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FR3014412B1 - DEVICE FOR ADJUSTING SHUTTERS OF AIRCRAFT SURFACES - Google Patents

DEVICE FOR ADJUSTING SHUTTERS OF AIRCRAFT SURFACES Download PDF

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Publication number
FR3014412B1
FR3014412B1 FR1461682A FR1461682A FR3014412B1 FR 3014412 B1 FR3014412 B1 FR 3014412B1 FR 1461682 A FR1461682 A FR 1461682A FR 1461682 A FR1461682 A FR 1461682A FR 3014412 B1 FR3014412 B1 FR 3014412B1
Authority
FR
France
Prior art keywords
drive shaft
adjusting
aircraft surfaces
drive
flaps
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
FR1461682A
Other languages
French (fr)
Other versions
FR3014412A1 (en
Inventor
Bernhard Hauber
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 FR3014412A1 publication Critical patent/FR3014412A1/en
Application granted granted Critical
Publication of FR3014412B1 publication Critical patent/FR3014412B1/en
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
    • B64C13/24—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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/14—Adjustable control surfaces or members, e.g. rudders forming slots
    • B64C9/16—Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/40—Weight reduction

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Automation & Control Theory (AREA)
  • Transmission Devices (AREA)
  • Shutters For Cameras (AREA)

Abstract

L'invention concerne un dispositif d'ajustement de volets (10, 20) de surfaces portantes d'aéronefs. Le dispositif comprend des entraînements de volet (40) pour l'ajustement des volets (10, 20) ainsi qu'au moins un arbre d'entraînement (50) relié de telle sorte aux entraînements de volet (40) que ceux-ci peuvent être entraînés par l'arbre d'entraînement (50), une unité d'entraînement (110, 112) pour l'entraînement de l'arbre d'entraînement (50) ou des arbres d'entraînement (50, 50') étant prévue dans chacune des surfaces portantes, et un frein central (60) agissant sur le ou les arbres d'entraînement (50) étant disposé entre les surfaces portantes.The invention relates to a device for adjusting flaps (10, 20) of aircraft carrying surfaces. The device comprises flap drives (40) for adjusting the flaps (10, 20) and at least one drive shaft (50) connected in such a way to the flap drives (40) that they can be driven by the drive shaft (50), a drive unit (110, 112) for driving the drive shaft (50) or drive shafts (50, 50') being provided in each of the bearing surfaces, and a central brake (60) acting on the drive shaft(s) (50) being disposed between the bearing surfaces.

FR1461682A 2013-12-05 2014-11-28 DEVICE FOR ADJUSTING SHUTTERS OF AIRCRAFT SURFACES Active FR3014412B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102013020158.6A DE102013020158B4 (en) 2013-12-05 2013-12-05 Device for adjusting flaps on aircraft wings
DE102013020158.6 2013-12-05

Publications (2)

Publication Number Publication Date
FR3014412A1 FR3014412A1 (en) 2015-06-12
FR3014412B1 true FR3014412B1 (en) 2018-06-08

Family

ID=53184806

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1461682A Active FR3014412B1 (en) 2013-12-05 2014-11-28 DEVICE FOR ADJUSTING SHUTTERS OF AIRCRAFT SURFACES

Country Status (2)

Country Link
DE (1) DE102013020158B4 (en)
FR (1) FR3014412B1 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2548622A (en) * 2016-03-24 2017-09-27 Goodrich Actuation Systems Ltd Splined couplings

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE10361891A1 (en) 2003-12-23 2005-08-04 Airbus Deutschland Gmbh Device for controlling and adjusting flaps on aircraft wings
DE102007021748B4 (en) * 2007-05-09 2019-12-12 Liebherr-Aerospace Lindenberg Gmbh Drive system for a vault-variable aircraft wing
DE102008022092A1 (en) * 2008-05-05 2009-11-19 Airbus Deutschland Gmbh Fault-tolerant control system for adjusting the flaps of an aircraft with adjustable kinematics with a fixed axis of rotation
DE102010047512A1 (en) * 2010-10-05 2012-04-05 Airbus Operations Gmbh High-lift system for an aircraft with two separate drive units
DE102011016336A1 (en) * 2011-04-07 2012-10-11 Airbus Operations Gmbh High-lift system for an aircraft
DE102011117706B4 (en) * 2011-11-04 2023-07-06 Liebherr-Aerospace Lindenberg Gmbh Drive system for flaps and/or slats of an aircraft

Also Published As

Publication number Publication date
DE102013020158B4 (en) 2024-02-01
FR3014412A1 (en) 2015-06-12
DE102013020158A1 (en) 2015-06-11

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