DE68928110D1 - Steuerungssystem für den Antrieb eines Luftfahrzeugs - Google Patents

Steuerungssystem für den Antrieb eines Luftfahrzeugs

Info

Publication number
DE68928110D1
DE68928110D1 DE68928110T DE68928110T DE68928110D1 DE 68928110 D1 DE68928110 D1 DE 68928110D1 DE 68928110 T DE68928110 T DE 68928110T DE 68928110 T DE68928110 T DE 68928110T DE 68928110 D1 DE68928110 D1 DE 68928110D1
Authority
DE
Germany
Prior art keywords
propulsion
aircraft
control system
control
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
Application number
DE68928110T
Other languages
English (en)
Other versions
DE68928110T2 (de
Inventor
Ward H Zimmerman
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Boeing Co
Original Assignee
Boeing Co
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 by Boeing Co filed Critical Boeing Co
Publication of DE68928110D1 publication Critical patent/DE68928110D1/de
Application granted granted Critical
Publication of DE68928110T2 publication Critical patent/DE68928110T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
    • G05D1/0055—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot with safety arrangements
    • G05D1/0077—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot with safety arrangements using redundant signals or controls
DE68928110T 1989-02-27 1989-08-25 Steuerungssystem für den Antrieb eines Luftfahrzeugs Expired - Lifetime DE68928110T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US07/317,292 US5044155A (en) 1989-02-27 1989-02-27 Aircraft propulsion control system

Publications (2)

Publication Number Publication Date
DE68928110D1 true DE68928110D1 (de) 1997-07-10
DE68928110T2 DE68928110T2 (de) 1997-09-18

Family

ID=23233009

Family Applications (2)

Application Number Title Priority Date Filing Date
DE68928110T Expired - Lifetime DE68928110T2 (de) 1989-02-27 1989-08-25 Steuerungssystem für den Antrieb eines Luftfahrzeugs
DE68924972T Expired - Lifetime DE68924972T2 (de) 1989-02-27 1989-08-25 Steuerungssystem des Antriebs eines Luftfahrzeugs.

Family Applications After (1)

Application Number Title Priority Date Filing Date
DE68924972T Expired - Lifetime DE68924972T2 (de) 1989-02-27 1989-08-25 Steuerungssystem des Antriebs eines Luftfahrzeugs.

Country Status (3)

Country Link
US (1) US5044155A (de)
EP (2) EP0384991B1 (de)
DE (2) DE68928110T2 (de)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5165240A (en) * 1991-09-18 1992-11-24 Allied-Signal Inc. Method for matching engine torques for multiple engine aircraft
US5424535A (en) * 1993-04-29 1995-06-13 The Boeing Company Optical angle sensor using polarization techniques
US5543627A (en) * 1994-09-23 1996-08-06 The Boeing Company Method for maximizing the solar cell OPTO-electronic conversion efficiency in optically controlled hydraulic actuators
US5709245A (en) * 1994-09-23 1998-01-20 The Boeing Company Optically controlled actuator
US5875818A (en) * 1994-09-23 1999-03-02 The Boeing Company Opto-electric/hydraulic servocactuation
DE19524992C1 (de) * 1995-07-08 1996-08-08 Mtu Muenchen Gmbh Regelung eines Wellentriebwerks mit einem Mikrosteuergerät
US6655125B2 (en) * 2001-12-05 2003-12-02 Honeywell International Inc. System architecture for electromechanical thrust reverser actuation systems
US8364340B2 (en) * 2009-03-31 2013-01-29 General Electric Company Method and systems for virtual sensor selection and blending
US8381510B2 (en) * 2009-04-30 2013-02-26 General Electric Company Method and systems for controlling engine thrust using variable trim
WO2010131069A1 (en) * 2009-05-11 2010-11-18 Clipper Windpower, Inc. Fiber optic distributed input/output system for wind turbine
FR2946015B1 (fr) * 2009-06-02 2011-07-15 Airbus France Systeme de gestion automatique de modes de controle de moteurs d'un aeronef multimoteur.
FR2959835B1 (fr) 2010-05-10 2012-06-15 Airbus Operations Sas Systeme de commande de vol et aeronef le comportant
US8634972B2 (en) * 2011-08-30 2014-01-21 General Electric Company Method and system for integrating engine control and flight control system

