FR3047725B1 - Dispositif hypersustentateur d'aeronef equipe d'au moins un systeme d'accouplement differencie - Google Patents

Dispositif hypersustentateur d'aeronef equipe d'au moins un systeme d'accouplement differencie Download PDF

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Publication number
FR3047725B1
FR3047725B1 FR1651128A FR1651128A FR3047725B1 FR 3047725 B1 FR3047725 B1 FR 3047725B1 FR 1651128 A FR1651128 A FR 1651128A FR 1651128 A FR1651128 A FR 1651128A FR 3047725 B1 FR3047725 B1 FR 3047725B1
Authority
FR
France
Prior art keywords
hypersustent
aircraft
device equipped
coupling system
differentiated coupling
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
FR1651128A
Other languages
English (en)
Other versions
FR3047725A1 (fr
Inventor
Deniz KESKIN
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.)
Airbus Operations SAS
Original Assignee
Airbus Operations 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 Airbus Operations SAS filed Critical Airbus Operations SAS
Priority to FR1651128A priority Critical patent/FR3047725B1/fr
Priority to US15/429,809 priority patent/US10479530B2/en
Publication of FR3047725A1 publication Critical patent/FR3047725A1/fr
Application granted granted Critical
Publication of FR3047725B1 publication Critical patent/FR3047725B1/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
    • 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
    • B64F5/40—Maintaining or repairing aircraft
    • 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
    • B64F5/60—Testing or inspecting aircraft components or systems
FR1651128A 2016-02-12 2016-02-12 Dispositif hypersustentateur d'aeronef equipe d'au moins un systeme d'accouplement differencie Active FR3047725B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR1651128A FR3047725B1 (fr) 2016-02-12 2016-02-12 Dispositif hypersustentateur d'aeronef equipe d'au moins un systeme d'accouplement differencie
US15/429,809 US10479530B2 (en) 2016-02-12 2017-02-10 Aircraft high-lift device equipped with at least one differentiated coupling system

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1651128 2016-02-12
FR1651128A FR3047725B1 (fr) 2016-02-12 2016-02-12 Dispositif hypersustentateur d'aeronef equipe d'au moins un systeme d'accouplement differencie

Publications (2)

Publication Number Publication Date
FR3047725A1 FR3047725A1 (fr) 2017-08-18
FR3047725B1 true FR3047725B1 (fr) 2018-01-26

Family

ID=55953237

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1651128A Active FR3047725B1 (fr) 2016-02-12 2016-02-12 Dispositif hypersustentateur d'aeronef equipe d'au moins un systeme d'accouplement differencie

Country Status (2)

Country Link
US (1) US10479530B2 (fr)
FR (1) FR3047725B1 (fr)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20220266998A1 (en) * 2021-02-19 2022-08-25 Lilium Eaircraft Gmbh Aircraft

Family Cites Families (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3045454A (en) * 1960-11-07 1962-07-24 Sherman Klove Company Universal joint
US4180222A (en) * 1976-12-27 1979-12-25 Lockheed Aircraft Corporation Aileron segment control for a flaperon system
US4441675A (en) * 1982-06-25 1984-04-10 Mcdonnell Douglas Corporation High lift surface actuation system
DE3530865A1 (de) * 1985-08-29 1987-03-12 Messerschmitt Boelkow Blohm Antriebs- und fuehrungsvorrichtung fuer ein an einem flugzeugtragfluegel angeordnetes klappensystem
US4779822A (en) * 1986-05-23 1988-10-25 Sundstrand Corporation Actuator system
US5743490A (en) * 1996-02-16 1998-04-28 Sundstrand Corporation Flap/slat actuation system for an aircraft
GB9619488D0 (en) * 1996-09-18 1996-10-30 Dowty Boulton Paul Ltd Flight control surface actuation system
DE19724772B4 (de) * 1997-06-12 2004-02-12 Airbus Deutschland Gmbh Flexible Kupplung für die Wellen eines von einer zentralen Antriebseinheit angetriebenen Transmissionssystems in Luftfahrzeugen
DE10313728B4 (de) * 2003-03-27 2011-07-21 Airbus Operations GmbH, 21129 Klappensystem am Tragflügel eines Starrflügel-Flugzeuges
US6824099B1 (en) * 2003-07-10 2004-11-30 The Boeing Company Brake systems for aircraft wing flaps and other control surfaces
DE102007063157A1 (de) * 2007-12-30 2009-07-09 Airbus Deutschland Gmbh System zur Betätigung von zumindest einer Stellklappe eines Flugzeugs sowie ein Verfahren zur Überprüfung des Systems
DE102008052754A1 (de) * 2008-10-22 2010-05-06 Airbus Deutschland Gmbh Verstellvorrichtung zur Ankopplung an eine Verstellklappe eines Flugzeugs, fehlertolerantes Stellsystem und Verfahren zur Rekonfiguration eines Stellsystems
DE102010047540A1 (de) * 2010-10-05 2012-04-05 Airbus Operations Gmbh Hochauftriebssystem für einen Tragflügel eines Flugzeugs
US20120108349A1 (en) * 2010-10-27 2012-05-03 Guy Foley Multi-Lobed and Constant Contact Gear Mechanism
DE102011008561A1 (de) * 2011-01-14 2012-07-19 Airbus Operations Gmbh Funktionsüberwachtes Führungssystem zur Verstellung zumindest einer Systemkomponente sowie Verfahren zur Funktionsüberwachung eines solchen Führungssystems
US9422986B2 (en) * 2011-12-01 2016-08-23 Nsk Ltd. Telescopic shaft
US8910906B2 (en) * 2012-05-15 2014-12-16 Hamilton Sundstrand Corporation Articulable rotational coupling for an aircraft
US9222520B2 (en) * 2013-03-14 2015-12-29 Ashot Ashkelon Industries Ltd. Secure universal-joint
WO2015068107A1 (fr) * 2013-11-05 2015-05-14 Ashot Ashkelon Industries Ltd. Joint de cardan biseauté
GB2529447A (en) * 2014-08-20 2016-02-24 Crompton Technology Group Ltd Flexible coupling
EP3037346B1 (fr) * 2014-12-22 2018-10-24 Airbus Operations GmbH Procédé pour tester un composant dans un système hypersustentateur d'avion

Also Published As

Publication number Publication date
US10479530B2 (en) 2019-11-19
US20170233107A1 (en) 2017-08-17
FR3047725A1 (fr) 2017-08-18

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