FR2997922B1 - DEVICE FOR ADJUSTING SHUTTERS OF AIRCRAFT SURFACES - Google Patents

DEVICE FOR ADJUSTING SHUTTERS OF AIRCRAFT SURFACES Download PDF

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Publication number
FR2997922B1
FR2997922B1 FR1359932A FR1359932A FR2997922B1 FR 2997922 B1 FR2997922 B1 FR 2997922B1 FR 1359932 A FR1359932 A FR 1359932A FR 1359932 A FR1359932 A FR 1359932A FR 2997922 B1 FR2997922 B1 FR 2997922B1
Authority
FR
France
Prior art keywords
aircraft surfaces
adjusting shutters
shutters
adjusting
aircraft
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
FR1359932A
Other languages
French (fr)
Other versions
FR2997922A1 (en
Inventor
Tobias Hartmann
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 FR2997922A1 publication Critical patent/FR2997922A1/en
Application granted granted Critical
Publication of FR2997922B1 publication Critical patent/FR2997922B1/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
FR1359932A 2012-11-14 2013-10-14 DEVICE FOR ADJUSTING SHUTTERS OF AIRCRAFT SURFACES Active FR2997922B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102012022287.4 2012-11-14
DE201210022287 DE102012022287A1 (en) 2012-11-14 2012-11-14 Device for adjusting flaps of wings of aircraft, has damper actuators that are driven using drive shaft for adjusting flaps so that wings of each flap is adjusted

Publications (2)

Publication Number Publication Date
FR2997922A1 FR2997922A1 (en) 2014-05-16
FR2997922B1 true FR2997922B1 (en) 2018-03-23

Family

ID=50555506

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1359932A Active FR2997922B1 (en) 2012-11-14 2013-10-14 DEVICE FOR ADJUSTING SHUTTERS OF AIRCRAFT SURFACES

Country Status (2)

Country Link
DE (1) DE102012022287A1 (en)
FR (1) FR2997922B1 (en)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102015201935B4 (en) * 2015-02-04 2022-08-04 Zf Friedrichshafen Ag Arrangement for controlling flaps on the wings of an aircraft
DE102018117759A1 (en) * 2018-07-23 2020-01-23 Liebherr-Aerospace Lindenberg Gmbh High-lift system for an aircraft
CN110877714A (en) * 2018-09-04 2020-03-13 庞巴迪公司 High lift actuation system with clutch architecture
US10773795B2 (en) * 2018-09-24 2020-09-15 The Boeing Company Distributed linear hydraulic high lift actuation system with synchronization members
US11608161B2 (en) 2020-04-08 2023-03-21 The Boeing Company Flap actuation systems and related methods
CN111516857A (en) * 2020-04-30 2020-08-11 庆安集团有限公司 Flap distributed driving system

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE4033277A1 (en) * 1990-10-19 1992-04-23 Airbus Gmbh DRIVING DEVICE FOR FLAPS ARRANGED ON AIRCRAFT WINGS
US20040200928A1 (en) * 2003-04-14 2004-10-14 Arthur Degenholtz Actuator and flap arrangement with actuator interconnection
DE10361891A1 (en) 2003-12-23 2005-08-04 Airbus Deutschland Gmbh Device for controlling and adjusting flaps on aircraft wings
US7494094B2 (en) 2004-09-08 2009-02-24 The Boeing Company Aircraft wing systems for providing differential motion to deployable lift devices
DE102007021748B4 (en) * 2007-05-09 2019-12-12 Liebherr-Aerospace Lindenberg Gmbh Drive system for a vault-variable aircraft wing
DE102010044678A1 (en) * 2010-09-08 2012-03-08 Airbus Operations Gmbh Monitoring system for a control system of an aircraft, control system and method for reconfiguration of the control system
DE102010047512A1 (en) * 2010-10-05 2012-04-05 Airbus Operations Gmbh High-lift system for an aircraft with two separate drive units

Also Published As

Publication number Publication date
FR2997922A1 (en) 2014-05-16
DE102012022287A1 (en) 2014-05-15

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