DE60125277D1 - Stellantrieb, insbesondere für Flugzeuge - Google Patents

Stellantrieb, insbesondere für Flugzeuge

Info

Publication number
DE60125277D1
DE60125277D1 DE60125277T DE60125277T DE60125277D1 DE 60125277 D1 DE60125277 D1 DE 60125277D1 DE 60125277 T DE60125277 T DE 60125277T DE 60125277 T DE60125277 T DE 60125277T DE 60125277 D1 DE60125277 D1 DE 60125277D1
Authority
DE
Germany
Prior art keywords
aircraft
actuator
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
DE60125277T
Other languages
English (en)
Other versions
DE60125277T2 (de
Inventor
Fernand Rodrigues
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.)
Goodrich Actuation Systems SAS
Original Assignee
Goodrich Actuation Systems SAS
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 Goodrich Actuation Systems SAS filed Critical Goodrich Actuation Systems SAS
Application granted granted Critical
Publication of DE60125277D1 publication Critical patent/DE60125277D1/de
Publication of DE60125277T2 publication Critical patent/DE60125277T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C13/00Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • B64C13/24Transmitting means
    • B64C13/38Transmitting means with power amplification
    • B64C13/50Transmitting means with power amplification using electrical energy
    • B64C13/505Transmitting means with power amplification using electrical energy having duplication or stand-by provisions
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C13/00Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • B64C13/24Transmitting means
    • B64C13/26Transmitting means without power amplification or where power amplification is irrelevant
    • B64C13/28Transmitting means without power amplification or where power amplification is irrelevant mechanical
    • B64C13/341Transmitting means without power amplification or where power amplification is irrelevant mechanical having duplication or stand-by provisions
DE60125277T 2000-05-22 2001-05-18 Stellantrieb, insbesondere für Flugzeuge Expired - Lifetime DE60125277T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0006550A FR2809080B1 (fr) 2000-05-22 2000-05-22 Dispositif d'actionnement, notamment pour commande de vol d'aeronef
FR0006550 2000-05-22

Publications (2)

Publication Number Publication Date
DE60125277D1 true DE60125277D1 (de) 2007-02-01
DE60125277T2 DE60125277T2 (de) 2007-05-24

Family

ID=8850500

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60125277T Expired - Lifetime DE60125277T2 (de) 2000-05-22 2001-05-18 Stellantrieb, insbesondere für Flugzeuge

Country Status (5)

Country Link
US (1) US6588704B2 (de)
EP (1) EP1157923B1 (de)
DE (1) DE60125277T2 (de)
ES (1) ES2276755T3 (de)
FR (1) FR2809080B1 (de)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6802475B2 (en) * 2002-07-04 2004-10-12 Smiths Wolverhampton Limited Flight surface actuator
DE102004047008A1 (de) * 2004-09-28 2006-03-30 Liebherr-Aerospace Lindenberg Gmbh Vorrichtung zur Einstellung von Flugzeughöhenflossen
DE102007044642A1 (de) * 2007-09-19 2009-04-02 Liebherr-Aerospace Lindenberg Gmbh Flugzeughochauftriebssystem
US8072172B2 (en) * 2008-12-17 2011-12-06 Honeywell International Inc. Redundant electromechanical actuator for control surfaces
US8504221B2 (en) * 2009-01-16 2013-08-06 The Boeing Company Apparatus and method for controlling a control surface of a vehicle based on a load identified on the control surface
EP2296064B1 (de) * 2009-09-10 2019-04-24 Sikorsky Aircraft Corporation Leben verbesserndes Flugsteuerungssystem
US9145926B2 (en) * 2012-12-10 2015-09-29 Sikorsky Aircraft Corporation Friction clutch for shaft driven accessories
CN106184774B (zh) * 2015-04-29 2018-07-24 陕西飞机工业(集团)有限公司 多梯度人感装置及其设计方法
CN105947185B (zh) * 2016-06-02 2018-01-30 江西洪都航空工业集团有限责任公司 一种低摩擦力的弹簧载荷机构

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3426650A (en) * 1965-12-23 1969-02-11 Bell Aerospace Corp Triple channel redundant hydraeric control system
US3940094A (en) * 1974-10-30 1976-02-24 Grumman Aerospace Corporation Wing sweep control system
US3958779A (en) * 1975-05-27 1976-05-25 Fairchild Industries Inc. Aircraft control system with a jam isolating coupling
US4096931A (en) * 1976-06-16 1978-06-27 Caterpillar Tractor Co. Modular steering clutch and brake package
US4533097A (en) * 1983-07-11 1985-08-06 Sundstrand Corporation Multi-motor actuation system for a power drive unit
FR2562028B1 (fr) * 1984-04-03 1986-06-27 Aerospatiale Systeme pour la commande d'une surface aerodynamique horizontale a incidence variable d'un aeronef et agencement de commande hydraulique a servovalve pour un tel systeme
US4577738A (en) * 1984-07-06 1986-03-25 Force Control Industries, Inc. Drive system with oil shear clutch-brake unit
US4683407A (en) * 1985-04-02 1987-07-28 Plessey Incorporated Authority limiter
DE3638820A1 (de) * 1986-09-12 1988-03-24 Messerschmitt Boelkow Blohm Seitenruder-steuerungsanordnung fuer luftfahrzeuge
US5092539A (en) * 1989-10-13 1992-03-03 Bell Helicopter Textron Inc. Jam resistant ball screw actuator
US5806805A (en) * 1996-08-07 1998-09-15 The Boeing Company Fault tolerant actuation system for flight control actuators
US5921361A (en) * 1997-07-24 1999-07-13 Midwest Brake Bond Company Press drive with oil shear clutch/brake drives
FR2778164B1 (fr) * 1998-04-29 2000-06-23 Aerospatiale Systeme de commande mixte pour surface aerodynamique d'aeronef
US6227481B1 (en) * 1999-08-06 2001-05-08 Bell Helicopter Textron, Inc. Method and apparatus for controlling force fights in a rotating shaft

Also Published As

Publication number Publication date
FR2809080A1 (fr) 2001-11-23
US20010042811A1 (en) 2001-11-22
US6588704B2 (en) 2003-07-08
DE60125277T2 (de) 2007-05-24
ES2276755T3 (es) 2007-07-01
EP1157923A1 (de) 2001-11-28
FR2809080B1 (fr) 2002-08-30
EP1157923B1 (de) 2006-12-20

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition