ATE542739T1 - Flugzeugflügel - Google Patents

Flugzeugflügel

Info

Publication number
ATE542739T1
ATE542739T1 AT07705160T AT07705160T ATE542739T1 AT E542739 T1 ATE542739 T1 AT E542739T1 AT 07705160 T AT07705160 T AT 07705160T AT 07705160 T AT07705160 T AT 07705160T AT E542739 T1 ATE542739 T1 AT E542739T1
Authority
AT
Austria
Prior art keywords
slat
extension
main body
body portion
leading
Prior art date
Application number
AT07705160T
Other languages
English (en)
Inventor
Daniel Dodd
Francois Cathelain
Original Assignee
Airbus Operations Ltd
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 Ltd filed Critical Airbus Operations Ltd
Application granted granted Critical
Publication of ATE542739T1 publication Critical patent/ATE542739T1/de

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/28—Leading or trailing edges attached to primary structures, e.g. forming fixed slots
    • 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
    • B64C9/22—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)
  • Mechanical Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Tires In General (AREA)
  • Toys (AREA)
  • Feedback Control In General (AREA)
  • Joining Of Building Structures In Genera (AREA)
  • Radio Relay Systems (AREA)
AT07705160T 2006-02-28 2007-02-07 Flugzeugflügel ATE542739T1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GBGB0604026.5A GB0604026D0 (en) 2006-02-28 2006-02-28 Aircraft wing
PCT/GB2007/000429 WO2007099285A1 (en) 2006-02-28 2007-02-07 Aircraft wing

Publications (1)

Publication Number Publication Date
ATE542739T1 true ATE542739T1 (de) 2012-02-15

Family

ID=36218861

Family Applications (1)

Application Number Title Priority Date Filing Date
AT07705160T ATE542739T1 (de) 2006-02-28 2007-02-07 Flugzeugflügel

Country Status (10)

Country Link
US (1) US8353483B2 (de)
EP (1) EP1991459B1 (de)
JP (1) JP5240458B2 (de)
CN (1) CN101389530B (de)
AT (1) ATE542739T1 (de)
BR (1) BRPI0708289A2 (de)
CA (1) CA2638042C (de)
GB (1) GB0604026D0 (de)
RU (1) RU2468962C2 (de)
WO (1) WO2007099285A1 (de)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2009101461A1 (en) 2008-02-12 2009-08-20 Bombardier Inc. Improved slat configuration for fixed-wing aircraft
GB0902685D0 (en) * 2009-02-18 2009-04-01 Airbus Uk Ltd Aircraft wing assembly
CN102275635A (zh) * 2010-10-14 2011-12-14 王一况 刨刀形翼型与飞机、空天飞机
CN102682169B (zh) * 2012-05-11 2014-06-11 中国航空工业集团公司西安飞机设计研究所 基于五个控制剖面的缝翼展向控制曲线的设计方法
CA3046603A1 (en) 2016-12-12 2018-06-21 Bombardier Inc. Aircraft slat
CN107444612B (zh) * 2017-08-15 2023-04-18 中国空气动力研究与发展中心高速空气动力研究所 一种λ机翼飞翼布局无人飞行器的变机翼前缘装置
CN110789729B (zh) * 2018-08-02 2024-01-30 中国商用飞机有限责任公司 飞机缝翼笛形管导向工装及更换方法

