FR1564055A - - Google Patents
Info
- Publication number
- FR1564055A FR1564055A FR1564055DA FR1564055A FR 1564055 A FR1564055 A FR 1564055A FR 1564055D A FR1564055D A FR 1564055DA FR 1564055 A FR1564055 A FR 1564055A
- Authority
- FR
- France
- 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
- F02K—JET-PROPULSION PLANTS
- F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
- F02K1/06—Varying effective area of jet pipe or nozzle
- F02K1/15—Control or regulation
- F02K1/16—Control or regulation conjointly with another control
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB01509/67A GB1215931A (en) | 1967-03-11 | 1967-03-11 | Improvements in or relating to gas turbine engines |
Publications (1)
Publication Number | Publication Date |
---|---|
FR1564055A true FR1564055A (en) | 1969-04-18 |
Family
ID=9987554
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1564055D Expired FR1564055A (en) | 1967-03-11 | 1968-03-08 |
Country Status (3)
Country | Link |
---|---|
US (1) | US3523423A (en) |
FR (1) | FR1564055A (en) |
GB (1) | GB1215931A (en) |
Families Citing this family (25)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3579992A (en) * | 1969-01-03 | 1971-05-25 | United Aircraft Corp | Power plant variable geometry control |
GB1340879A (en) * | 1970-08-11 | 1973-12-19 | Secr Defence | Control system for gas turbine engine |
GB1310784A (en) * | 1970-09-17 | 1973-03-21 | Nissan Motor | Control system for gas turbine engine |
US3686860A (en) * | 1970-09-25 | 1972-08-29 | Chandler Evans Inc | Nozzle control |
DE2208040C3 (en) * | 1972-02-21 | 1979-05-23 | Robert Bosch Gmbh, 7000 Stuttgart | Control circuit for the process temperature of a gas turbine |
DE2241363B2 (en) * | 1972-08-23 | 1975-01-09 | Motoren- Und Turbinen-Union Muenchen Gmbh, 8000 Muenchen | Control device for a gas turbine engine, in particular a motor vehicle |
US3797233A (en) * | 1973-06-28 | 1974-03-19 | United Aircraft Corp | Integrated control for a turbopropulsion system |
US3872292A (en) * | 1973-07-26 | 1975-03-18 | Us Navy | Sonic means for detecting compressor stall |
US3938321A (en) * | 1974-03-04 | 1976-02-17 | General Motors Corporation | Gas turbine control |
US3952502A (en) * | 1974-03-04 | 1976-04-27 | General Motors Corporation | Gas turbine control |
US3971208A (en) * | 1974-04-01 | 1976-07-27 | The Garrett Corporation | Gas turbine fuel control |
US4134258A (en) * | 1974-06-10 | 1979-01-16 | Nippondenso Co., Ltd. | Fuel control system |
GB1519144A (en) * | 1974-07-09 | 1978-07-26 | Lucas Industries Ltd | Electronic fuel control for a gas turbine engine |
GB1519143A (en) * | 1974-07-09 | 1978-07-26 | Lucas Industries Ltd | Electronic fuel control for a gas turbine engine |
US4206597A (en) * | 1976-04-23 | 1980-06-10 | The Boeing Company | Fan R.P.M. control loop stabilization using high rotor speed |
US4397148A (en) * | 1980-07-02 | 1983-08-09 | General Electric Company | Control system for an augmented turbofan engine |
US4813226A (en) * | 1987-01-12 | 1989-03-21 | Grosselfinger Robert A | Demand control of variable geometry gas turbine power plant |
US4947643A (en) * | 1988-09-20 | 1990-08-14 | United Technologies Corporation | Active geometry control system for gas turbine engines |
US5301500A (en) * | 1990-07-09 | 1994-04-12 | General Electric Company | Gas turbine engine for controlling stall margin |
US5206810A (en) * | 1991-02-07 | 1993-04-27 | General Electric Company | Redundant actuator control |
US7011498B2 (en) * | 1998-04-03 | 2006-03-14 | Athena Technologies, Inc. | Optimization method for power generation systems |
US6171055B1 (en) * | 1998-04-03 | 2001-01-09 | Aurora Flight Sciences Corporation | Single lever power controller for manned and unmanned aircraft |
US9506405B2 (en) | 1998-04-03 | 2016-11-29 | Rockwell Collins Control Technologies, Inc. | Apparatus and method for controlling power generation system |
EP2064434B1 (en) * | 2006-10-12 | 2012-06-27 | United Technologies Corporation | Operational line management of low pressure compressor in a turbofan engine |
EP2066872B1 (en) * | 2006-10-12 | 2014-06-18 | United Technologies Corporation | Method and device to avoid turbofan instability in a gas turbine engine. |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2933887A (en) * | 1953-07-16 | 1960-04-26 | Rolls Royce | Compound gas turbine engine with control for low-pressure rotor |
US3021668A (en) * | 1957-01-11 | 1962-02-20 | Bendix Corp | Nozzle area control for turbojet engines |
GB862334A (en) * | 1958-12-05 | 1961-03-08 | Rolls Royce | Improvements in or relating to gas turbine jet propulsion engines |
US3289411A (en) * | 1963-09-13 | 1966-12-06 | Bendix Corp | Coordinated afterburner fuel control and exhaust nozzle area control for gas turbine engine |
-
1967
- 1967-03-11 GB GB01509/67A patent/GB1215931A/en not_active Expired
-
1968
- 1968-03-08 FR FR1564055D patent/FR1564055A/fr not_active Expired
- 1968-03-11 US US711958A patent/US3523423A/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
US3523423A (en) | 1970-08-11 |
GB1215931A (en) | 1970-12-16 |
Similar Documents
Legal Events
Date | Code | Title | Description |
---|---|---|---|
TP | Transmission of property | ||
TP | Transmission of property | ||
TP | Transmission of property | ||
ST | Notification of lapse |