Family Cites Families (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3280185A (en) * 1965-10-01 1966-10-18 American Home Prod 3-substituted 1, 2, 4-cyclopentanetrione, 1-thiosemicarbazones
US3811273A (en) * 1973-03-08 1974-05-21 United Aircraft Corp Slaved fuel control for multi-engined aircraft
US4116000A (en) * 1976-11-01 1978-09-26 United Technologies Corporation Engine control system
US4161650A (en) * 1978-04-06 1979-07-17 Lockheed Aircraft Corporation Self-powered fiber optic interconnect system
US4303976A (en) * 1978-09-15 1981-12-01 Lucas Industries, Ltd. Fuel control for a multi-engine gas turbine installation
US4199663A (en) * 1978-11-06 1980-04-22 The Boeing Company Autonomous terminal data communications system
US4249266A (en) * 1979-11-06 1981-02-03 Perkins Research & Mfg. Co., Inc. Fiber optics communication system
AU7223781A (en) * 1980-08-21 1982-03-17 Garrett Corp., The Engine management system
EP0267398B1 (de) * 1980-09-02 1992-02-26 Deutsche Airbus GmbH Anordnung, insbesondere für Luftfahrzeuge, zur Übertragung von Steuersignalen
EP0267397B1 (de) * 1980-09-02 1992-09-16 Deutsche Airbus GmbH Anordnung, insbesondere für Luftfahrzeuge, zur Übertragung von Steuersignalen
FR2496762B1 (fr) * 1980-12-24 1985-06-28 Psa Grpt Int Eco Rech Develop Dispositif d'allumage et de reallumage pour turbine a gaz
US4410948A (en) * 1981-02-13 1983-10-18 The Bendix Corporation Multi-engine autothrottle providing automatic engine EPR equalization
US4545077A (en) * 1982-10-29 1985-10-01 Lockheed Corporation Electro-optical data bus
US4621335A (en) * 1983-05-31 1986-11-04 Allied Corporation Real time recall feature for an engine data processor system
US4546353A (en) * 1984-02-06 1985-10-08 The United States Of America As Represented By The Secretary Of The Air Force Asymmetric thrust warning system for dual engine aircraft
US4655034A (en) * 1984-12-20 1987-04-07 United Technologies Corporation Transient gas turbine engine bleed control
US4653981A (en) * 1985-09-30 1987-03-31 United Technologies Corporation Propeller synchrophaser
US4651563A (en) * 1985-10-16 1987-03-24 Sperry Corporation Jet engine testing apparatus
GB8629492D0 (en) * 1986-12-10 1987-01-21 Smiths Industries Plc Optical radiation sensor apparatus
US4845617A (en) * 1987-06-01 1989-07-04 United Technologies Corporation Autofeather state maintenance
US4903478A (en) * 1987-06-25 1990-02-27 General Electric Company Dual manifold fuel system
US4875168A (en) * 1987-12-22 1989-10-17 United Technologies Corporation Engine speed control apparatus
US4843232A (en) * 1987-12-28 1989-06-27 Allied-Signal Inc. Optic switch and speed sensor

Also Published As

Publication number Publication date
EP0617348A2 (de) 1994-09-28
US5044155A (en) 1991-09-03
EP0384991A1 (de) 1990-09-05
EP0617348A3 (de) 1994-11-02
DE68928110T2 (de) 1997-09-18
DE68924972D1 (de) 1996-01-11
DE68924972T2 (de) 1996-04-18
EP0617348B1 (de) 1997-06-04
EP0384991B1 (de) 1995-11-29

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Legal Events

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8364 No opposition during term of opposition