ES2018760A4 - Dispositivo de control electromecanico utilizable en la conduccion de un vehiculo. - Google Patents
Dispositivo de control electromecanico utilizable en la conduccion de un vehiculo.Info
- Publication number
- ES2018760A4 ES2018760A4 ES90401312T ES90401312T ES2018760A4 ES 2018760 A4 ES2018760 A4 ES 2018760A4 ES 90401312 T ES90401312 T ES 90401312T ES 90401312 T ES90401312 T ES 90401312T ES 2018760 A4 ES2018760 A4 ES 2018760A4
- Authority
- ES
- Spain
- Prior art keywords
- vehicle
- driving
- 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.)
- Granted
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 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
- G05D1/0061—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot 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
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 true ES2018760A4 (es) | 1991-05-16 |
ES2018760T3 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) | DE69015701T2 (es) |
ES (1) | ES2018760T3 (es) |
FR (1) | FR2647922B1 (es) |
Families Citing this family (17)
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 |
US8074940B2 (en) * | 2007-08-08 | 2011-12-13 | 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 |
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)
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 |
-
1989
- 1989-05-31 FR FR8907492A patent/FR2647922B1/fr not_active Expired - Fee Related
-
1990
- 1990-05-17 EP EP90401312A patent/EP0401079B1/fr not_active Expired - Lifetime
- 1990-05-17 DE DE69015701T patent/DE69015701T2/de not_active Expired - Fee Related
- 1990-05-17 ES ES90401312T patent/ES2018760T3/es not_active Expired - Lifetime
- 1990-05-17 DE DE199090401312T patent/DE401079T1/de active Pending
- 1990-05-30 US US07/530,697 patent/US5059882A/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
US5059882A (en) | 1991-10-22 |
FR2647922A1 (fr) | 1990-12-07 |
DE69015701T2 (de) | 1995-06-08 |
EP0401079B1 (fr) | 1995-01-04 |
DE69015701D1 (de) | 1995-02-16 |
ES2018760T3 (es) | 1995-03-01 |
DE401079T1 (de) | 1991-03-21 |
EP0401079A1 (fr) | 1990-12-05 |
FR2647922B1 (fr) | 1993-12-31 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
FG2A | Definitive protection |
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