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
Application number
Other languages
French (fr)
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed filed Critical
Application granted granted Critical
Publication of FR1564055A publication Critical patent/FR1564055A/fr
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K1/00Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/06Varying effective area of jet pipe or nozzle
    • F02K1/15Control or regulation
    • F02K1/16Control or regulation conjointly with another control
FR1564055D 1967-03-11 1968-03-08 Expired FR1564055A (en)

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)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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

Also Published As

Publication number Publication date
US3523423A (en) 1970-08-11
GB1215931A (en) 1970-12-16

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Legal Events

Date Code Title Description
TP Transmission of property
TP Transmission of property
TP Transmission of property
ST Notification of lapse