FR2888009B1 - Dispositif de commande comportant deux manches couples pour permettre de placer des organes commandes dans des positions souhaitees - Google Patents

Dispositif de commande comportant deux manches couples pour permettre de placer des organes commandes dans des positions souhaitees

Info

Publication number
FR2888009B1
FR2888009B1 FR0506715A FR0506715A FR2888009B1 FR 2888009 B1 FR2888009 B1 FR 2888009B1 FR 0506715 A FR0506715 A FR 0506715A FR 0506715 A FR0506715 A FR 0506715A FR 2888009 B1 FR2888009 B1 FR 2888009B1
Authority
FR
France
Prior art keywords
control device
desired positions
allow placement
sleeves coupled
controlled organs
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.)
Active
Application number
FR0506715A
Other languages
English (en)
Other versions
FR2888009A1 (fr
Inventor
Eric Granier
Jeremie Guerard
Max Maurice Viet
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.)
Dassault Aviation SA
Original Assignee
Dassault Aviation 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 Dassault Aviation SA filed Critical Dassault Aviation SA
Priority to FR0506715A priority Critical patent/FR2888009B1/fr
Priority to US11/476,767 priority patent/US7648106B2/en
Priority to GB0612876A priority patent/GB2427906B/en
Publication of FR2888009A1 publication Critical patent/FR2888009A1/fr
Application granted granted Critical
Publication of FR2888009B1 publication Critical patent/FR2888009B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • 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
    • 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
    • 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
    • B64C13/12—Dual control apparatus
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05G—CONTROL DEVICES OR SYSTEMS INSOFAR AS CHARACTERISED BY MECHANICAL FEATURES ONLY
    • G05G11/00—Manually-actuated control mechanisms provided with two or more controlling members co-operating with one single controlled member
    • 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
    • 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
    • G05G2009/04703—Mounting of controlling member
    • G05G2009/04714—Mounting of controlling member with orthogonal axes
    • G05G2009/04718—Mounting of controlling member with orthogonal axes with cardan or gimbal type joint
    • 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
FR0506715A 2005-06-30 2005-06-30 Dispositif de commande comportant deux manches couples pour permettre de placer des organes commandes dans des positions souhaitees Active FR2888009B1 (fr)

Priority Applications (3)

Application Number Priority Date Filing Date Title
FR0506715A FR2888009B1 (fr) 2005-06-30 2005-06-30 Dispositif de commande comportant deux manches couples pour permettre de placer des organes commandes dans des positions souhaitees
US11/476,767 US7648106B2 (en) 2005-06-30 2006-06-29 Control system including two control columns that are coupled to enable controlled members to be placed in required positions
GB0612876A GB2427906B (en) 2005-06-30 2006-06-29 Control system including two coupled control columns for placing controlled members in required positions

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0506715A FR2888009B1 (fr) 2005-06-30 2005-06-30 Dispositif de commande comportant deux manches couples pour permettre de placer des organes commandes dans des positions souhaitees

Publications (2)

Publication Number Publication Date
FR2888009A1 FR2888009A1 (fr) 2007-01-05
FR2888009B1 true FR2888009B1 (fr) 2007-09-07

Family

ID=35789240

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0506715A Active FR2888009B1 (fr) 2005-06-30 2005-06-30 Dispositif de commande comportant deux manches couples pour permettre de placer des organes commandes dans des positions souhaitees

Country Status (3)

Country Link
US (1) US7648106B2 (fr)
FR (1) FR2888009B1 (fr)
GB (1) GB2427906B (fr)

Families Citing this family (24)

