FR3123630B1 - Système de commande de compensateur de vol pour aéronef à retour haptique - Google Patents

Système de commande de compensateur de vol pour aéronef à retour haptique Download PDF

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Publication number
FR3123630B1
FR3123630B1 FR2105919A FR2105919A FR3123630B1 FR 3123630 B1 FR3123630 B1 FR 3123630B1 FR 2105919 A FR2105919 A FR 2105919A FR 2105919 A FR2105919 A FR 2105919A FR 3123630 B1 FR3123630 B1 FR 3123630B1
Authority
FR
France
Prior art keywords
control system
aircraft flight
trim control
haptic feedback
flight trim
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
FR2105919A
Other languages
English (en)
Other versions
FR3123630A1 (fr
Inventor
Remi-Louis Lawniczak
Christophe Bastide
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 FR2105919A priority Critical patent/FR3123630B1/fr
Priority to US18/566,023 priority patent/US12459636B2/en
Priority to PCT/FR2022/051063 priority patent/WO2022254162A1/fr
Priority to EP22735207.7A priority patent/EP4347396A1/fr
Publication of FR3123630A1 publication Critical patent/FR3123630A1/fr
Application granted granted Critical
Publication of FR3123630B1 publication Critical patent/FR3123630B1/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
    • B64C13/24—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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/54—Mechanisms for controlling blade adjustment or movement relative to rotor head, e.g. lag-lead movement
    • B64C27/56—Mechanisms for controlling blade adjustment or movement relative to rotor head, e.g. lag-lead movement characterised by the control initiating means, e.g. manually actuated
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/54—Mechanisms for controlling blade adjustment or movement relative to rotor head, e.g. lag-lead movement
    • B64C27/58—Transmitting means, e.g. interrelated with initiating means or means acting on blades
    • B64C27/68—Transmitting means, e.g. interrelated with initiating means or means acting on blades using electrical energy, e.g. having electrical power amplification
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/04—Helicopters

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Automation & Control Theory (AREA)
  • Mechanical Engineering (AREA)
  • Mechanical Control Devices (AREA)
  • Control Of Electric Motors In General (AREA)
  • Hydraulic Clutches, Magnetic Clutches, Fluid Clutches, And Fluid Joints (AREA)

Abstract

Ce système de commande de compensateur de vol d’aéronef comprend un moteur (3) et un actionneur (6) à friction variable couplé au moteur et à un arbre de sortie (8). L’actionneur à friction variable comprenant un embrayage magnétique à couple de friction variable lié à l’arbre de sortie Figure pour l’abrégé : Fig 1
FR2105919A 2021-06-04 2021-06-04 Système de commande de compensateur de vol pour aéronef à retour haptique Active FR3123630B1 (fr)

Priority Applications (4)

Application Number Priority Date Filing Date Title
FR2105919A FR3123630B1 (fr) 2021-06-04 2021-06-04 Système de commande de compensateur de vol pour aéronef à retour haptique
US18/566,023 US12459636B2 (en) 2021-06-04 2022-06-03 Flight compensator control system for aircraft with haptic feedback
PCT/FR2022/051063 WO2022254162A1 (fr) 2021-06-04 2022-06-03 Système de commande de compensateur de vol pour aéronef à retour haptique
EP22735207.7A EP4347396A1 (fr) 2021-06-04 2022-06-03 Système de commande de compensateur de vol pour aéronef à retour haptique

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR2105919 2021-06-04
FR2105919A FR3123630B1 (fr) 2021-06-04 2021-06-04 Système de commande de compensateur de vol pour aéronef à retour haptique

Publications (2)

Publication Number Publication Date
FR3123630A1 FR3123630A1 (fr) 2022-12-09
FR3123630B1 true FR3123630B1 (fr) 2025-06-27

Family

ID=76920948

Family Applications (1)

Application Number Title Priority Date Filing Date
FR2105919A Active FR3123630B1 (fr) 2021-06-04 2021-06-04 Système de commande de compensateur de vol pour aéronef à retour haptique

Country Status (4)

Country Link
US (1) US12459636B2 (fr)
EP (1) EP4347396A1 (fr)
FR (1) FR3123630B1 (fr)
WO (1) WO2022254162A1 (fr)

Family Cites Families (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2736518A (en) * 1952-07-29 1956-02-28 Northrop Aircraft Inc Aircraft trim and artificial feel system
GB763506A (en) * 1953-06-30 1956-12-12 Bendix Aviat Corp Monitoring apparatus for automatic pilot systems
US4228386A (en) * 1978-06-02 1980-10-14 Sperry Corporation Aircraft servoactuator apparatus
US4345195A (en) * 1979-12-13 1982-08-17 Sperry Corporation Strapdown multifunction servoactuator apparatus for aircraft
US4426607A (en) * 1982-03-12 1984-01-17 Sperry Corporation Differential linkage apparatus for an aircraft series servoactuator apparatus
US4717098A (en) * 1986-05-19 1988-01-05 Mcdonnell Douglas Corporation Actuator for a g-limiter override
US20030183728A1 (en) * 2002-03-29 2003-10-02 The Boeing Company Aircraft control surface controller and associated method
US7044024B1 (en) * 2003-05-12 2006-05-16 Trutrak Flight Systems, Inc. Apparatus and method for servo control of an aircraft
FR2970697B1 (fr) * 2011-01-24 2015-11-20 Sagem Defense Securite Dispositif d'actionnement d'un equipement pilotable automatiquement ou manuellement avec detection de la reprise du pilotage manuel
FR3025493B1 (fr) * 2014-09-09 2016-11-25 Sagem Defense Securite Dispositif de manche de commande de vol d'aeronef a retour d'effort avec voie de secours
US9656745B2 (en) * 2015-01-30 2017-05-23 Bell Helicopter Textron Inc. Magnetorheological actuator with torsional spring
US10106245B2 (en) * 2015-10-19 2018-10-23 Honeywell International Inc. Automatic flight control actuator systems
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
US10030756B2 (en) * 2016-06-02 2018-07-24 Honeywell International Inc. Automatic flight control actuator systems
GB2552373A (en) * 2016-07-22 2018-01-24 Bae Systems Plc Control systems and methods
FR3086076B1 (fr) * 2018-09-13 2021-07-30 Safran Electronics & Defense Dispositif d'application d'effort pour un mini-manche actif
FR3095804B1 (fr) * 2019-05-06 2021-09-24 Safran Electronics & Defense Dispositif d’application d’effort pour manche de pilotage
FR3102459B1 (fr) * 2019-10-23 2021-09-24 Safran Electronics & Defense Dispositif d’application d’effort pour manche de pilotage en situation de manque de courant
US11518497B2 (en) * 2020-07-15 2022-12-06 Beta Air, Llc Hover and thrust control assembly for dual-mode aircraft
US11560225B2 (en) * 2020-07-15 2023-01-24 Beta Air, Llc Hover and thrust control assembly for dual-mode aircraft

Also Published As

Publication number Publication date
FR3123630A1 (fr) 2022-12-09
US20240246660A1 (en) 2024-07-25
EP4347396A1 (fr) 2024-04-10
WO2022254162A1 (fr) 2022-12-08
US12459636B2 (en) 2025-11-04

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