FR2640690B1 - Systeme et procede de commande d'un moteur a turbines a gaz - Google Patents
Systeme et procede de commande d'un moteur a turbines a gazInfo
- Publication number
- FR2640690B1 FR2640690B1 FR898911037A FR8911037A FR2640690B1 FR 2640690 B1 FR2640690 B1 FR 2640690B1 FR 898911037 A FR898911037 A FR 898911037A FR 8911037 A FR8911037 A FR 8911037A FR 2640690 B1 FR2640690 B1 FR 2640690B1
- Authority
- FR
- France
- Prior art keywords
- controlling
- gas turbine
- turbine engine
- engine
- gas
- 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
Links
- RLQJEEJISHYWON-UHFFFAOYSA-N flonicamid Chemical compound FC(F)(F)C1=CC=NC=C1C(=O)NCC#N RLQJEEJISHYWON-UHFFFAOYSA-N 0.000 title 1
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
- F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
- F02C9/26—Control of fuel supply
- F02C9/28—Regulating systems responsive to plant or ambient parameters, e.g. temperature, pressure, rotor speed
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
- G05D1/08—Control of attitude, i.e. control of roll, pitch, or yaw
- G05D1/0808—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft
- G05D1/0858—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft specially adapted for vertical take-off of aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Radar, Positioning & Navigation (AREA)
- General Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Remote Sensing (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Automation & Control Theory (AREA)
- Electrical Control Of Air Or Fuel Supplied To Internal-Combustion Engine (AREA)
- Feedback Control In General (AREA)
- Engine Equipment That Uses Special Cycles (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US07/287,231 US4993221A (en) | 1988-12-21 | 1988-12-21 | Gas turbine engine control system |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2640690A1 FR2640690A1 (fr) | 1990-06-22 |
FR2640690B1 true FR2640690B1 (fr) | 1994-06-10 |
Family
ID=23101996
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR898911037A Expired - Fee Related FR2640690B1 (fr) | 1988-12-21 | 1989-08-18 | Systeme et procede de commande d'un moteur a turbines a gaz |
Country Status (5)
Country | Link |
---|---|
US (1) | US4993221A (fr) |
JP (1) | JP2755713B2 (fr) |
DE (1) | DE3926707C2 (fr) |
FR (1) | FR2640690B1 (fr) |
GB (1) | GB2226430B (fr) |
Families Citing this family (27)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5252860A (en) * | 1989-12-11 | 1993-10-12 | Westinghouse Electric Corp. | Gas turbine control system having maximum instantaneous load-pickup limiter |
DE69024958T2 (de) * | 1990-10-25 | 1996-05-30 | The Boeing Co., Seattle, Wash. | Luftgeschwindigkeitsregelsystem für Flugzeugvortriebsregler |
US5231823A (en) * | 1991-08-22 | 1993-08-03 | General Electric Company | Supervisory control system |
US5331559A (en) * | 1991-09-18 | 1994-07-19 | Alliedsignal Inc. | Apparatus for preventing propeller overshoot |
US5289685A (en) * | 1992-11-16 | 1994-03-01 | General Electric Company | Fuel supply system for a gas turbine engine |
US5303542A (en) * | 1992-11-16 | 1994-04-19 | General Electric Company | Fuel supply control method for a gas turbine engine |
US5761895A (en) * | 1995-08-28 | 1998-06-09 | General Electric Company | Transient load controller for gas turbine power generator |
US6082092A (en) * | 1998-04-08 | 2000-07-04 | General Electric Co. | Combustion dynamics control for variable fuel gas composition and temperature based on gas control valve feedback |
RU2126903C1 (ru) * | 1998-06-09 | 1999-02-27 | Открытое акционерное общество Научно-производственное предприятие "Электронно-гидравлическая автоматика" | Способ обнаружения отказов датчиков и контроля исправности объекта |
US6250877B1 (en) | 2000-07-19 | 2001-06-26 | General Electric Co. | Steam turbine controller having method and apparatus for providing variable frequency regulation |
US6619027B1 (en) | 2000-10-13 | 2003-09-16 | General Electric Company | Gas turbine having rotor overspeed and overboost protection |
US6578794B1 (en) | 2000-11-28 | 2003-06-17 | General Electric Co. | Methods and systems for jet engine overthrust protection |
US6633828B2 (en) | 2001-03-21 | 2003-10-14 | Honeywell International Inc. | Speed signal variance detection fault system and method |
US6609378B2 (en) * | 2002-01-17 | 2003-08-26 | Honeywell International Inc. | Energy based fuel control system for gas turbine engines running on multiple fuel types |
US7431015B2 (en) * | 2006-01-31 | 2008-10-07 | Honeywell International Inc. | Fuel metering system proportional bypass valve error compensation system and method |
FR2899640B1 (fr) * | 2006-04-05 | 2011-11-25 | Eurocopter France | Procede et dispositif pour realiser un controle de l'etat de sante d'un turbomoteur d'un giravion bimoteur |
US7703272B2 (en) * | 2006-09-11 | 2010-04-27 | Gas Turbine Efficiency Sweden Ab | System and method for augmenting turbine power output |
