FR2767111B1 - Aile d'avion equipee d'un volet d'atterrissage - Google Patents

Aile d'avion equipee d'un volet d'atterrissage

Info

Publication number
FR2767111B1
FR2767111B1 FR9809840A FR9809840A FR2767111B1 FR 2767111 B1 FR2767111 B1 FR 2767111B1 FR 9809840 A FR9809840 A FR 9809840A FR 9809840 A FR9809840 A FR 9809840A FR 2767111 B1 FR2767111 B1 FR 2767111B1
Authority
FR
France
Prior art keywords
aircraft wing
landing flap
wing equipped
landing
flap
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.)
Expired - Fee Related
Application number
FR9809840A
Other languages
English (en)
Other versions
FR2767111A1 (fr
Inventor
Claus Bauer
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 GmbH
Original Assignee
Daimler Benz AG
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 Daimler Benz AG filed Critical Daimler Benz AG
Publication of FR2767111A1 publication Critical patent/FR2767111A1/fr
Application granted granted Critical
Publication of FR2767111B1 publication Critical patent/FR2767111B1/fr
Anticipated expiration legal-status Critical
Expired - Fee Related 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
    • B64C9/16—Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing
    • B64C9/18—Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing by single flaps
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/38—Adjustment of complete wings or parts thereof
    • B64C3/44—Varying camber
    • B64C3/50—Varying camber by leading or trailing edge flaps
    • 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
FR9809840A 1997-07-31 1998-07-31 Aile d'avion equipee d'un volet d'atterrissage Expired - Fee Related FR2767111B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19732953A DE19732953C1 (de) 1997-07-31 1997-07-31 Tragflügel mit Landeklappe

Publications (2)

Publication Number Publication Date
FR2767111A1 FR2767111A1 (fr) 1999-02-12
FR2767111B1 true FR2767111B1 (fr) 2003-05-16

Family

ID=7837452

Family Applications (1)

Application Number Title Priority Date Filing Date
FR9809840A Expired - Fee Related FR2767111B1 (fr) 1997-07-31 1998-07-31 Aile d'avion equipee d'un volet d'atterrissage

Country Status (5)

Country Link
US (1) US6076775A (fr)
DE (1) DE19732953C1 (fr)
FR (1) FR2767111B1 (fr)
GB (1) GB2331734B (fr)
IT (1) ITMI981598A1 (fr)

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE19858435C1 (de) * 1998-12-17 2000-06-29 Daimler Chrysler Ag Deckhaut-Steg-Struktur
GB2386884B (en) * 2002-03-28 2005-09-14 Richard Linsley-Hood Aerofoil with variable camber
DE602004029655D1 (en) * 2003-03-03 2010-12-02 Flexsys Inc Adaptives flexibles flügel- und rotorsystem
US6827311B2 (en) * 2003-04-07 2004-12-07 Honeywell International, Inc. Flight control actuation system
DE10325950A1 (de) * 2003-06-07 2005-01-05 Airbus Deutschland Gmbh Flügel, insbesondere Tragflügel eines Flugzeugs, mit veränderbarem Profil
DE102004006940B4 (de) 2004-02-12 2009-02-26 Airbus Deutschland Gmbh Landeklappenführung für Luftfahrzeuge
DE102004049504A1 (de) * 2004-10-11 2006-04-13 Airbus Deutschland Gmbh Flugzeugflügel, Verfahren zum Betreiben eines Flugzeugflügels und Verwendung einer schwenkbaren Hinterkante an einem Hauptflügel eines Flugzeugflügels zum Justieren der Form und Breite eines Luftspalts
US20070138341A1 (en) * 2004-12-07 2007-06-21 Joshi Shiv P Transformable skin
DE102005045759A1 (de) 2005-09-23 2007-04-12 Airbus Deutschland Gmbh Fortschrittlicheflügelhinterkante am Flügel eines Flugzeugs
DE102005061750A1 (de) * 2005-12-21 2007-07-05 Eads Deutschland Gmbh Flexible Steuerfläche für ein Luftfahrzeug
DE102006036464B4 (de) * 2006-08-04 2009-08-20 Airbus Deutschland Gmbh Hochauftriebssystem für ein Flugzeug
DE102007036996A1 (de) * 2007-08-06 2009-02-19 Airbus Deutschland Gmbh Hochauftriebssystem für ein Flugzeug
EP3670330B1 (fr) * 2018-12-20 2022-02-09 Bombardier Inc. Système de déploiement de volet d'avion
EP4286271A1 (fr) * 2022-06-01 2023-12-06 Asco Industries NV Ensemble de volet de bord de fuite

