FR3053310B1 - Aircraft airfoil comprising a hinged flap - Google Patents

Aircraft airfoil comprising a hinged flap Download PDF

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Publication number
FR3053310B1
FR3053310B1 FR1656149A FR1656149A FR3053310B1 FR 3053310 B1 FR3053310 B1 FR 3053310B1 FR 1656149 A FR1656149 A FR 1656149A FR 1656149 A FR1656149 A FR 1656149A FR 3053310 B1 FR3053310 B1 FR 3053310B1
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FR
France
Prior art keywords
shaft
rotation
shutter
profile
mobile
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
FR1656149A
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French (fr)
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FR3053310A1 (en
Inventor
Jerome Colmagro
Olivier Pautis
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
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Airbus Operations SAS
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Publication date
Application filed by Airbus Operations SAS filed Critical Airbus Operations SAS
Priority to FR1656149A priority Critical patent/FR3053310B1/en
Publication of FR3053310A1 publication Critical patent/FR3053310A1/en
Application granted granted Critical
Publication of FR3053310B1 publication Critical patent/FR3053310B1/en
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
    • B64C9/02—Mounting or supporting thereof
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/40—Arrangements for mounting power plants in aircraft
    • B64D27/402—Arrangements for mounting power plants in aircraft comprising box like supporting frames, e.g. pylons or arrangements for embracing the power plant

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Pivots And Pivotal Connections (AREA)

Abstract

La présente invention se rapporte à une partie (1) à profil aérodynamique mobile d'un aéronef comprenant au moins un profilé (2) aérodynamique présentant une zone mobile en rotation de structure simplifiée permettant de maximiser la surface mobile ainsi qu'au profilé proprement dit. Le profilé aérodynamique d'aéronef comporte un volet (16) articulé en rotation autour d'un arbre (18) en rotation ; l'arbre (18) est muni de moyens permettant de lier l'arbre (18) à au moins une nervure (20) de rigidification du carénage du volet en rotation autour de l'axe X-X de l'arbre (18). L'arbre permet de réduire le nombre d'éléments nécessaires à la fixation et à la rotation du volet. Il permet également de requérir un espace réduit pour la structure du volet et les moyens permettant son mouvement en rotation. La présente invention concerne également le procédé d'assemblage dudit profilé et de ladite partie constitutive l'intégrant.The present invention relates to a part (1) with a mobile aerodynamic profile of an aircraft comprising at least one aerodynamic profile (2) having a mobile zone in rotation of simplified structure making it possible to maximize the mobile surface as well as to the profile itself. . The aircraft airfoil comprises a flap (16) articulated in rotation around a shaft (18) in rotation; the shaft (18) is provided with means making it possible to link the shaft (18) to at least one rib (20) for stiffening the fairing of the shutter in rotation around the X-X axis of the shaft (18). The shaft makes it possible to reduce the number of elements necessary for fixing and rotating the shutter. It also makes it possible to require a reduced space for the structure of the shutter and the means allowing its movement in rotation. The present invention also relates to the method of assembling said profile and said constituent part incorporating it.

FR1656149A 2016-06-30 2016-06-30 Aircraft airfoil comprising a hinged flap Active FR3053310B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1656149A FR3053310B1 (en) 2016-06-30 2016-06-30 Aircraft airfoil comprising a hinged flap

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1656149 2016-06-30
FR1656149A FR3053310B1 (en) 2016-06-30 2016-06-30 Aircraft airfoil comprising a hinged flap

Publications (2)

Publication Number Publication Date
FR3053310A1 FR3053310A1 (en) 2018-01-05
FR3053310B1 true FR3053310B1 (en) 2021-12-24

Family

ID=56842911

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1656149A Active FR3053310B1 (en) 2016-06-30 2016-06-30 Aircraft airfoil comprising a hinged flap

Country Status (1)

Country Link
FR (1) FR3053310B1 (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3134797A1 (en) * 2022-04-26 2023-10-27 Airbus (S.A.S.) Aircraft comprising at least one flexible profile made of composite material forming at least one element among a coupling shaft of a movable surface and a movable surface
CN115258128B (en) * 2022-09-27 2022-12-02 成都市鸿侠科技有限责任公司 Reinforcing structure for processing aircraft wall panel

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB560480A (en) * 1942-11-11 1944-04-05 Blackburn Aircraft Ltd Improvements in and relating to the construction of aircraft control surfaces
GB734446A (en) * 1953-03-20 1955-08-03 Armstrong Whitworth Co Eng Operating the flaps of aircraft wings
GB0803692D0 (en) * 2008-02-29 2008-04-09 Airbus Uk Ltd Fitting for pivotally connecting aerodynamic control element to aircraft structure
DE102010024121B4 (en) * 2010-06-17 2017-04-06 Airbus Defence and Space GmbH Actuator unit
GB201209666D0 (en) * 2012-05-31 2012-07-18 Airbus Operations Ltd A hinge assembly for rotatably mounting a control surface on an aircraft

Also Published As

Publication number Publication date
FR3053310A1 (en) 2018-01-05

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