FR2960213B1 - Systeme de levier de commande actif - Google Patents

Systeme de levier de commande actif

Info

Publication number
FR2960213B1
FR2960213B1 FR1154368A FR1154368A FR2960213B1 FR 2960213 B1 FR2960213 B1 FR 2960213B1 FR 1154368 A FR1154368 A FR 1154368A FR 1154368 A FR1154368 A FR 1154368A FR 2960213 B1 FR2960213 B1 FR 2960213B1
Authority
FR
France
Prior art keywords
control lever
active control
lever system
active
lever
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.)
Expired - Fee Related
Application number
FR1154368A
Other languages
English (en)
Other versions
FR2960213A1 (fr
Inventor
Matthias Stiefenhofer
Matthias Ludwig
Michael Rottach
Ralph Neumann
Manfred Schlosser
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.)
Liebherr Aerospace Lindenberg GmbH
Original Assignee
Liebherr Aerospace Lindenberg GmbH
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 Liebherr Aerospace Lindenberg GmbH filed Critical Liebherr Aerospace Lindenberg GmbH
Publication of FR2960213A1 publication Critical patent/FR2960213A1/fr
Application granted granted Critical
Publication of FR2960213B1 publication Critical patent/FR2960213B1/fr
Expired - Fee Related 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
    • B64C13/24—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
    • B64C13/341—Transmitting means without power amplification or where power amplification is irrelevant mechanical having duplication or stand-by provisions
    • 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
    • B64C13/343—Transmitting means without power amplification or where power amplification is irrelevant mechanical overriding of personal controls; with automatic return to inoperative position
    • 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
    • B64C13/505—Transmitting means with power amplification using electrical energy having duplication or stand-by provisions
    • 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
    • B64C13/506—Transmitting means with power amplification using electrical energy overriding of personal controls; with automatic return to inoperative position
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Automation & Control Theory (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Mechanical Control Devices (AREA)
  • Control Of Position Or Direction (AREA)
  • Feedback Control In General (AREA)
FR1154368A 2010-05-20 2011-05-19 Systeme de levier de commande actif Expired - Fee Related FR2960213B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE102010022200A DE102010022200A1 (de) 2010-05-20 2010-05-20 Steuerknüppelsystem

Publications (2)

Publication Number Publication Date
FR2960213A1 FR2960213A1 (fr) 2011-11-25
FR2960213B1 true FR2960213B1 (fr) 2016-11-18

Family

ID=44900488

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1154368A Expired - Fee Related FR2960213B1 (fr) 2010-05-20 2011-05-19 Systeme de levier de commande actif

Country Status (4)

Country Link
US (1) US20110284696A1 (fr)
DE (1) DE102010022200A1 (fr)
FR (1) FR2960213B1 (fr)
RU (1) RU2011120142A (fr)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3031959B1 (fr) * 2015-01-27 2017-02-17 Ratier Figeac Soc Procede et dispositif de conjugaison d'organes de pilotage
CA3023826A1 (fr) 2016-05-11 2017-11-16 Bombardier Inc. Procede et systeme pour afficher une entree de commande d'aeronef
DE102016014974A1 (de) * 2016-12-15 2018-06-21 Liebherr-Aerospace Lindenberg Gmbh Aktuatorsteuerung zur Steuerung von Aktuatoren eines Fluggeräts
RU2728219C1 (ru) * 2019-10-07 2020-07-28 Александр Викторович Атаманов Система для балансирного управления летательным аппаратом

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2747022C2 (de) * 1977-10-19 1985-05-15 Siemens AG, 1000 Berlin und 8000 München Schaltungsanordnung für den elektrischen Direktantrieb einer rotierenden Trennvorrichtung
US5209661A (en) * 1990-10-29 1993-05-11 Systems Control Technology, Inc. Motor control desired dynamic load of a simulating system and method
EP0601000B1 (fr) * 1991-08-28 1997-01-29 United Technologies Corporation Systeme de commande verticale pour aeronef a voilure tournante
US5264768A (en) * 1992-10-06 1993-11-23 Honeywell, Inc. Active hand controller feedback loop
US5347204A (en) * 1992-10-06 1994-09-13 Honeywell Inc. Position dependent rate dampening in any active hand controller
US5694014A (en) * 1995-08-22 1997-12-02 Honeywell Inc. Active hand controller redundancy and architecture
US5828197A (en) * 1996-10-25 1998-10-27 Immersion Human Interface Corporation Mechanical interface having multiple grounded actuators
US6459228B1 (en) * 2001-03-22 2002-10-01 Mpc Products Corporation Dual input servo coupled control sticks
US7108232B2 (en) * 2004-02-05 2006-09-19 Hoh Roger H Helicopter force-feel and stability augmentation system with parallel servo-actuator
EP1977292A2 (fr) * 2006-01-17 2008-10-08 Gulfstream Aerospace Corporation Système et procédé associés à un système de commande de secours intégré
US7750593B2 (en) * 2006-10-26 2010-07-06 Honeywell International Inc. Active human-machine interface system without a force sensor
US20080156939A1 (en) * 2007-01-03 2008-07-03 Honeywell International, Inc. Active pilot flight control stick system with passive electromagnetic feedback

Also Published As

Publication number Publication date
DE102010022200A1 (de) 2011-11-24
RU2011120142A (ru) 2012-11-27
FR2960213A1 (fr) 2011-11-25
US20110284696A1 (en) 2011-11-24

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