BR112022007683A2 - Dispositivo de aplicação de força para manche em uma situação de falha de energia - Google Patents

Dispositivo de aplicação de força para manche em uma situação de falha de energia

Info

Publication number
BR112022007683A2
BR112022007683A2 BR112022007683A BR112022007683A BR112022007683A2 BR 112022007683 A2 BR112022007683 A2 BR 112022007683A2 BR 112022007683 A BR112022007683 A BR 112022007683A BR 112022007683 A BR112022007683 A BR 112022007683A BR 112022007683 A2 BR112022007683 A2 BR 112022007683A2
Authority
BR
Brazil
Prior art keywords
rod
application device
power
magnetic
failure situation
Prior art date
Application number
BR112022007683A
Other languages
English (en)
Other versions
BR112022007683B1 (pt
Inventor
Lawniczak Remi-Louis
Coppée Pascal
Attrazic Yannick
Original Assignee
Safran Electronics & Defense
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 & Defense filed Critical Safran Electronics & Defense
Publication of BR112022007683A2 publication Critical patent/BR112022007683A2/pt
Publication of BR112022007683B1 publication Critical patent/BR112022007683B1/pt

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
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Automation & Control Theory (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Mechanical Engineering (AREA)
  • Braking Arrangements (AREA)
  • Mechanical Control Devices (AREA)
  • Position Input By Displaying (AREA)

Abstract

DISPOSITIVO DE APLICAÇÃO DE FORÇA PARA MANCHE EM UMA SITUAÇÃO DE FALHA DE ENERGIA. A presente invenção refere-se a um dispositivo de aplicação de força para um manche de uma aeronave que compreende uma haste e uma alavanca de controle configurada para rotacionar a haste em torno de um primeiro eixo geométrico, em que o dispositivo compreende: um freio magnético que compreende uma parte de frenagem configurada para ser conectada à haste e um volume que contém um fluido reológico em contato com a parte de frenagem, de resistência ao cisalhamento variável como uma função de um campo magnético aplicada ao fluido reológico, um motor de retroalimentação de força configurado para exercer uma força resistiva em oposição à rotação da haste em torno do primeiro eixo geométrico, uma fonte de energia de motor, um elemento magnético móvel polarizado em direção a uma posição próxima ao freio magnético e meios de distanciamento configurados para manter o elemento magnético móvel em uma posição na direção contrária do freio magnético, quando tais meios de distanciamento são alimentados pela fonte de energia.
BR112022007683-5A 2019-10-23 2020-10-23 Dispositivo de aplicação de força para manche de aeronave, manche ativo de aeronave e uso do dispositivo BR112022007683B1 (pt)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FRFR1911882 2019-10-23
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

Publications (2)

Publication Number Publication Date
BR112022007683A2 true BR112022007683A2 (pt) 2022-07-12
BR112022007683B1 BR112022007683B1 (pt) 2023-01-10

Family

ID=69572114

Family Applications (1)

Application Number Title Priority Date Filing Date
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

Country Status (6)

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

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
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
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 (en) * 2008-03-27 2019-05-08 Lakeview Innovation Ltd. Dual differential semi-active actuator fit for interaction tasks and fast motion
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
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
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
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
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

Also Published As

Publication number Publication date
US11628925B2 (en) 2023-04-18
FR3102459A1 (fr) 2021-04-30
SE545108C2 (en) 2023-04-04
CA3155200A1 (fr) 2021-04-29
SE2250478A1 (en) 2022-04-21
FR3102459B1 (fr) 2021-09-24
WO2021079075A1 (fr) 2021-04-29
BR112022007683B1 (pt) 2023-01-10
CA3155200C (fr) 2023-06-27
US20220348310A1 (en) 2022-11-03

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Legal Events

Date Code Title Description
B09A Decision: intention to grant [chapter 9.1 patent gazette]
B16A Patent or certificate of addition of invention granted [chapter 16.1 patent gazette]

Free format text: PRAZO DE VALIDADE: 20 (VINTE) ANOS CONTADOS A PARTIR DE 23/10/2020, OBSERVADAS AS CONDICOES LEGAIS