter-generator system |
FR2950657A1 (fr) * | 2009-09-29 | 2011-04-01 | Snecma | Procede et dispositif de controle d'une partie tournante du corps haute pression d'un moteur d'avion. |
US8925328B2 (en) * | 2009-10-26 | 2015-01-06 | Siemens Energy, Inc. | Gas turbine starting process |
US8555653B2 (en) * | 2009-12-23 | 2013-10-15 | General Electric Company | Method for starting a turbomachine |
US9086018B2 (en) * | 2010-04-23 | 2015-07-21 | Hamilton Sundstrand Corporation | Starting a gas turbine engine to maintain a dwelling speed after light-off |
US8355855B2 (en) * | 2010-05-21 | 2013-01-15 | General Electric Company | Systems and methods for controlling an integrated drive train |
US9145833B2 (en) * | 2010-05-25 | 2015-09-29 | General Electric Company | Gas turbine startup control |
US8380388B2 (en) * | 2010-06-01 | 2013-02-19 | GM Global Technology Operations LLC | Method and apparatus for monitoring a starter motor for an internal combustion engine |
US9151180B2 (en) | 2010-06-15 | 2015-10-06 | Hamilton Sundstrand Corporation | Lubrication driven gas turbine engine actuation system |
US8955334B2 (en) * | 2010-07-22 | 2015-02-17 | General Electric Company | Systems and methods for controlling the startup of a gas turbine |
IT1401923B1 (it) * | 2010-09-09 | 2013-08-28 | Nuovo Pignone Spa | Metodi e dispositivi per testare un rotore a bassa velocita ed a basso momento in un turbomacchinario |
JP5738098B2 (ja) * | 2011-07-05 | 2015-06-17 | 三菱日立パワーシステムズ株式会社 | ガスタービンシステム |
US9140194B2 (en) * | 2012-01-11 | 2015-09-22 | Honeywell International Inc. | Gas turbine engine starter-generator with integrated lube oil scavenge functionality |
US8666633B2 (en) | 2012-02-07 | 2014-03-04 | Honeywell International Inc. | Engine systems with efficient start control logic |
US8808142B2 (en) | 2012-04-09 | 2014-08-19 | Hamilton Sundstrand Corporation | Aircraft APU electrical starter torque limiter |
US8738215B2 (en) | 2012-05-04 | 2014-05-27 | Ford Global Technologies, Llc | Methods and systems for a hybrid vehicle |
US8738217B2 (en) * | 2012-05-04 | 2014-05-27 | Ford Global Technologies, Llc | Methods and systems for a hybrid vehicle |
FR2995345B1 (fr) | 2012-09-10 | 2018-06-15 | Safran Helicopter Engines | Procede et systeme de demarrage d'un turbomoteur d'aeronef |
US20140102111A1 (en) * | 2012-10-16 | 2014-04-17 | General Electric Company | Systems and Methods for Distributing Torque Contribution |
WO2014149088A2 (en) * | 2013-03-15 | 2014-09-25 | Rolls-Royce North American Technologies, Inc. | Methods and systems for operating a gas turbine engine |
WO2015133994A1 (en) | 2014-03-04 | 2015-09-11 | Sikorsky Aircraft Corporation | Electrical augmentation of a gas turbine engine |
US9803553B2 (en) * | 2014-04-25 | 2017-10-31 | Rolls-Royce North American Technologies, Inc. | Method to control electric starter generator for gas turbine engines |
US10696417B2 (en) | 2015-06-25 | 2020-06-30 | Pratt & Whitney Canada Corp. | Auxiliary power unit with excess air recovery |
US10590842B2 (en) | 2015-06-25 | 2020-03-17 | Pratt & Whitney Canada Corp. | Compound engine assembly with bleed air |
US10710738B2 (en) * | 2015-06-25 | 2020-07-14 | Pratt & Whitney Canada Corp. | Auxiliary power unit with intercooler |
EP3320203B1 (de) * | 2015-07-08 | 2019-12-18 | GE Aviation Systems LLC | Luftanlasser und verfahren zur bestimmung einer hydrostatischen sperre |
BR112018014725A2 (pt) | 2016-01-20 | 2018-12-11 | Ge Aviation Systems Llc | métodos de inicialização de um motor de combustão e conjunto do acionador de partida de ar de turbina |
CN107241046B (zh) * | 2017-06-13 | 2019-08-27 | 中山大洋电机股份有限公司 | 一种无位置传感器的bldc电机的启动方法 |
FR3076322B1 (fr) * | 2017-12-29 | 2021-09-24 | Safran Aircraft Engines | Procede et dispositif de demarrage pour une turbomachine par temps froid |
GB201803038D0 (en) | 2018-02-26 | 2018-04-11 | Rolls Royce Plc | Methods and apparatus for controlling at least a part of a start-up or re light process of a gas turbine engine |
US11174793B2 (en) * | 2018-09-19 | 2021-11-16 | Raytheon Technologies Corporation | Hydraulic starter assembly for a gas turbine engine |
GB201819694D0 (en) | 2018-12-03 | 2019-01-16 | Rolls Royce | Methods and apparatus for controlling at least part of a start-up or re-light process of a gas turbine engine |
GB201819695D0 (en) | 2018-12-03 | 2019-01-16 | Rolls Royce Plc | Methods and apparatus for controlling at least part of a start-up or re-light process of a gas turbine engine |
GB201819696D0 (en) | 2018-12-03 | 2019-01-16 | Rolls Royce Plc | Methods and apparatus for controlling at least part of a start-up or re-light process of a gas turbine engine |
US20230030319A1 (en) * | 2021-07-29 | 2023-02-02 | The Boeing Company | Gas turbine engine starter systems and associated methods |
