FR3102459B1 - Dispositif d’application d’effort pour manche de pilotage en situation de manque de courant - Google Patents

Dispositif d’application d’effort pour manche de pilotage en situation de manque de courant Download PDF

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Publication number
FR3102459B1
FR3102459B1 FR1911882A FR1911882A FR3102459B1 FR 3102459 B1 FR3102459 B1 FR 3102459B1 FR 1911882 A FR1911882 A FR 1911882A FR 1911882 A FR1911882 A FR 1911882A FR 3102459 B1 FR3102459 B1 FR 3102459B1
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FR
France
Prior art keywords
shaft
force
magnetic
current source
lack
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
FR1911882A
Other languages
English (en)
Other versions
FR3102459A1 (fr
Inventor
Remi-Louis Lawniczak
Pascal Coppée
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 FR1911882A priority Critical patent/FR3102459B1/fr
Priority to PCT/FR2020/051919 priority patent/WO2021079075A1/fr
Priority to US17/771,188 priority patent/US11628925B2/en
Priority to BR112022007683-5A priority patent/BR112022007683B1/pt
Priority to CA3155200A priority patent/CA3155200C/fr
Priority to SE2250478A priority patent/SE545108C2/en
Publication of FR3102459A1 publication Critical patent/FR3102459A1/fr
Application granted granted Critical
Publication of FR3102459B1 publication Critical patent/FR3102459B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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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
    • 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
    • B64C13/26—Transmitting means without power amplification or where power amplification is irrelevant
    • B64C13/28—Transmitting means without power amplification or where power amplification is irrelevant mechanical
    • B64C13/345—Transmitting means without power amplification or where power amplification is irrelevant mechanical with artificial feel
    • 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
    • G05G5/00—Means for preventing, limiting or returning the movements of parts of a control mechanism, e.g. locking controlling member
    • G05G5/03—Means for enhancing the operator's awareness of arrival of the controlling member at a command or datum position; Providing feel, e.g. means for creating a 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
    • 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

Abstract

La présente invention concerne un dispositif d’application d’effort pour un manche de pilotage d’un aéronef comprenant un arbre et un levier de commande configuré pour entraîner en rotation l’arbre autour d’un premier axe, le dispositif comprenant :- un frein magnétique comportant une pièce de freinage reliée à l’arbre, et un volume contenant un fluide rhéologique en contact avec la pièce de freinage, de résistance au cisaillement variable en fonction d’un champ magnétique appliqué au fluide rhéologique,- un moteur de retour d’effort configuré pour exercer un effort résistif s’opposant à la rotation de l’arbre autour du premier axe, - une source de courant du moteur de retour d’effort,- un élément magnétique mobile sollicité vers une position rapprochée du frein magnétique,- des moyens d’éloignement configurés pour maintenir l’élément magnétique mobile en position éloignée du frein magnétique, quand ces moyens d’éloignement sont alimentés par la source de courant. Figure pour l’abrégé : Fig. 5a
FR1911882A 2019-10-23 2019-10-23 Dispositif d’application d’effort pour manche de pilotage en situation de manque de courant Active FR3102459B1 (fr)

Priority Applications (6)

Application Number Priority Date Filing Date Title
FR1911882A FR3102459B1 (fr) 2019-10-23 2019-10-23 Dispositif d’application d’effort pour manche de pilotage en situation de manque de courant
PCT/FR2020/051919 WO2021079075A1 (fr) 2019-10-23 2020-10-23 Dispositif d'application d'effort pour manche de pilotage en situation de manque de courant
US17/771,188 US11628925B2 (en) 2019-10-23 2020-10-23 Force application device for control stick in a power failure situation
BR112022007683-5A BR112022007683B1 (pt) 2019-10-23 2020-10-23 Dispositivo de aplicação de força para manche de aeronave, manche ativo de aeronave e uso do dispositivo
CA3155200A CA3155200C (fr) 2019-10-23 2020-10-23 Dispositif d'application d'effort pour manche de pilotage en situation de manque de courant
SE2250478A SE545108C2 (en) 2019-10-23 2020-10-23 Force application device for control stick in a power failure situation

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1911882A FR3102459B1 (fr) 2019-10-23 2019-10-23 Dispositif d’application d’effort pour manche de pilotage en situation de manque de courant
FR1911882 2019-10-23

Publications (2)

Publication Number Publication Date
FR3102459A1 FR3102459A1 (fr) 2021-04-30
FR3102459B1 true FR3102459B1 (fr) 2021-09-24

Family

ID=69572114

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1911882A Active FR3102459B1 (fr) 2019-10-23 2019-10-23 Dispositif d’application d’effort pour manche de pilotage en situation de manque de courant

Country Status (6)

Country Link
US (1) US11628925B2 (fr)
BR (1) BR112022007683B1 (fr)
CA (1) CA3155200C (fr)
FR (1) FR3102459B1 (fr)
SE (1) SE545108C2 (fr)
WO (1) WO2021079075A1 (fr)

Families Citing this family (5)

* 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
FR3091260B1 (fr) * 2018-12-28 2020-12-25 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
FR3128940B1 (fr) * 2021-11-08 2023-09-29 Safran Electronics & Defense Dispositif d’application d’effort de manche de pilotage, manche, procédé , programme et aéronef
CN114776754A (zh) * 2022-04-27 2022-07-22 西安交通大学 一种变位移式磁流体可变阻尼旋转关节

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4106728A (en) * 1977-01-17 1978-08-15 Sperry Rand Corporation Fail safe force feel system
US5721566A (en) * 1995-01-18 1998-02-24 Immersion Human Interface Corp. Method and apparatus for providing damping force feedback
US7888901B2 (en) * 2006-11-15 2011-02-15 Honeywell International Inc. Active human-machine interface system including an electrically controllable damper
EP2881224B1 (fr) * 2008-03-27 2019-05-08 Lakeview Innovation Ltd. Actionneur semi-actif à double différentiel adapté pour des tâches d'interaction et un mouvement rapide
FR3011815B1 (fr) 2013-10-15 2016-01-08 Sagem Defense Securite Dispositif de commande de vol d'un aeronef
US9656746B2 (en) * 2014-01-31 2017-05-23 Bell Helicopter Textron Inc. Magnetorheological haptic trim actuator
FR3056315B1 (fr) * 2016-09-21 2018-09-28 Commissariat A L'energie Atomique Et Aux Energies Alternatives Interface haptique a au moins deux degres de liberte presentant un ressenti haptique ameliore
FR3056202B1 (fr) * 2016-09-21 2020-12-11 Commissariat Energie Atomique Poste de commande pour nacelles elevatrices et nacelle elevatrice comportant un tel poste de commande
US10074245B2 (en) * 2017-01-10 2018-09-11 Woodward, Inc. Force feel using a brushless DC motor
FR3086076B1 (fr) * 2018-09-13 2021-07-30 Safran Electronics & Defense Dispositif d'application d'effort pour un mini-manche actif
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
FR3091260B1 (fr) * 2018-12-28 2020-12-25 Safran Electronics & Defense Dispositif d’application d’effort pour un manche de pilotage d’un aéronef

Also Published As

Publication number Publication date
BR112022007683A2 (pt) 2022-07-12
CA3155200C (fr) 2023-06-27
FR3102459A1 (fr) 2021-04-30
US11628925B2 (en) 2023-04-18
BR112022007683B1 (pt) 2023-01-10
SE2250478A1 (en) 2022-04-21
US20220348310A1 (en) 2022-11-03
SE545108C2 (en) 2023-04-04
CA3155200A1 (fr) 2021-04-29
WO2021079075A1 (fr) 2021-04-29

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