FR1011175A - Perfectionnement aux ailes d'avions - Google Patents

Perfectionnement aux ailes d'avions

Info

Publication number
FR1011175A
FR1011175A FR1011175DA FR1011175A FR 1011175 A FR1011175 A FR 1011175A FR 1011175D A FR1011175D A FR 1011175DA FR 1011175 A FR1011175 A FR 1011175A
Authority
FR
France
Prior art keywords
improvement
aircraft wings
wings
aircraft
wings improvement
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
Application number
Other languages
English (en)
Inventor
P Briend
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.)
Office National dEtudes et de Recherches Aerospatiales ONERA
Original Assignee
Office National dEtudes et de Recherches Aerospatiales ONERA
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 Office National dEtudes et de Recherches Aerospatiales ONERA filed Critical Office National dEtudes et de Recherches Aerospatiales ONERA
Application granted granted Critical
Publication of FR1011175A publication Critical patent/FR1011175A/fr
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C9/00Adjustable control surfaces or members, e.g. rudders
    • B64C9/14Adjustable control surfaces or members, e.g. rudders forming slots
    • B64C9/22Adjustable control surfaces or members, e.g. rudders forming slots at the front of the wing
    • B64C9/24Adjustable 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)
FR1011175D 1948-12-20 1948-12-20 Perfectionnement aux ailes d'avions Expired FR1011175A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1011175T 1948-12-20

Publications (1)

Publication Number Publication Date
FR1011175A true FR1011175A (fr) 1952-06-19

Family

ID=9569685

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1011175D Expired FR1011175A (fr) 1948-12-20 1948-12-20 Perfectionnement aux ailes d'avions

Country Status (1)

Country Link
FR (1) FR1011175A (fr)

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1129379B (de) * 1960-11-11 1962-05-10 Dornier Werke Gmbh Flugzeugtragfluegel mit festem Vorfluegel
DE1179809B (de) * 1959-01-24 1964-10-15 Josef Ksoll Quertriebsflaeche, insbesondere Flugzeugtragfluegel, mit einem Vorfluegel
US3363859A (en) * 1960-05-19 1968-01-16 Dehavilland Aircraft Aircraft
US3375998A (en) * 1962-04-16 1968-04-02 Alberto Alvarez Calderon Leading edge flap and apparatus thereof
FR2172411A1 (fr) * 1972-02-16 1973-09-28 Ver Flugtechnische Werke
DE1781465B1 (de) * 1966-10-25 1976-03-04 Messerschmitt Boelkow Blohm Tragfluegel fuer luftfahrzeuge mit einem beweglichen vorfluegel
US4640477A (en) * 1984-12-31 1987-02-03 The Boeing Company Closing device for an airfoil
EP1057723A3 (fr) * 1999-06-04 2002-08-28 DLR Deutsches Zentrum für Luft- und Raumfahrt e.V. Aile auxiliaire pour ailes principales d'aéronef
WO2006056160A1 (fr) * 2004-11-23 2006-06-01 Airbus Deutschland Gmbh Configuration permettant de reduire le bruit aerodynamique d'une aile auxiliaire d'avion
WO2011123204A1 (fr) * 2010-03-31 2011-10-06 The Boeing Company Système de bec de bord d'attaque à faible bruit doté d'éléments de bord d'attaque de voilure déployable
CN102935889A (zh) * 2012-11-16 2013-02-20 中国航空工业集团公司西安飞机设计研究所 一种可减阻降噪的前缘缝翼空腔整形机构
US8424810B1 (en) 2010-03-31 2013-04-23 The Boeing Company Low noise wing slat system with rigid cove-filled slat
US8864083B1 (en) 2010-03-31 2014-10-21 The Boeing Company Low noise wing slat system with a fixed wing leading edge and deployable bridging panels

