FR3105171B1 - Dispositif d’application d’effort pour un manche de pilotage d’un aéronef et procédé d’utilisation d’un tel manche - Google Patents

Dispositif d’application d’effort pour un manche de pilotage d’un aéronef et procédé d’utilisation d’un tel manche Download PDF

Info

Publication number
FR3105171B1
FR3105171B1 FR1915211A FR1915211A FR3105171B1 FR 3105171 B1 FR3105171 B1 FR 3105171B1 FR 1915211 A FR1915211 A FR 1915211A FR 1915211 A FR1915211 A FR 1915211A FR 3105171 B1 FR3105171 B1 FR 3105171B1
Authority
FR
France
Prior art keywords
shaft
stick
application device
force application
force
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
FR1915211A
Other languages
English (en)
Other versions
FR3105171A1 (fr
Inventor
Yvon Joncour
Rémi-Louis Lawniczak
Philippe Bezivin
Clément Guillon
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 FR1915211A priority Critical patent/FR3105171B1/fr
Priority to US17/757,625 priority patent/US20230028481A1/en
Priority to PCT/EP2020/083962 priority patent/WO2021121939A1/fr
Publication of FR3105171A1 publication Critical patent/FR3105171A1/fr
Application granted granted Critical
Publication of FR3105171B1 publication Critical patent/FR3105171B1/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
    • 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
    • B64C13/10—Initiating means actuated personally comprising warning devices
    • 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)
  • Braking Arrangements (AREA)
  • Mechanical Control Devices (AREA)

Abstract

Un dispositif d’application d’effort (D) pour un manche de pilotage (M) d’un aéronef, le manche de pilotage (M) comprenant un levier (1) de commande configuré pour entraîner en rotation un premier arbre (A1) et un deuxième arbre (B1), le dispositif d’application d’effort (D) comprenant un premier organe de retour d’effort (31) configuré pour exercer un effort résistif s’opposant à la rotation du premier arbre (A1), un deuxième organe de retour d’effort (32) configuré pour exercer un effort résistif s’opposant à la rotation du deuxième arbre (B1) et un dispositif de freinage commun (5) comportant un carter (50), un premier organe de freinage (51) et un deuxième organe de freinage (52) coaxiaux qui sont montés rotatifs dans le carter (50) et configurés pour coopérer respectivement avec le premier arbre (A1) et le deuxième arbre (B1) de manière à les freiner, de préférence, simultanément. Figure de l’abrégé : Figure 2
FR1915211A 2019-12-20 2019-12-20 Dispositif d’application d’effort pour un manche de pilotage d’un aéronef et procédé d’utilisation d’un tel manche Active FR3105171B1 (fr)

Priority Applications (3)

Application Number Priority Date Filing Date Title
FR1915211A FR3105171B1 (fr) 2019-12-20 2019-12-20 Dispositif d’application d’effort pour un manche de pilotage d’un aéronef et procédé d’utilisation d’un tel manche
US17/757,625 US20230028481A1 (en) 2019-12-20 2020-11-30 Force application device for an aircraft control column and method for using such a control column
PCT/EP2020/083962 WO2021121939A1 (fr) 2019-12-20 2020-11-30 Dispositif d'application d'effort pour un manche de pilotage d'un aéronef et procédé d'utilisation d'un tel manche

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1915211 2019-12-20
FR1915211A FR3105171B1 (fr) 2019-12-20 2019-12-20 Dispositif d’application d’effort pour un manche de pilotage d’un aéronef et procédé d’utilisation d’un tel manche

Publications (2)

Publication Number Publication Date
FR3105171A1 FR3105171A1 (fr) 2021-06-25
FR3105171B1 true FR3105171B1 (fr) 2022-04-15

Family

ID=70154581

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1915211A Active FR3105171B1 (fr) 2019-12-20 2019-12-20 Dispositif d’application d’effort pour un manche de pilotage d’un aéronef et procédé d’utilisation d’un tel manche

Country Status (3)

Country Link
US (1) US20230028481A1 (fr)
FR (1) FR3105171B1 (fr)
WO (1) WO2021121939A1 (fr)

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2647922B1 (fr) * 1989-05-31 1993-12-31 Sextant Avionique Dispositif de commande electromecanique utilisable pour le pilotage d'un vehicule
US6437771B1 (en) * 1995-01-18 2002-08-20 Immersion Corporation Force feedback device including flexure member between actuator and user object
WO1998033136A1 (fr) * 1997-01-27 1998-07-30 Immersion Human Interface Corporation Procede et appareil incluant un actionneur perfectionne procurant un retour d'effort bande large et realiste
US7888901B2 (en) * 2006-11-15 2011-02-15 Honeywell International Inc. Active human-machine interface system including an electrically controllable damper
FR3011815B1 (fr) 2013-10-15 2016-01-08 Sagem Defense Securite Dispositif de commande de vol d'un aeronef
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

Also Published As

Publication number Publication date
FR3105171A1 (fr) 2021-06-25
US20230028481A1 (en) 2023-01-26
WO2021121939A1 (fr) 2021-06-24

Similar Documents

Publication Publication Date Title
US2423191A (en) Control apparatus for variable pitch propeller adjusting devices
FR3086076B1 (fr) Dispositif d'application d'effort pour un mini-manche actif
US9656745B2 (en) Magnetorheological actuator with torsional spring
FR3102459B1 (fr) Dispositif d’application d’effort pour manche de pilotage en situation de manque de courant
CA2500842C (fr) Systeme de pilotage longitudinal d'un aeronef roulant sur le sol
FR2728537A1 (fr) Dispositif pour l'actionnement d'un organe commande pour un aeronef, tel que notamment un helicoptere, a commandes de vol electriques
FR3105171B1 (fr) Dispositif d’application d’effort pour un manche de pilotage d’un aéronef et procédé d’utilisation d’un tel manche
US2874787A (en) Air driven power unit
US9656746B2 (en) Magnetorheological haptic trim actuator
US10611472B2 (en) Coaxial rotor yaw control
KR101531572B1 (ko) 기계식 통합 조종간을 구비한 회전익기
FR3086711B1 (fr) Organe de transmission de force assemble et mecanisme a double embrayage humide comprenant ledit organe
US2661169A (en) Aircraft control stick force linkage
FR3072079B1 (fr) Dispositif de generation, par friction, de sensation d'efforts pour un systeme de commande de vol d'un aeronef
EP4080318A1 (fr) Dispositif de commande d'un ensemble de réduction d énergie mécanique d'un aéronef et procédé associé
US9643719B2 (en) Electro-rheological elastomeric, variable-stiffness flight control device
US2857775A (en) Holding brake for reversible screw jack
US2960167A (en) Engine control
CN107709156A (zh) 用于控制涡轮螺旋桨发动机的具有可变倾角叶片的螺旋桨的设备
FR3086273B1 (fr) Dispositif de commande de vol d’un aeronef
US2962258A (en) Slotted vane turbine governor
CN204312433U (zh) 先导控制阀
Domaszuk The application of positive pressure breathing for improving+ Gz acceleration tolerance.
US3802118A (en) Model airplane control line load regulating system
FR3060528B1 (fr) Dispositif de commande des surfaces mobiles et d'une roue directrice d'un aeronef

Legal Events

Date Code Title Description
PLFP Fee payment

Year of fee payment: 2

PLSC Publication of the preliminary search report

Effective date: 20210625

PLFP Fee payment

Year of fee payment: 3

PLFP Fee payment

Year of fee payment: 4

PLFP Fee payment

Year of fee payment: 5