DE69015701D1 - Elektromechanische Steuervorrichtung,verwendbar für die Steuerung eines Fahrzeugs. - Google Patents

Elektromechanische Steuervorrichtung,verwendbar für die Steuerung eines Fahrzeugs.

Info

Publication number
DE69015701D1
DE69015701D1 DE69015701T DE69015701T DE69015701D1 DE 69015701 D1 DE69015701 D1 DE 69015701D1 DE 69015701 T DE69015701 T DE 69015701T DE 69015701 T DE69015701 T DE 69015701T DE 69015701 D1 DE69015701 D1 DE 69015701D1
Authority
DE
Germany
Prior art keywords
vehicle
controlling
control device
electromechanical control
device usable
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 - Fee Related
Application number
DE69015701T
Other languages
English (en)
Other versions
DE69015701T2 (de
Inventor
Gerard Marcillat
Jean-Pierre Mota
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.)
Thales Avionics SAS
Original Assignee
Thales Avionics 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
Family has litigation
First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=9382443&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=DE69015701(D1) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by Thales Avionics SAS filed Critical Thales Avionics SAS
Publication of DE69015701D1 publication Critical patent/DE69015701D1/de
Application granted granted Critical
Publication of DE69015701T2 publication Critical patent/DE69015701T2/de
Anticipated expiration legal-status Critical
Expired - Fee Related 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
    • B64C13/02—Initiating means
    • B64C13/04—Initiating means actuated personally
    • B64C13/042—Initiating means actuated personally operated by hand
    • B64C13/0421—Initiating means actuated personally operated by hand control sticks for primary flight controls
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/0055—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements
    • G05D1/0061—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements for transition from automatic pilot to manual pilot and vice versa
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05G—CONTROL DEVICES OR SYSTEMS INSOFAR AS CHARACTERISED BY MECHANICAL FEATURES ONLY
    • G05G9/00—Manually-actuated control mechanisms provided with one single controlling member co-operating with two or more controlled members, e.g. selectively, simultaneously
    • G05G9/02—Manually-actuated control mechanisms provided with one single controlling member co-operating with two or more controlled members, e.g. selectively, simultaneously the controlling member being movable in different independent ways, movement in each individual way actuating one controlled member only
    • G05G9/04—Manually-actuated control mechanisms provided with one single controlling member co-operating with two or more controlled members, e.g. selectively, simultaneously the controlling member being movable in different independent ways, movement in each individual way actuating one controlled member only in which movement in two or more ways can occur simultaneously
    • G05G9/047—Manually-actuated control mechanisms provided with one single controlling member co-operating with two or more controlled members, e.g. selectively, simultaneously the controlling member being movable in different independent ways, movement in each individual way actuating one controlled member only in which movement in two or more ways can occur simultaneously the controlling member being movable by hand about orthogonal axes, e.g. joysticks
    • G05G2009/04766—Manually-actuated control mechanisms provided with one single controlling member co-operating with two or more controlled members, e.g. selectively, simultaneously the controlling member being movable in different independent ways, movement in each individual way actuating one controlled member only in which movement in two or more ways can occur simultaneously the controlling member being movable by hand about orthogonal axes, e.g. joysticks providing feel, e.g. indexing means, means to create counterforce

Landscapes

  • Engineering & Computer Science (AREA)
  • Automation & Control Theory (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Mechanical Control Devices (AREA)
  • Toys (AREA)
  • Hydraulic Clutches, Magnetic Clutches, Fluid Clutches, And Fluid Joints (AREA)
  • Steering Controls (AREA)
DE69015701T 1989-05-31 1990-05-17 Elektromechanische Steuervorrichtung,verwendbar für die Steuerung eines Fahrzeugs. Expired - Fee Related DE69015701T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8907492A FR2647922B1 (fr) 1989-05-31 1989-05-31 Dispositif de commande electromecanique utilisable pour le pilotage d'un vehicule

Publications (2)

Publication Number Publication Date
DE69015701D1 true DE69015701D1 (de) 1995-02-16
DE69015701T2 DE69015701T2 (de) 1995-06-08

Family

ID=9382443

Family Applications (2)

Application Number Title Priority Date Filing Date
DE69015701T Expired - Fee Related DE69015701T2 (de) 1989-05-31 1990-05-17 Elektromechanische Steuervorrichtung,verwendbar für die Steuerung eines Fahrzeugs.
DE199090401312T Pending DE401079T1 (de) 1989-05-31 1990-05-17 Elektromechanische antriebsvorrichtung, verwendbar fuer die steuerung eines fahrzeugs.

Family Applications After (1)

Application Number Title Priority Date Filing Date
DE199090401312T Pending DE401079T1 (de) 1989-05-31 1990-05-17 Elektromechanische antriebsvorrichtung, verwendbar fuer die steuerung eines fahrzeugs.