* Cited by examiner, † Cited by third party
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US9340278B2 (en) * 2006-05-17 2016-05-17 Textron Innovations, Inc. Flight control system
US8078340B2 (en) * 2007-11-12 2011-12-13 Honeywell International Inc. Active user interface haptic feedback and linking control system using either force or position data
US8136421B2 (en) * 2008-01-10 2012-03-20 Honeywell International Inc. Gimbal assembly including flexible substrate wiring harnesses
FR2958050B1 (fr) * 2010-03-24 2012-12-28 Dassault Aviat Procede et systeme de gestion de la variation d'energie d'un aeronef
FR2958033B1 (fr) 2010-03-24 2012-05-25 Dassault Aviat Dispositif d'affichage de la variation d'energie d'un aeronef, procede et systeme d'affichage de la variation d'energie correspondants
US9405312B2 (en) * 2010-07-28 2016-08-02 Woodward Mpc, Inc. Active control column with manually activated reversion to passive control column
US9051045B2 (en) * 2010-07-28 2015-06-09 Woodward Mpc, Inc. Indirect drive active control column
US8814103B2 (en) * 2010-07-28 2014-08-26 Woodward Mpc, Inc. Position control system for cross coupled operation of fly-by-wire control columns
US8469317B2 (en) * 2010-10-22 2013-06-25 Woodward Mpc, Inc. Line replaceable, fly-by-wire control columns with push-pull interconnect rods
US9126676B2 (en) 2011-10-28 2015-09-08 Woodward Mpc, Inc. Compact two axis gimbal for control stick
US9096325B2 (en) * 2013-11-18 2015-08-04 Bell Helicopter Textron Inc. Fly-by-wire engine power control system
US10676185B2 (en) 2014-08-28 2020-06-09 Sikorsky Aircraft Corporation Rotary wing aircraft pitch control system
WO2016043942A2 (fr) * 2014-08-28 2016-03-24 Sikorsky Aircraft Corporation Système de commande de pas
FR3031959B1 (fr) * 2015-01-27 2017-02-17 Ratier Figeac Soc Procede et dispositif de conjugaison d'organes de pilotage
DE102016108472B4 (de) * 2015-05-11 2021-03-04 Grammer Aktiengesellschaft Steuersystem für Fahrzeuge
EP3096197B1 (fr) * 2015-05-11 2020-11-25 Grammer Ag Systeme de commande pour vehicules
GB2549272A (en) 2016-04-11 2017-10-18 Bae Systems Plc Control systems
GB2549270B (en) * 2016-04-11 2022-12-07 Bae Systems Plc Control systems and methods
FR3051928B1 (fr) * 2016-05-30 2019-01-25 Robert Bosch Gmbh Telecommande a manette munie d'un mecanisme de reaction a moteur et ressort de rappel
US10351257B2 (en) 2017-09-28 2019-07-16 Hamilton Sundstrand Corporation Retention member monitoring system for slat-flap control lever
US11085391B2 (en) * 2018-12-07 2021-08-10 Textron Innovations, Inc. Throttle system
US20220009616A1 (en) * 2020-07-13 2022-01-13 Embraer S.A. Rudder system architecture for electrical actuators
FR3117623A1 (fr) * 2020-12-15 2022-06-17 Dassault Aviation Dispositif de pilotage d'un aéronef et procédé associé
FR3117624B1 (fr) 2020-12-15 2022-12-16 Dassault Aviat Dispositif de pilotage d'un aéronef et procédé associé

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SE442852B (sv) * 1983-04-18 1986-02-03 Saab Scania Ab Forfarande och anordning vid styrsystem for att astadkomma forhojd momentgradient for sma manoverdonsrorelser
FR2643502B1 (fr) * 1989-02-20 1996-01-19 Aerospatiale Dispositif de commande a manche basculant, notamment pour aeronef, et systeme comportant un tel dispositif
US5291113A (en) 1992-10-06 1994-03-01 Honeywell Inc. Servo coupled hand controllers
FR2754515B1 (fr) * 1996-10-14 1998-12-24 Aerospatiale Dispositif d'aide au pilotage sur un aeronef a commande de vol electrique
FR2756392B1 (fr) * 1996-11-22 1999-01-22 Aerospatiale Systeme de couplage de manches de commande
JP2000195370A (ja) * 1998-12-28 2000-07-14 Sony Computer Entertainment Inc 反力発生装置
JP3091743B1 (ja) * 1999-03-30 2000-09-25 株式会社コミュータヘリコプタ先進技術研究所 操縦装置
US6459228B1 (en) * 2001-03-22 2002-10-01 Mpc Products Corporation Dual input servo coupled control sticks
US6644600B1 (en) * 2002-04-25 2003-11-11 Rockwell Collins, Inc. Method and system for providing manipulation restraining forces for a stick controller on an aircraft

Also Published As

Publication number Publication date
US20090314901A1 (en) 2009-12-24
US7648106B2 (en) 2010-01-19
GB0612876D0 (en) 2006-08-09
GB2427906A (en) 2007-01-10
GB2427906B (en) 2009-06-10
FR2888009A1 (fr) 2007-01-05

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