Family Cites Families (32)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB587527A (en) * | 1944-01-31 | 1947-04-29 | Power Jets Res & Dev Ltd | Improvements in or relating to internal combustion turbines |
US3470691A (en) * | 1968-06-17 | 1969-10-07 | Avco Corp | Automatic starting and protection system for a gas turbine |
US3793826A (en) * | 1972-12-08 | 1974-02-26 | Gen Motors Corp | Electronic start control circuit for gas turbine engine |
US3937974A (en) * | 1974-08-30 | 1976-02-10 | General Electric Company | Starter-generator utilizing phase controlled rectifiers to drive a dynamoelectric machine as a brushless DC motor in the starting mode with starter position sense variation with speed |
US4119861A (en) * | 1975-10-15 | 1978-10-10 | Tokyo Shibaura Electric Company, Ltd. | Starting apparatus for gas turbine-generator mounted on electric motor driven motorcar |
US4043119A (en) * | 1976-02-20 | 1977-08-23 | Sundstrand Corporation | Acceleration and speed control circuit for jet engine accessory equipment |
US4281509A (en) * | 1976-11-19 | 1981-08-04 | The Garrett Corporation | Fuel control system |
US4276743A (en) * | 1976-11-19 | 1981-07-07 | The Garrett Corporation | Fuel control system |
US4337615A (en) * | 1979-03-21 | 1982-07-06 | The Garrett Corporation | Gas turbine fuel control system |
US4456830A (en) * | 1982-04-22 | 1984-06-26 | Lockheed Corporation | AC Motor-starting for aircraft engines using APU free turbine driven generators |
US4473752A (en) * | 1982-05-27 | 1984-09-25 | Lockheed Corporation | Aircraft engine starting with synchronous ac generator |
SU1059236A1 (ru) * | 1982-06-16 | 1983-12-07 | Производственное Объединение Турбостроения "Ленинградский Металлический Завод" | Система запуска газотурбинной установки |
US4494372A (en) * | 1983-06-10 | 1985-01-22 | Lockheed Corporation | Multi role primary/auxiliary power system with engine start capability for aircraft |
US4627234A (en) * | 1983-06-15 | 1986-12-09 | Sundstrand Corporation | Gas turbine engine/load compressor power plants |
US4708030A (en) * | 1985-03-18 | 1987-11-24 | Sundstrand Corporation | Multi-range starter-generator drive |
US4724331A (en) * | 1986-02-25 | 1988-02-09 | The Boeing Company | Method and apparatus for starting an aircraft engine |
US4684081A (en) * | 1986-06-11 | 1987-08-04 | Lockheed Corporation | Multifunction power system for an aircraft |
JPS6430500A (en) * | 1987-07-24 | 1989-02-01 | Shinko Electric Co Ltd | Brushless starting generator exciter |
US4868406A (en) * | 1988-07-05 | 1989-09-19 | Sundstrand Corporation | Electrically compensated constant speed drive with prime mover start capability |
US4942493A (en) * | 1988-11-02 | 1990-07-17 | Sundstrand Corporation | Method and apparatus for detecting prime mover start malfunction |
JPH02131377A (ja) * | 1988-11-08 | 1990-05-21 | Mitsubishi Electric Corp | 始動装置 |
US5028803A (en) * | 1989-03-22 | 1991-07-02 | Sundstrand Corporation | Integrated drive generator system with direct motor drive prime mover starting |
US4984425A (en) * | 1989-05-30 | 1991-01-15 | United Technologies Corporation | Acceleration control for a gas turbine engine |
US4968926A (en) * | 1989-10-25 | 1990-11-06 | Sundstrand Corporation | Power conversion system with stepped waveform DC to AC converter having prime mover start capability |
US4992721A (en) * | 1990-01-26 | 1991-02-12 | Sundstrand Corporation | Inverter for starting/generating system |
US5051670A (en) * | 1990-07-30 | 1991-09-24 | Aircraft Parts Corp. | Aircraft DC starter-generator torque controller |
US5165223A (en) * | 1990-12-10 | 1992-11-24 | Sundstrand Corporation | Process for starting a gas turbine and gas turbine |
US5172543A (en) * | 1990-12-26 | 1992-12-22 | Sundstrand Corporation | Starting system for a gas turbine and method of starting a gas turbine |
US5123239A (en) * | 1991-02-14 | 1992-06-23 | Sundstrand Corporation | Method of starting a gas turbine engine |
US5127220A (en) * | 1991-02-28 | 1992-07-07 | Allied-Signal Inc. | Method for accelerating a gas turbine engine |
US5212943A (en) * | 1991-10-08 | 1993-05-25 | Sundstrand Corporation | Reduced thermal stress turbine starting strategy |
US5428275A (en) * | 1993-05-12 | 1995-06-27 | Sundstrand Corporation | Controlled starting method for a gas turbine engine |
-
1994
- 1994-03-14 EP EP94103897A patent/EP0623741B1/de not_active Expired - Lifetime
- 1994-03-14 DE DE69427384T patent/DE69427384T2/de not_active Expired - Lifetime
-
1995
- 1995-09-07 US US08/525,227 patent/US6035626A/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
US6035626A (en) | 2000-03-14 |
DE69427384D1 (de) | 2001-07-12 |
EP0623741B1 (de) | 2001-06-06 |
EP0623741A1 (de) | 1994-11-09 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8363 | Opposition against the patent | ||
8365 | Fully valid after opposition proceedings |