FR3095804B1 - Dispositif d’application d’effort pour manche de pilotage - Google Patents

Dispositif d’application d’effort pour manche de pilotage Download PDF

Info

Publication number
FR3095804B1
FR3095804B1 FR1904712A FR1904712A FR3095804B1 FR 3095804 B1 FR3095804 B1 FR 3095804B1 FR 1904712 A FR1904712 A FR 1904712A FR 1904712 A FR1904712 A FR 1904712A FR 3095804 B1 FR3095804 B1 FR 3095804B1
Authority
FR
France
Prior art keywords
magnetic
emitter
force application
pilot stick
shaft
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
FR1904712A
Other languages
English (en)
Other versions
FR3095804A1 (fr
Inventor
Rémi-Louis Lawniczak
Yannick Attrazic
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
Safran Electronics and Defense 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
Application filed by Safran Electronics and Defense SAS filed Critical Safran Electronics and Defense SAS
Priority to FR1904712A priority Critical patent/FR3095804B1/fr
Priority to CN202080038569.0A priority patent/CN113874285A/zh
Priority to PCT/EP2020/062586 priority patent/WO2020225305A1/fr
Priority to US17/609,100 priority patent/US11433989B2/en
Publication of FR3095804A1 publication Critical patent/FR3095804A1/fr
Application granted granted Critical
Publication of FR3095804B1 publication Critical patent/FR3095804B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • 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
    • G—PHYSICS
    • G06—COMPUTING; CALCULATING OR COUNTING
    • G06F—ELECTRIC DIGITAL DATA PROCESSING
    • G06F3/00—Input arrangements for transferring data to be processed into a form capable of being handled by the computer; Output arrangements for transferring data from processing unit to output unit, e.g. interface arrangements
    • G06F3/01—Input arrangements or combined input and output arrangements for interaction between user and computer
    • G06F3/016—Input arrangements with force or tactile feedback as computer generated output to the user
    • 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
    • B64C13/503—Fly-by-Wire
    • 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
    • B64C13/507—Transmitting means with power amplification using electrical energy with artificial feel
    • 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
    • G05G2009/0474—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 characterised by means converting mechanical movement into electric signals
    • G05G2009/04748—Position sensor for rotary movement, e.g. potentiometer
    • 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
    • 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
    • G05G2009/04774—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 with additional switches or sensors on the handle

Abstract

La présente invention concerne un dispositif d’application d’effort pour un manche de pilotage d’un aéronef, dans lequel le manche de pilotage comprend un levier (1) de commande entraînant en rotation un arbre (A1) autour d’un premier axe (A), le dispositif comprenant un frein magnétique (5a) qui comprend un élément aimantable (50a) relié à l’arbre, ainsi qu’un émetteur magnétique (51a) opposé à l’élément aimantable en étant libre en rotation autour du premier axe par rapport à l’élément aimantable, ledit émetteur magnétique présentant un état activé, dans lequel l’émetteur magnétique est alimenté en courant et génère un champ magnétique au niveau d’un volume occupé par l’élément aimantable, et un état désactivé dans lequel l’émetteur magnétique n’est pas alimenté en courant et ne génère pas de champ magnétique, de sorte à empêcher une rotation de l’élément aimantable par rapport à l’émetteur magnétique autour de l’arbre.Figure pour l’abrégé : Fig. 3
FR1904712A 2019-05-06 2019-05-06 Dispositif d’application d’effort pour manche de pilotage Active FR3095804B1 (fr)

Priority Applications (4)

Application Number Priority Date Filing Date Title
FR1904712A FR3095804B1 (fr) 2019-05-06 2019-05-06 Dispositif d’application d’effort pour manche de pilotage
CN202080038569.0A CN113874285A (zh) 2019-05-06 2020-05-06 用于控制杆的力施加设备
PCT/EP2020/062586 WO2020225305A1 (fr) 2019-05-06 2020-05-06 Dispositif d'application d'effort pour manche de pilotage
US17/609,100 US11433989B2 (en) 2019-05-06 2020-05-06 Force application device for a control stick

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1904712 2019-05-06
FR1904712A FR3095804B1 (fr) 2019-05-06 2019-05-06 Dispositif d’application d’effort pour manche de pilotage

Publications (2)

Publication Number Publication Date
FR3095804A1 FR3095804A1 (fr) 2020-11-13
FR3095804B1 true FR3095804B1 (fr) 2021-09-24

Family

ID=67875633

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1904712A Active FR3095804B1 (fr) 2019-05-06 2019-05-06 Dispositif d’application d’effort pour manche de pilotage

Country Status (4)

Country Link
US (1) US11433989B2 (fr)
CN (1) CN113874285A (fr)
FR (1) FR3095804B1 (fr)
WO (1) WO2020225305A1 (fr)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3090574B1 (fr) * 2018-12-21 2021-04-02 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
FR3116509B1 (fr) * 2020-11-26 2022-11-04 Safran Dispositif de guidage à sureté renforcée

