ES2018760T3 - Dispositivo de mando electromecanico utilizable para el pilotaje de un vehiculo. - Google Patents

Dispositivo de mando electromecanico utilizable para el pilotaje de un vehiculo.

Info

Publication number
ES2018760T3
ES2018760T3 ES90401312T ES90401312T ES2018760T3 ES 2018760 T3 ES2018760 T3 ES 2018760T3 ES 90401312 T ES90401312 T ES 90401312T ES 90401312 T ES90401312 T ES 90401312T ES 2018760 T3 ES2018760 T3 ES 2018760T3
Authority
ES
Spain
Prior art keywords
control device
piloting
vehicle
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 - Lifetime
Application number
ES90401312T
Other languages
English (en)
Other versions
ES2018760A4 (es
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=***_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=ES2018760(T3) "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 ES2018760A4 publication Critical patent/ES2018760A4/es
Application granted granted Critical
Publication of ES2018760T3 publication Critical patent/ES2018760T3/es
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
    • B64C13/02—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)
  • Aviation & Aerospace Engineering (AREA)
  • Automation & Control Theory (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)

Abstract

EL DISPOSITIVO DE CONTROL SEGUN EL INVENTO HACE INTERVENIR UN MANGO DE DIRECCION (1) ARTICULADO EN UN SOPORTE MEDIANTE UNA ARTICULACION (3) CON DOS GRADOS DE LIBERTAD Y DOS EJES DE SALIDA (4,5), CONSTANDO UN CONJUNTO DE DETECCION DE UNOS CAPTADORES DE POSICION (D1,D2) ASOCIADOS A CADA UNO DE DICHOS EJES (4,5), ACTUANDO DOS ELECTROMECANISMOS (M) EN LOS EJES (4,5) MEDIANTE DOS DISPOSITIVOS DE TRANSMISION RESPECTIVOS (8,9), DE FORMA QUE SE OPONGAN A LOS MOVIMIENTOS DEL MANGO (1) DE LOS EFECTOS RESISTENTES DE ACUERDO CON UNA LEY DE ESFUERZO PREDETERMINADA. EL DISPOSITIVO DE TRANSMISION (,9) CONSTA DE UN ENLACE ELASTICO (T) DISPUESTO EN SERIE. EL INVENTO PERMITE INCREMENTAR CONSIDERABLEMENTE LA SEGURIDAD DE LOS DISPOSITIVOS DE CONTROL Y, EN PARTICULAR, AQUELLOS UTILIZADOS EN LAS AERONAVES.
ES90401312T 1989-05-31 1990-05-17 Dispositivo de mando electromecanico utilizable para el pilotaje de un vehiculo. Expired - Lifetime ES2018760T3 (es)

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
ES2018760A4 ES2018760A4 (es) 1991-05-16
ES2018760T3 true ES2018760T3 (es) 1995-03-01

Family

ID=9382443

Family Applications (1)

Application Number Title Priority Date Filing Date
ES90401312T Expired - Lifetime ES2018760T3 (es) 1989-05-31 1990-05-17 Dispositivo de mando electromecanico utilizable para el pilotaje de un vehiculo.

Country Status (5)

Country Link
US (1) US5059882A (es)
EP (1) EP0401079B1 (es)
DE (2) DE401079T1 (es)
ES (1) ES2018760T3 (es)
FR (1) FR2647922B1 (es)

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
KR101533414B1 (ko) * 2007-08-08 2015-07-03 무그 인코포레이티드 조종간
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
FR3091262A1 (fr) * 2018-12-28 2020-07-03 Safran Electronics & Defense Dispositif d’application d’effort pour un manche de pilotage d’un aéronef
WO2020136357A1 (fr) * 2018-12-28 2020-07-02 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
FR2647922B1 (fr) 1993-12-31
DE401079T1 (de) 1991-03-21
EP0401079B1 (fr) 1995-01-04
US5059882A (en) 1991-10-22
EP0401079A1 (fr) 1990-12-05
FR2647922A1 (fr) 1990-12-07
DE69015701D1 (de) 1995-02-16
ES2018760A4 (es) 1991-05-16
DE69015701T2 (de) 1995-06-08

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