Family Cites Families (30)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2973925A (en) * 1958-03-24 1961-03-07 Lockheed Aircraft Corp Aerodynamically automatic airfoil slat mechanism
US3486720A (en) * 1967-12-07 1969-12-30 Boeing Co Continuous slot forming leading edge slats for cranked wings
US3576301A (en) * 1969-06-20 1971-04-27 Joseph W Stickle Direct lift control system
JPS5810277B2 (ja) * 1977-02-08 1983-02-24 川崎重工業株式会社 航空機用高揚力装置
JPS5614160Y2 (de) * 1977-07-01 1981-04-02
US4189120A (en) * 1977-12-14 1980-02-19 Boeing Commercial Airplane Company Variable camber leading edge flap
CA1100463A (en) * 1978-11-22 1981-05-05 Frederick L. Gilbertson Nozzle structure with notches
US4398688A (en) * 1979-12-26 1983-08-16 Lockheed Corporation Leading edge flap for an airfoil
FR2492337A1 (fr) * 1980-10-16 1982-04-23 Aerospatiale Aile d'aeronef pourvue d'un systeme hypersustentateur dans son bord d'attaque et aeronef comportant une telle aile
US4399970A (en) 1980-11-13 1983-08-23 The Boeing Company Wing leading edge slat
FR2555960B1 (fr) * 1983-12-06 1986-09-19 Aerospatiale Aile d'aeronef en fleche pourvue d'un systeme hypersustentateur et d'un mat de suspension de moteur, ainsi que mat de suspension de moteur pour une telle aile
US5056741A (en) * 1989-09-29 1991-10-15 The Boeing Company Apparatus and method for aircraft wing stall control
US5167383A (en) 1990-08-18 1992-12-01 Yoshio Nozaki STOL aircraft
RU2022879C1 (ru) * 1991-04-09 1994-11-15 Авиационный научно-технический комплекс им.О.К.Антонова Носок крыла самолета
JP2606289Y2 (ja) * 1993-06-07 2000-10-10 富士重工業株式会社 航空機のナセル装置
DE19719922C1 (de) * 1997-05-13 1998-11-12 Daimler Benz Aerospace Airbus Einrichtung zur Beeinflussung einer Wurzelströmung
US6073889A (en) 1997-10-16 2000-06-13 The Boeing Company Wing flap seal bump
DE19910551C2 (de) 1999-03-10 2001-04-05 Eads Airbus Gmbh Flugzeugtragfläche mit mindestens einem kurzgekoppelten Triebwerk
US6598834B2 (en) * 2000-02-14 2003-07-29 Aerotech Services Inc. Method for reducing fuel consumption in aircraft
JP4535550B2 (ja) * 2000-02-23 2010-09-01 富士重工業株式会社 回転翼航空機の回転翼羽根
US6435458B1 (en) * 2001-02-12 2002-08-20 The Boeing Company Tailored wing assembly for an aircraft moveable slat system
US6478541B1 (en) * 2001-08-16 2002-11-12 The Boeing Company Tapered/segmented flaps for rotor blade-vortex interaction (BVI) noise and vibration reduction
JP2004039867A (ja) 2002-07-03 2004-02-05 Sony Corp 多層配線回路モジュール及びその製造方法
US20050045764A1 (en) * 2003-08-29 2005-03-03 Supersonic Aerospace International, Llc Canard position and dihedral for boom reduction and pitch/directional control
US7070146B2 (en) * 2003-08-29 2006-07-04 Supersonic Aerospace International, Llc Aircraft thickness/camber control device for low sonic boom
BE1015867A3 (fr) * 2004-01-22 2005-10-04 Sonaca Sa Ensemble de bord d'attaque d'un element de voilure d'aeronef et element de voilure equipee d'au moins un tel ensemble.
US7357358B2 (en) 2004-02-27 2008-04-15 The Boeing Company Aircraft leading edge device systems and corresponding sizing methods
US6978971B1 (en) * 2004-06-15 2005-12-27 The Boeing Company Methods and apparatuses for controlling airflow proximate to engine/airfoil systems
US7264206B2 (en) * 2004-09-30 2007-09-04 The Boeing Company Leading edge flap apparatuses and associated methods
WO2009101461A1 (en) * 2008-02-12 2009-08-20 Bombardier Inc. Improved slat configuration for fixed-wing aircraft

Also Published As

Publication number Publication date
GB0604026D0 (en) 2006-04-12
JP2009528220A (ja) 2009-08-06
EP1991459A1 (de) 2008-11-19
US20090008506A1 (en) 2009-01-08
JP5240458B2 (ja) 2013-07-17
CN101389530B (zh) 2011-06-01
CN101389530A (zh) 2009-03-18
RU2008138594A (ru) 2010-04-10
WO2007099285A1 (en) 2007-09-07
CA2638042A1 (en) 2007-09-07
EP1991459B1 (de) 2012-01-25
US8353483B2 (en) 2013-01-15
RU2468962C2 (ru) 2012-12-10
BRPI0708289A2 (pt) 2011-05-24
CA2638042C (en) 2014-09-16

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