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6704001B1 (en) * 1995-11-17 2004-03-09 Immersion Corporation Force feedback device including actuator with moving magnet
GB2347990B (en) * 1998-11-04 2003-05-14 Immersion Corp Force feedback device including actuator with moving magnet
US6320284B1 (en) * 1998-12-23 2001-11-20 Engineering Matters, Inc. Motor assembly allowing output in multiple degrees of freedom
ATE484017T1 (de) * 2002-08-06 2010-10-15 Rockwell Collins Inc Direkte antriebssteuereinheit mit haptischer rückmeldung
US20070235594A1 (en) * 2006-04-06 2007-10-11 Honeywell International, Inc. Pilot flight control stick feedback system
US20080156939A1 (en) * 2007-01-03 2008-07-03 Honeywell International, Inc. Active pilot flight control stick system with passive electromagnetic feedback
FR2920744B1 (fr) * 2007-09-07 2010-04-09 Eurocopter France Verin de compensation pour commande de vol de giravion
MX2008004203A (es) * 2008-03-28 2009-09-28 Michael Robert Axford Motores a pistones que utilizan la energia electromecanica como fuerza impulsora de los pistones.
FR2954835B1 (fr) * 2009-12-30 2012-04-13 Ratier Figeac Soc Dispositif de pilotage de vehicule a actionneur electromagnetique
FR3011815B1 (fr) 2013-10-15 2016-01-08 Sagem Defense Securite Dispositif de commande de vol d'un aeronef
CN106061837B (zh) * 2014-02-28 2018-04-10 赛峰电子与防务公司 用于飞行器的飞行控制装置
FR3054259B1 (fr) * 2016-07-22 2021-06-04 Peugeot Citroen Automobiles Sa Poignee deployable a detection d’obstacle
US10782784B2 (en) * 2017-06-21 2020-09-22 Nanoport Technology Inc. Magnetic tactile feedback actuator having one or more electropermanent magnets and method of operating same

Also Published As

Publication number Publication date
US20220212780A1 (en) 2022-07-07
WO2020225305A1 (fr) 2020-11-12
FR3095804A1 (fr) 2020-11-13
US11433989B2 (en) 2022-09-06
CN113874285A (zh) 2021-12-31

Similar Documents

Publication Publication Date Title
FR3095804B1 (fr) Dispositif d’application d’effort pour manche de pilotage
EP2740200B1 (fr) Ensemble compact de positionnement comprenant un actionneur et un capteur intégré dans la culasse de l'actionneur
JP2922886B2 (ja) 宇宙航行機の配備機構用ダンパ
FR2896285A1 (fr) Dispositif de suspension magnetique d'un rotor
US20080169733A1 (en) Fan and motor thereof
FR2536473A1 (fr) Pompe turbomoleculaire
US20190083839A1 (en) Magnetoresistance adjustment device of fitness equipment
US10750731B1 (en) Micro external adjustable spool braking system
CA2470089C (fr) Dispositif de guidage d'une aube a angle de calage variable
CA1154129A (fr) Dispositif traducteur electrohydraulique permettant notamment de controler une pression dans une transmission automatique
FR3091260B1 (fr) Dispositif d’application d’effort pour un manche de pilotage d’un aéronef
FR2835053A1 (fr) Capteur de course comportant un element convertisseur magnetoelectrique
JPH026292A (ja) 制御可能な固定したプロペラー
CH493960A (fr) Dispositif d'entraînement électromagnétique comprenant une armature à position d'équilibre réglable
US20120282090A1 (en) Hydraulic cyclic blade speed control apparatus and method
CA2091237A1 (fr) Dispositif de transmission d'energie de commande mecanique, notamment pour le controle de la pression de freinage dans un frein
FR3086273B1 (fr) Dispositif de commande de vol d’un aeronef
NL9002642A (nl) Inrichting voor het onderbreken van een materiestroom.
FR3116165A1 (fr) Actionneur électromagnétique rotatif à commande manuelle et valve de frein de parking équipée d’un tel actionneur
FR3075257A1 (fr) Dispositif de reglage du calage d'une helice
US8766585B2 (en) Device for controlling an on-board apparatus
JP6878161B2 (ja) 魚釣用リール
FR3101253B1 (fr) Dispositif antichute, de préférence à rappel automatique
FR3078839A1 (fr) Machine electrique a flux axial avec longueur d’entrefer modulable
JP2006283798A (ja) 揺動型減衰装置およびそれを備えたベルトテンショナ装置

Legal Events

Date Code Title Description
PLFP Fee payment

Year of fee payment: 2

PLSC Publication of the preliminary search report

Effective date: 20201113

PLFP Fee payment

Year of fee payment: 3

PLFP Fee payment

Year of fee payment: 4

PLFP Fee payment

Year of fee payment: 5