FR2454406B1 - - Google Patents

Info

Publication number
FR2454406B1
FR2454406B1 FR8005572A FR8005572A FR2454406B1 FR 2454406 B1 FR2454406 B1 FR 2454406B1 FR 8005572 A FR8005572 A FR 8005572A FR 8005572 A FR8005572 A FR 8005572A FR 2454406 B1 FR2454406 B1 FR 2454406B1
Authority
FR
France
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
Application number
FR8005572A
Other versions
FR2454406A1 (fr
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.)
Vereinigte Flugtechnische Werke GmbH
Vereinigte Flugtechnische Werke Fokker GmbH
Original Assignee
Vereinigte Flugtechnische Werke GmbH
Vereinigte Flugtechnische Werke Fokker 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 Vereinigte Flugtechnische Werke GmbH, Vereinigte Flugtechnische Werke Fokker GmbH filed Critical Vereinigte Flugtechnische Werke GmbH
Publication of FR2454406A1 publication Critical patent/FR2454406A1/fr
Application granted granted Critical
Publication of FR2454406B1 publication Critical patent/FR2454406B1/fr
Granted legal-status Critical Current

Links

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
    • B64C9/22—Adjustable control surfaces or members, e.g. rudders forming slots at the front of the wing
    • B64C9/24—Adjustable control surfaces or members, e.g. rudders forming slots at the front of the wing by single flap

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Transmission Devices (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Toys (AREA)
  • Transmissions By Endless Flexible Members (AREA)
  • Retarders (AREA)
  • Mechanically-Actuated Valves (AREA)
FR8005572A 1979-04-20 1980-03-12 Avion a ailes portantes muni de parties avant mobiles Granted FR2454406A1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE2916040A DE2916040C2 (de) 1979-04-20 1979-04-20 Tragflügel für ein Luftfahrzeug mit beweglichen Vorflügeln

Publications (2)

Publication Number Publication Date
FR2454406A1 FR2454406A1 (fr) 1980-11-14
FR2454406B1 true FR2454406B1 (fr) 1984-10-19

Family

ID=6068845

Family Applications (1)

Application Number Title Priority Date Filing Date
FR8005572A Granted FR2454406A1 (fr) 1979-04-20 1980-03-12 Avion a ailes portantes muni de parties avant mobiles

Country Status (5)

Country Link
US (1) US4437631A (fr)
DE (1) DE2916040C2 (fr)
FR (1) FR2454406A1 (fr)
GB (1) GB2048181B (fr)
NL (1) NL187005C (fr)

