FR2442967B1 - Dispositif de commande d'alimentation en carburant pour moteur a turbine - Google Patents
Dispositif de commande d'alimentation en carburant pour moteur a turbineInfo
- Publication number
- FR2442967B1 FR2442967B1 FR7929045A FR7929045A FR2442967B1 FR 2442967 B1 FR2442967 B1 FR 2442967B1 FR 7929045 A FR7929045 A FR 7929045A FR 7929045 A FR7929045 A FR 7929045A FR 2442967 B1 FR2442967 B1 FR 2442967B1
- Authority
- FR
- France
- Prior art keywords
- control device
- fuel supply
- turbine engine
- supply control
- turbine
- 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
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
- F02C7/262—Restarting after flame-out
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Output Control And Ontrol Of Special Type Engine (AREA)
- Supercharger (AREA)
- High-Pressure Fuel Injection Pump Control (AREA)
- Electrical Control Of Air Or Fuel Supplied To Internal-Combustion Engine (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US05/964,770 US4245462A (en) | 1978-11-29 | 1978-11-29 | Starting system for a turbine engine |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2442967A1 FR2442967A1 (fr) | 1980-06-27 |
FR2442967B1 true FR2442967B1 (fr) | 1986-04-25 |
Family
ID=25508971
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR7929045A Expired FR2442967B1 (fr) | 1978-11-29 | 1979-11-26 | Dispositif de commande d'alimentation en carburant pour moteur a turbine |
Country Status (7)
Country | Link |
---|---|
US (1) | US4245462A (fr) |
JP (1) | JPS5575540A (fr) |
CA (1) | CA1120276A (fr) |
DE (1) | DE2948117A1 (fr) |
FR (1) | FR2442967B1 (fr) |
GB (1) | GB2035461B (fr) |
SE (1) | SE435203B (fr) |
Families Citing this family (19)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4337615A (en) * | 1979-03-21 | 1982-07-06 | The Garrett Corporation | Gas turbine fuel control system |
GB2065779B (en) * | 1979-12-21 | 1983-09-21 | Rolls Royce | Gas turbine fuel system |
US4517796A (en) * | 1983-06-03 | 1985-05-21 | Allied Corporation | Power lever apparatus for a turbine engine |
US4837697A (en) * | 1987-07-31 | 1989-06-06 | Allied-Signal Inc. | Overspeed governor for an electronic controlled fuel system |
GB8911806D0 (en) * | 1989-05-23 | 1989-07-12 | Rolls Royce Plc | Gas turbine engine fuel control system with enhanced relight capability |
US5103629A (en) * | 1989-11-20 | 1992-04-14 | Westinghouse Electric Corp. | Gas turbine control system having optimized ignition air flow control |
US5132009A (en) * | 1990-02-26 | 1992-07-21 | Allied-Signal Inc. | Filter for a fuel system |
US5465570A (en) * | 1993-12-22 | 1995-11-14 | United Technologies Corporation | Fuel control system for a staged combustor |
US5579632A (en) * | 1995-04-10 | 1996-12-03 | Alliedsignal Inc. | Overspeed governor control system |
US5907949A (en) * | 1997-02-03 | 1999-06-01 | United Technologies Corporation | Starting fuel control method for a turbine engine |
US7197870B2 (en) * | 2004-10-14 | 2007-04-03 | Hamilton Sundstrand Corporation | Pressure/flow sensing stall recovery for a ram air turbine |
US7490471B2 (en) * | 2005-12-08 | 2009-02-17 | General Electric Company | Swirler assembly |
US9115648B2 (en) * | 2009-04-10 | 2015-08-25 | General Electric Company | Corrected megawatt backup curve methodology |
US8572985B2 (en) * | 2009-06-26 | 2013-11-05 | Pratt & Whitney Canada Corp. | Air filtration system for gas turbine engine pneumatic system |
CN101598067B (zh) * | 2009-07-10 | 2013-09-18 | 哈尔滨东安发动机(集团)有限公司 | 燃气轮机自动起动的控制方法 |
FR2991388B1 (fr) * | 2012-05-29 | 2016-01-15 | Snecma | Turbomachine pour moteur d'aeronef |
FR3001260B1 (fr) * | 2013-01-18 | 2017-04-21 | Astrium Sas | Dispositif de demarrage d'une turbopompe de moteur fusee |
US11428170B2 (en) * | 2016-07-01 | 2022-08-30 | Raytheon Technologies Corporation | Descent operation for an aircraft parallel hybrid gas turbine electric propulsion system |
CN110886661B (zh) * | 2018-09-11 | 2024-05-28 | 普拉特-惠特尼加拿大公司 | 设定根据飞行器速度变化的发动机起动燃料流的方法和系统 |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2720751A (en) * | 1949-12-23 | 1955-10-18 | Bendix Aviat Corp | Fuel scheduling control system for gas turbine engines |
US2892309A (en) * | 1953-12-21 | 1959-06-30 | Sperry Rand Corp | Fuel metering system for starting gas turbine engines |
US3075350A (en) * | 1958-12-19 | 1963-01-29 | Bendix Corp | Gas turbine fuel control including timing device for scheduling acceleration |
US3672163A (en) * | 1970-01-02 | 1972-06-27 | Chandler Evans Inc | Integral fuel control |
US3922850A (en) * | 1973-04-30 | 1975-12-02 | Colt Ind Operating Corp | Turbine engine fuel control |
US4010605A (en) * | 1974-08-08 | 1977-03-08 | Westinghouse Electric Corporation | Accurate, stable and highly responsive gas turbine startup speed control with fixed time acceleration especially useful in combined cycle electric power plants |
US4117668A (en) * | 1975-11-19 | 1978-10-03 | United Technologies Corporation | Stall detector for gas turbine engine |
US4044554A (en) * | 1976-07-19 | 1977-08-30 | General Motors Corporation | Gas turbine engine fuel control |
-
1978
- 1978-11-29 US US05/964,770 patent/US4245462A/en not_active Expired - Lifetime
-
1979
- 1979-10-18 CA CA000337960A patent/CA1120276A/fr not_active Expired
- 1979-11-20 GB GB7940075A patent/GB2035461B/en not_active Expired
- 1979-11-26 FR FR7929045A patent/FR2442967B1/fr not_active Expired
- 1979-11-29 JP JP15494879A patent/JPS5575540A/ja active Granted
- 1979-11-29 DE DE19792948117 patent/DE2948117A1/de not_active Ceased
- 1979-11-29 SE SE7909855A patent/SE435203B/sv not_active IP Right Cessation
Also Published As
Publication number | Publication date |
---|---|
GB2035461B (en) | 1982-10-13 |
JPS5575540A (en) | 1980-06-06 |
FR2442967A1 (fr) | 1980-06-27 |
JPS6227257B2 (fr) | 1987-06-13 |
DE2948117A1 (de) | 1980-06-12 |
SE435203B (sv) | 1984-09-10 |
SE7909855L (sv) | 1980-05-30 |
US4245462A (en) | 1981-01-20 |
GB2035461A (en) | 1980-06-18 |
CA1120276A (fr) | 1982-03-23 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
ST | Notification of lapse |