Cited By (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1179809B (de) * 1959-01-24 1964-10-15 Josef Ksoll Quertriebsflaeche, insbesondere Flugzeugtragfluegel, mit einem Vorfluegel
US3363859A (en) * 1960-05-19 1968-01-16 Dehavilland Aircraft Aircraft
DE1129379B (de) * 1960-11-11 1962-05-10 Dornier Werke Gmbh Flugzeugtragfluegel mit festem Vorfluegel
US3375998A (en) * 1962-04-16 1968-04-02 Alberto Alvarez Calderon Leading edge flap and apparatus thereof
DE1781465B1 (de) * 1966-10-25 1976-03-04 Messerschmitt Boelkow Blohm Tragfluegel fuer luftfahrzeuge mit einem beweglichen vorfluegel
FR2172411A1 (fr) * 1972-02-16 1973-09-28 Ver Flugtechnische Werke
US4640477A (en) * 1984-12-31 1987-02-03 The Boeing Company Closing device for an airfoil
EP1057723A3 (fr) * 1999-06-04 2002-08-28 DLR Deutsches Zentrum für Luft- und Raumfahrt e.V. Aile auxiliaire pour ailes principales d'aéronef
US8006941B2 (en) 2004-11-23 2011-08-30 Airbus Deutschland Gmbh System for reducing aerodynamic noise at a supplementary wing of an aircraft
JP2008520483A (ja) * 2004-11-23 2008-06-19 エアバス・ドイチュラント・ゲーエムベーハー 航空機補助翼において空力騒音を低減するシステム
US7766281B2 (en) 2004-11-23 2010-08-03 Airbus Deutschland Gmbh System for reducing aerodynamic noise at a supplementary wing of an aircraft
DE102004056537B4 (de) * 2004-11-23 2010-09-09 Eads Deutschland Gmbh Anordnung zur Minderung des aerodynamischen Lärms an einem Zusatzflügel eines Flugzeuges
WO2006056160A1 (fr) * 2004-11-23 2006-06-01 Airbus Deutschland Gmbh Configuration permettant de reduire le bruit aerodynamique d'une aile auxiliaire d'avion
CN102834315A (zh) * 2010-03-31 2012-12-19 波音公司 带有可展开机翼前缘元件的低噪音机翼缝翼系统
US8276852B2 (en) 2010-03-31 2012-10-02 The Boeing Company Low noise wing slat system with deployable wing leading edge elements
WO2011123204A1 (fr) * 2010-03-31 2011-10-06 The Boeing Company Système de bec de bord d'attaque à faible bruit doté d'éléments de bord d'attaque de voilure déployable
US8424810B1 (en) 2010-03-31 2013-04-23 The Boeing Company Low noise wing slat system with rigid cove-filled slat
JP2013523521A (ja) * 2010-03-31 2013-06-17 ザ・ボーイング・カンパニー 展開可能な翼前縁要素を備える低騒音翼スラットシステム
AU2011233687B2 (en) * 2010-03-31 2014-01-16 The Boeing Company Low noise wing slat system with deployable wing leading edge elements
US8864083B1 (en) 2010-03-31 2014-10-21 The Boeing Company Low noise wing slat system with a fixed wing leading edge and deployable bridging panels
RU2566833C2 (ru) * 2010-03-31 2015-10-27 Зе Боинг Компани Малошумящая система предкрылка с элеметами, размещенными в передней кромке крыла и выполненными с возможностью развертывания
CN102834315B (zh) * 2010-03-31 2016-01-13 波音公司 带有可展开机翼前缘元件的低噪音机翼缝翼系统
KR101847659B1 (ko) 2010-03-31 2018-04-10 더 보잉 컴파니 전개가능한 날개 선행 에지 부재들을 구비한 저소음 날개 슬랫 시스템
CN102935889A (zh) * 2012-11-16 2013-02-20 中国航空工业集团公司西安飞机设计研究所 一种可减阻降噪的前缘缝翼空腔整形机构

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