US7854110B2 (en) | 2006-11-16 | 2010-12-21 | Siemens Energy, Inc. | Integrated fuel gas characterization system |
FR2916419B1 (fr) * | 2007-05-22 | 2010-04-23 | Eurocopter France | Helicoptere hybride rapide a grande distance franchissable et rotor de sustentation optimise. |
JP4831836B2 (ja) * | 2007-12-13 | 2011-12-07 | 三菱重工業株式会社 | ガスタービンの制御方法およびガスタービン発電装置 |
GB2461925A (en) * | 2008-07-18 | 2010-01-20 | Rolls Royce Plc | Engine fuel control system |
US8321104B2 (en) * | 2008-07-18 | 2012-11-27 | Rolls-Royce Plc | Control system |
US8484981B2 (en) * | 2008-08-26 | 2013-07-16 | Siemens Energy, Inc. | Integrated fuel gas characterization system |
US8768598B2 (en) * | 2011-12-26 | 2014-07-01 | Textron Innovations Inc. | Dual gain digital engine control |
EP3201086B1 (fr) * | 2014-10-01 | 2019-07-31 | Sikorsky Aircraft Corporation | Gestion de puissance entre un propulseur et un rotor coaxial d'un hélicoptère |
FR3031500B1 (fr) * | 2015-01-12 | 2017-01-13 | Turbomeca | Dispositif et procede de regulation d'un moteur auxiliaire adapte pour fournir une puissance propulsive au rotor d'un helicoptere |
US11920521B2 (en) | 2022-02-07 | 2024-03-05 | General Electric Company | Turboshaft load control using feedforward and feedback control |
Family Cites Families (22)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3114240A (en) * | 1959-09-04 | 1963-12-17 | Bendix Corp | Torque indicator and control for turbo-shaft gas turbine engine |
US3152444A (en) * | 1961-03-01 | 1964-10-13 | Bendix Corp | Fuel control apparatus for turbo-shaft engines |
GB1205323A (en) * | 1968-01-22 | 1970-09-16 | Mini Of Technology | Engine fuel supply servo systems |
US4188781A (en) * | 1978-04-25 | 1980-02-19 | General Electric Company | Non-linear dual mode regulator circuit |
US4258545A (en) * | 1978-06-15 | 1981-03-31 | General Electric Company | Optimal control for a gas turbine engine |
US4313167A (en) * | 1979-07-27 | 1982-01-26 | General Electric Company | Thrust control system for a gas turbine engine |
US4411595A (en) * | 1979-09-19 | 1983-10-25 | General Electric Company | Control system for gas turbine engine |
US4276744A (en) * | 1979-09-19 | 1981-07-07 | General Electric Company | Control system for gas turbine engine |
US4286324A (en) * | 1979-09-24 | 1981-08-25 | Maxwell Ingram | Prime mover fuel efficiency control system |
GB2065779B (en) * | 1979-12-21 | 1983-09-21 | Rolls Royce | Gas turbine fuel system |
US4423592A (en) * | 1980-11-28 | 1984-01-03 | Aviation Electric Ltd. | Fuel control system for gas turbine engine |
US4593523A (en) * | 1980-12-17 | 1986-06-10 | Allied Corporation | Method and apparatus for acceleration limiting a gas turbine engine |
US4625510A (en) * | 1981-04-24 | 1986-12-02 | Bendix Avelex Inc. | Stress limiter apparatus for a gas turbine engine |
US4449360A (en) * | 1981-04-30 | 1984-05-22 | Aviation Electric Ltd. | Stall detector and surge prevention feature for a gas turbine engine |
US4507915A (en) * | 1981-04-30 | 1985-04-02 | Allied Corporation | Stall detector and surge prevention feature for a gas turbine engine |
US4423593A (en) * | 1982-04-16 | 1984-01-03 | Chandler Evans Inc. | Fuel control for controlling helicopter rotor/turbine acceleration |
US4466526A (en) * | 1982-04-16 | 1984-08-21 | Chandler Evans Inc. | Helicopter engine control with rotor speed decay anticipator |
US4522026A (en) * | 1983-02-07 | 1985-06-11 | Pratt & Whitney Canada Inc. | Power/torque limiter unit for free turbine type engines |
DE3306889A1 (de) * | 1983-02-26 | 1984-08-30 | MTU Motoren- und Turbinen-Union München GmbH, 8000 München | Einrichtung zur regelung der lastverteilung und der drehzahl von gasturbinenanlagen, insbesondere -triebwerken |
US4578945A (en) * | 1983-11-10 | 1986-04-01 | Chandler Evans Inc. | Overspeed limiter for gas turbine fuel control |
US4693077A (en) * | 1986-07-18 | 1987-09-15 | General Motors Corporation | Closed-loop engine control with feedback torque error compensation |
US4716723A (en) * | 1986-09-05 | 1988-01-05 | Woodward Governor Company | Fuel controls for gas turbine engines |
-
1988
- 1988-12-21 US US07/287,231 patent/US4993221A/en not_active Expired - Lifetime
-
1989
- 1989-08-12 DE DE3926707A patent/DE3926707C2/de not_active Expired - Fee Related
- 1989-08-18 GB GB8918922A patent/GB2226430B/en not_active Expired - Fee Related
- 1989-08-18 FR FR898911037A patent/FR2640690B1/fr not_active Expired - Fee Related
- 1989-08-21 JP JP1213138A patent/JP2755713B2/ja not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
GB2226430B (en) | 1993-03-17 |
DE3926707C2 (de) | 1998-12-24 |
JP2755713B2 (ja) | 1998-05-25 |
DE3926707A1 (de) | 1990-06-28 |
FR2640690A1 (fr) | 1990-06-22 |
US4993221A (en) | 1991-02-19 |
GB8918922D0 (en) | 1989-09-27 |
JPH02188630A (ja) | 1990-07-24 |
GB2226430A (en) | 1990-06-27 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
BR | Restoration of rights | ||
ST | Notification of lapse |
Effective date: 20080430 |