Family Cites Families (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US32907A (en) * 1861-07-23 Churn
DE703375C (de) * 1939-01-12 1941-03-07 Gerhard Fieseler Steuerflaeche fuer Luftfahrzeuge
US3042371A (en) * 1958-09-04 1962-07-03 United Aircraft Corp Variable camber balding
FR1496151A (fr) * 1966-06-20 1967-09-29 Giravions Dorand Volet déviateur pour jet de fluide
US3583660A (en) * 1969-08-18 1971-06-08 Lockheed Aircraft Corp Lift and control augmenter for airfoils
US4053124A (en) * 1975-08-22 1977-10-11 The Boeing Company Variable camber airfoil
DE2804254C2 (de) * 1978-02-01 1985-02-07 Grob, Burkhart, Dipl.-Ing. ETH, 8023 Großhesselohe Tragflügel mit Klappe
US4247066A (en) * 1978-02-21 1981-01-27 General Dynamics Corporation Airfoil variable cambering device and method
US4395008A (en) * 1980-01-22 1983-07-26 British Aerospace Public Limited Company Aircraft wing and flap arrangement
US4351502A (en) * 1980-05-21 1982-09-28 The Boeing Company Continuous skin, variable camber airfoil edge actuating mechanism
DE3133961A1 (de) * 1981-08-27 1983-04-07 Vereinigte Flugtechnische Werke Gmbh, 2800 Bremen "betaetigungsanordnung fuer fluegelklappen"
US4427169A (en) * 1982-06-08 1984-01-24 Boeing Commercial Airplane Company Variable camber flap end seal
US4899284A (en) * 1984-09-27 1990-02-06 The Boeing Company Wing lift/drag optimizing system
DE3527497A1 (de) * 1985-07-31 1987-02-12 Airbus Gmbh Tragfluegel mit ausfahrbarer klappe und veraenderbarer woelbung
DE4107556C1 (fr) * 1991-03-08 1992-05-14 Deutsche Airbus Gmbh, 2000 Hamburg, De
US5150864A (en) * 1991-09-20 1992-09-29 Georgia Tech Research Corporation Variable camber control of airfoil
DE4243203A1 (de) * 1992-12-19 1994-06-23 Schempp Hirth Flugzeugbau Gmbh Tragflügel- oder Leitwerkprofil für Flugzeuge, insbesondere Segelflugzeuge
US5839700A (en) * 1996-06-03 1998-11-24 The United States Of America As Represented By The Secretary Of The Navy Articulated fin
DE19707392A1 (de) * 1997-02-25 1998-08-27 Deutsch Zentr Luft & Raumfahrt Aerodynamisches Bauteil, wie Landeklappe, Tragflügel, Höhen- oder Seitenleitwerk, mit veränderbarer Wölbung
US5839698A (en) * 1997-10-23 1998-11-24 Northrop Grumman Corporation Control surface continuous seal
US5887828A (en) * 1997-11-13 1999-03-30 Northrop Grumman Corporation Seamless mission adaptive control surface

Also Published As

Publication number Publication date
GB2331734B (en) 2002-01-16
ITMI981598A0 (it) 1998-07-13
ITMI981598A1 (it) 2000-01-13
GB2331734A (en) 1999-06-02
GB9816546D0 (en) 1998-09-30
US6076775A (en) 2000-06-20
DE19732953C1 (de) 1999-03-11
FR2767111A1 (fr) 1999-02-12

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Legal Events

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

Owner name: AIRBUS OPERATIONS GMBH

Effective date: 20111118

ST Notification of lapse

Effective date: 20150331