Country Status (5)

Country Link
US (1) US5059882A (de)
EP (1) EP0401079B1 (de)
DE (2) DE69015701T2 (de)
ES (1) ES2018760T3 (de)
FR (1) FR2647922B1 (de)

Families Citing this family (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1995012153A1 (en) * 1992-10-06 1995-05-04 Honeywell Inc. Position dependent rate dampening in an active hand controller
FR2708112B1 (fr) * 1993-07-22 1995-09-01 Ratier Figeac Soc Dispositif de commande à manche de pilotage, notamment mini-manche asservi pour aéronef.
US5412299A (en) * 1993-12-21 1995-05-02 Honeywell, Inc. Variable servo loop compensation in an active hand controller
FR2718102B1 (fr) * 1994-03-29 1996-06-28 Sfim Ind Procédé pour réaliser une loi d'effort antagoniste au mouvement d'un levier de commande de vol et son application au vérin de trim.
FR2728537A1 (fr) * 1994-12-21 1996-06-28 Eurocopter France Dispositif pour l'actionnement d'un organe commande pour un aeronef, tel que notamment un helicoptere, a commandes de vol electriques
US20030183728A1 (en) * 2002-03-29 2003-10-02 The Boeing Company Aircraft control surface controller and associated method
US6776376B2 (en) 2002-10-18 2004-08-17 Hamilton Sunstrand Flight control surface actuation system
FR2858967B1 (fr) * 2003-08-21 2005-10-28 Ratier Figeac Soc Dispositif de commande de vol a amortissement electrique
CA2669919C (en) * 2007-08-08 2015-06-23 Moog Inc. Control stick adapted for use in a fly-by-wire flight control system, and linkage for use therein
FR2920744B1 (fr) * 2007-09-07 2010-04-09 Eurocopter France Verin de compensation pour commande de vol de giravion
DE102008015874A1 (de) * 2008-03-26 2009-10-01 Lemförder Electronic GmbH Betätigungseinrichtung mit Haptikemulation
FR2952448B1 (fr) * 2009-11-06 2012-08-03 Ratier Figeac Soc Dispositif de controle electronique d'un organe de pilotage a microcontroleurs multifonctionnels, dispositif de pilotage et aeronef
US10196131B2 (en) * 2016-02-16 2019-02-05 The Boeing Company Hydraulic system and method for an aircraft flight control system
FR3086076B1 (fr) * 2018-09-13 2021-07-30 Safran Electronics & Defense Dispositif d'application d'effort pour un mini-manche actif
WO2020136357A1 (fr) * 2018-12-28 2020-07-02 Safran Electronics & Defense Dispositif d'application d'effort pour un manche de pilotage d'un aéronef
FR3091262A1 (fr) 2018-12-28 2020-07-03 Safran Electronics & Defense Dispositif d’application d’effort pour un manche de pilotage d’un aéronef
FR3105171B1 (fr) * 2019-12-20 2022-04-15 Safran Electronics & Defense Dispositif d’application d’effort pour un manche de pilotage d’un aéronef et procédé d’utilisation d’un tel manche

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
IL51185A (en) * 1976-02-03 1981-03-31 United Technologies Corp Method and apparatus for automatic aircraft heading control
US4168045A (en) * 1978-02-28 1979-09-18 United Technologies Corporation Speed and collective pitch bias of helicopter longitudinal cyclic pitch
US4345195A (en) * 1979-12-13 1982-08-17 Sperry Corporation Strapdown multifunction servoactuator apparatus for aircraft
CA1158219A (en) * 1980-04-01 1983-12-06 Edmond D. Diamond Multi-axis force stick, self-trimmed aircraft flight control system
US4500967A (en) * 1981-11-27 1985-02-19 United Technologies Corporation Aircraft short-term roll attitude retention system
SE442852B (sv) * 1983-04-18 1986-02-03 Saab Scania Ab Forfarande och anordning vid styrsystem for att astadkomma forhojd momentgradient for sma manoverdonsrorelser
DE3431583A1 (de) * 1984-08-28 1986-03-13 Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn Vorrichtung zur automatischen beseitigung von steuerkraftfehlern bei luftfahrzeugen, insbesondere hubschraubern
FR2590044B1 (fr) * 1985-09-27 1988-01-29 Applic Mach Motrices Dispositif de commande electrique motorise
US4696445A (en) * 1986-09-18 1987-09-29 United Technologies Corporation Collective control system for a helicopter
DE3724915A1 (de) * 1987-07-28 1989-02-09 Meyra Wilhelm Meyer Gmbh & Co Steuereinrichtung fuer elektrische rollstuehle oder dergl.
US4763100A (en) * 1987-08-13 1988-08-09 Wood Lawson A Joystick with additional degree of control

Also Published As

Publication number Publication date
EP0401079B1 (de) 1995-01-04
US5059882A (en) 1991-10-22
FR2647922A1 (fr) 1990-12-07
ES2018760T3 (es) 1995-03-01
ES2018760A4 (es) 1991-05-16
FR2647922B1 (fr) 1993-12-31
DE69015701T2 (de) 1995-06-08
DE401079T1 (de) 1991-03-21
EP0401079A1 (de) 1990-12-05

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Legal Events

Date Code Title Description
8363 Opposition against the patent
8365 Fully valid after opposition proceedings
8339 Ceased/non-payment of the annual fee