DE69824374D1 - Stellantrieb für die Steuerfläche eines Flugzeuges - Google Patents

Stellantrieb für die Steuerfläche eines Flugzeuges

Info

Publication number
DE69824374D1
DE69824374D1 DE69824374T DE69824374T DE69824374D1 DE 69824374 D1 DE69824374 D1 DE 69824374D1 DE 69824374 T DE69824374 T DE 69824374T DE 69824374 T DE69824374 T DE 69824374T DE 69824374 D1 DE69824374 D1 DE 69824374D1
Authority
DE
Germany
Prior art keywords
aircraft
actuator
control surface
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
DE69824374T
Other languages
English (en)
Other versions
DE69824374T2 (de
Inventor
Jean Thierry Audren
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.)
Safran Electronics and Defense SAS
Original Assignee
SFIM INDUSTRIES MASSY
SFIM Industries SA
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 SFIM INDUSTRIES MASSY, SFIM Industries SA filed Critical SFIM INDUSTRIES MASSY
Publication of DE69824374D1 publication Critical patent/DE69824374D1/de
Application granted granted Critical
Publication of DE69824374T2 publication Critical patent/DE69824374T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • B64C13/24—Transmitting means
    • B64C13/38—Transmitting means with power amplification
    • B64C13/50—Transmitting means with power amplification using electrical energy

Landscapes

  • Engineering & Computer Science (AREA)
  • Automation & Control Theory (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • General Electrical Machinery Utilizing Piezoelectricity, Electrostriction Or Magnetostriction (AREA)
  • Vibration Prevention Devices (AREA)
  • Reciprocating, Oscillating Or Vibrating Motors (AREA)
DE69824374T 1997-12-08 1998-12-08 Stellantrieb für die Steuerfläche eines Flugzeuges Expired - Lifetime DE69824374T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR9715480 1997-12-08
FR9715480A FR2771998B1 (fr) 1997-12-08 1997-12-08 Actionneur de gouverne de commande de vol d'aeronef

Publications (2)

Publication Number Publication Date
DE69824374D1 true DE69824374D1 (de) 2004-07-15
DE69824374T2 DE69824374T2 (de) 2005-06-02

Family

ID=9514298

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69824374T Expired - Lifetime DE69824374T2 (de) 1997-12-08 1998-12-08 Stellantrieb für die Steuerfläche eines Flugzeuges

Country Status (7)

Country Link
US (1) US6082672A (de)
EP (1) EP0921070B1 (de)
JP (1) JPH11227695A (de)
CA (1) CA2255996C (de)
DE (1) DE69824374T2 (de)
ES (1) ES2221137T3 (de)
FR (1) FR2771998B1 (de)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2825680B1 (fr) 2001-06-07 2003-09-26 Sagem Actionneur de commande de vol primaire a moteur a vibration
US8015973B2 (en) 2003-02-15 2011-09-13 Gulfstream Aerospace Corporation System and method for aircraft cabin atmospheric composition control
US7878461B2 (en) * 2006-01-17 2011-02-01 Gulfstream Aerospace Corporation System and method for an integrated backup control system
JP2009523658A (ja) 2006-01-17 2009-06-25 ガルフストリーム・エアロスペース・コーポレイション 分散型飛行制御システムのバックアップ制御のための装置及び方法
US7841559B1 (en) 2006-02-16 2010-11-30 Mbda Incorporated Aerial vehicle with variable aspect ratio deployable wings
US20090072083A1 (en) * 2006-06-02 2009-03-19 Honeywell International, Inc. Actuation system with redundant motor actuators
DE102007012425A1 (de) * 2007-03-15 2008-09-18 Airbus Deutschland Gmbh Verfahren und Einrichtung zur Höhenflossentrimmung bei einem Flugzeug
GB201015510D0 (en) * 2010-09-16 2010-10-27 Goodrich Actuation Systems Sas Power supply system
US8742711B2 (en) 2011-09-22 2014-06-03 Honeywell International Inc. Active feedback user interface system and gimbal assembly therefor
EP3423352B1 (de) * 2016-03-01 2021-05-26 Nanomotion Aktuator mit bogenförmiger bewegung und fin-servo auf der basis von piezo-elektrischen motoren
CN106516104A (zh) * 2016-11-30 2017-03-22 哈尔滨工业大学 用于降低旋翼振动的装置

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3021097A (en) * 1956-06-28 1962-02-13 Sperry Rand Corp Automatic pilot for dirigible craft
US3023985A (en) * 1959-07-09 1962-03-06 Lockheed Aircraft Corp Trim compensator
US4426607A (en) * 1982-03-12 1984-01-17 Sperry Corporation Differential linkage apparatus for an aircraft series servoactuator apparatus
US5001382A (en) * 1988-11-28 1991-03-19 Alps Electric Co., Ltd. Stepping motor and a method of driving the same
EP0543114A1 (de) * 1991-11-18 1993-05-26 Rockwell International Corporation Multiresonanter Antrieb
CA2088234C (en) * 1992-01-29 1999-09-14 Akio Atsuta A vibration driven motor or actuator
US5626312A (en) * 1994-07-06 1997-05-06 Mcdonnell Douglas Corporation Piezoelectric actuator
FR2742011B1 (fr) 1995-11-30 1998-02-20 Sfim Ind Moteur a vibrations a interface rotor/stator a alliage a memoire de forme
US5912525A (en) * 1996-03-21 1999-06-15 Nikon Corporation Vibration actuator
US5907211A (en) * 1997-02-28 1999-05-25 Massachusetts Institute Of Technology High-efficiency, large stroke electromechanical actuator

Also Published As

Publication number Publication date
US6082672A (en) 2000-07-04
FR2771998B1 (fr) 2000-02-25
EP0921070B1 (de) 2004-06-09
JPH11227695A (ja) 1999-08-24
EP0921070A1 (de) 1999-06-09
CA2255996C (fr) 2007-05-15
FR2771998A1 (fr) 1999-06-11
ES2221137T3 (es) 2004-12-16
DE69824374T2 (de) 2005-06-02
CA2255996A1 (fr) 1999-06-08

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8327 Change in the person/name/address of the patent owner

Owner name: SAGEM DEFENSE SECURITE S.A., PARIS, FR