Families Citing this family (30)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3133961A1 (de) * 1981-08-27 1983-04-07 Vereinigte Flugtechnische Werke Gmbh, 2800 Bremen "betaetigungsanordnung fuer fluegelklappen"
DE3321128A1 (de) * 1983-06-10 1984-12-13 The Boeing Co., Seattle, Wash. Mechanismus zum ausfahren und positionieren einer hochauftriebseinrichtung relativ zu einer tragflaeche
FR2547270B1 (fr) * 1983-06-10 1985-09-06 Boeing Co Mecanisme d'extension et de retraction pour un volet de bord d'attaque d'une aile d'avion
DE3636053A1 (de) * 1986-10-23 1988-05-11 Messerschmitt Boelkow Blohm Einrichtung zum ausfahren von slats
DE3721479A1 (de) * 1987-06-30 1989-01-19 Messerschmitt Boelkow Blohm Betaetigungsanordnung fuer vorfluegel eines luftfahrzeug-tragfluegels
US5681013A (en) * 1995-12-26 1997-10-28 The Boeing Company Vortex leading edge flap assembly for supersonic airplanes
US7249735B2 (en) * 2005-06-30 2007-07-31 The Boeing Company Translating conduit apparatus for an airplane or equipment
US10400818B2 (en) * 2007-12-06 2019-09-03 Roller Bearing Company Of America, Inc. Track roller bearings with rolling elements or liners
US20140131512A1 (en) * 2007-12-06 2014-05-15 Roller Bearing Company Of America, Inc. Seal and electrical conductor for lined track rollers used on actuation system for aircraft lift assisting devices
US10023302B2 (en) 2007-12-06 2018-07-17 Roller Bearing Company Of America, Inc. Actuation system for a lift assisting device and lined track rollers used therein
US20140339358A1 (en) * 2007-12-06 2014-11-20 Roller Bearing Company Of America, Inc. Electrical conductor for lined track rollers used on actuation system for aircraft lift assisting devices
US20110220762A1 (en) * 2007-12-06 2011-09-15 Roller Bearing Company Of America, Inc. Actuation system for a lift assisting device and roller bearings used therein
US8025257B2 (en) * 2007-12-06 2011-09-27 Roller Bearing Company Of America, Inc. Actuation system for a lift assisting device and roller bearings used therein
US9261132B2 (en) 2009-04-24 2016-02-16 Roller Bearing Company Of America, Inc. Low friction bearing assembly and link apparatus
GB0913473D0 (en) 2009-08-04 2009-09-16 Airbus Operations Ltd Support assembly
GB201008773D0 (en) * 2010-05-26 2010-07-14 Airbus Uk Ltd Aircraft slat assembly
GB201011378D0 (en) * 2010-07-06 2010-08-18 Ultra Electronics Ltd Linkage for guiding a flexible cable
CN102407939B (zh) * 2011-09-30 2013-08-07 北京航空航天大学 可变平板式仿生前缘襟翼装置
US8622350B1 (en) * 2011-11-14 2014-01-07 The Boeing Company Compound leading edge device for aircraft
US11149788B2 (en) * 2012-04-30 2021-10-19 Roller Bearing Company Of America, Inc. Hybrid bearing assembly with rolling elements and plain bearing
GB2533311A (en) * 2014-12-15 2016-06-22 Airbus Operations Ltd A track container
AU2016278098B2 (en) 2015-06-18 2020-06-18 Bae Systems Plc Aircraft wing system
EP3106385A1 (fr) * 2015-06-18 2016-12-21 BAE Systems PLC Systeme d'aile d'aeronef
AU2016278099B2 (en) 2015-06-18 2020-07-23 Bae Systems Plc Aircraft wing system
BE1023370B1 (fr) * 2016-01-27 2017-02-22 Sonaca S.A. Aile d'aeronef comprenant un volet mobile et un boitier de rangement de tubulure souple
EP3378762A1 (fr) 2017-03-24 2018-09-26 Airbus Operations GmbH Aile d'avion
EP3378760A1 (fr) * 2017-03-24 2018-09-26 Airbus Operations GmbH Aile pour aéronef
EP3878734B1 (fr) * 2020-03-11 2023-07-19 Airbus Operations GmbH Élément de guidage pour un agencement de profil aérodynamique hypersustentateur d'un avion, agencement de profil aérodynamique hypersustentateur et procédé de production
CN112141318B (zh) * 2020-09-27 2022-11-29 西北工业大学 基于指节式连杆驱动的后缘变弯度机构
CN115817795B (zh) * 2022-12-27 2023-08-01 江苏华阳重工股份有限公司 一种高性能襟翼舵体

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2231564B1 (fr) * 1973-05-29 1976-11-12 Dassault Avions
DE2355723C3 (de) * 1973-11-08 1979-05-23 Dornier Gmbh, 7990 Friedrichshafen Spaltklappensystem für Flugzeuge

Also Published As

Publication number Publication date
GB2048181B (en) 1982-12-08
NL8000483A (nl) 1980-10-22
GB2048181A (en) 1980-12-10
US4437631A (en) 1984-03-20
DE2916040A1 (de) 1980-10-30
FR2454406A1 (fr) 1980-11-14
DE2916040C2 (de) 1986-01-02
NL187005B (nl) 1990-12-03
NL187005C (nl) 1991-05-01

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Legal Events

Date Code Title Description
CD Change of name or company name
TP Transmission of property
ST Notification of lapse