JP2010512274A - 航空機翼 - Google Patents

航空機翼 Download PDF

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Publication number
JP2010512274A
JP2010512274A JP2009540653A JP2009540653A JP2010512274A JP 2010512274 A JP2010512274 A JP 2010512274A JP 2009540653 A JP2009540653 A JP 2009540653A JP 2009540653 A JP2009540653 A JP 2009540653A JP 2010512274 A JP2010512274 A JP 2010512274A
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JP
Japan
Prior art keywords
wing
slot
auxiliary
auxiliary wing
aircraft
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.)
Pending
Application number
JP2009540653A
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English (en)
Japanese (ja)
Other versions
JP2010512274A5 (enExample
Inventor
グローマン、ボリス
ライヒェンベルガー、ジョアン
ラコフスキー、トーマス
Original Assignee
エアバス・オペレーションズ・ゲーエムベーハー
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 エアバス・オペレーションズ・ゲーエムベーハー filed Critical エアバス・オペレーションズ・ゲーエムベーハー
Publication of JP2010512274A publication Critical patent/JP2010512274A/ja
Publication of JP2010512274A5 publication Critical patent/JP2010512274A5/ja
Pending legal-status Critical Current

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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
    • B64C—AEROPLANES; HELICOPTERS
    • B64C7/00—Structures or fairings not otherwise provided for
    • 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
    • B64C2009/143—Adjustable control surfaces or members, e.g. rudders forming slots comprising independently adjustable elements for closing or opening the slot between the main wing and leading or trailing edge flaps

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Toys (AREA)
  • Organic Low-Molecular-Weight Compounds And Preparation Thereof (AREA)
  • Artificial Filaments (AREA)
JP2009540653A 2006-12-11 2007-12-11 航空機翼 Pending JP2010512274A (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102006058650A DE102006058650B4 (de) 2006-12-11 2006-12-11 Tragflügel eines Flugzeugs
PCT/EP2007/010831 WO2008071399A1 (en) 2006-12-11 2007-12-11 Wing of an aircraft

Publications (2)

Publication Number Publication Date
JP2010512274A true JP2010512274A (ja) 2010-04-22
JP2010512274A5 JP2010512274A5 (enExample) 2011-02-03

Family

ID=39228641

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2009540653A Pending JP2010512274A (ja) 2006-12-11 2007-12-11 航空機翼

Country Status (10)

Country Link
US (1) US8191835B2 (enExample)
EP (1) EP2091812B1 (enExample)
JP (1) JP2010512274A (enExample)
CN (1) CN101588964B (enExample)
AT (1) ATE483627T1 (enExample)
BR (1) BRPI0720267A2 (enExample)
CA (1) CA2672068A1 (enExample)
DE (2) DE102006058650B4 (enExample)
RU (1) RU2009126419A (enExample)
WO (1) WO2008071399A1 (enExample)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2019172072A1 (ja) * 2018-03-07 2019-09-12 三菱重工業株式会社 高揚力装置及び航空機の翼

Families Citing this family (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102008050544A1 (de) * 2008-10-06 2010-04-29 Airbus Deutschland Gmbh An der Tragfläche eines Flugzeugs angeordneter Vorflügel
US8534611B1 (en) 2009-07-17 2013-09-17 The Boeing Company Moveable leading edge device for a wing
US8534610B1 (en) 2009-07-17 2013-09-17 The Boeing Company Method and apparatus for a leading edge slat on a wing of an aircraft
US9327824B2 (en) 2010-12-15 2016-05-03 The Boeing Company Adjustment of wings for variable camber for optimum take-off and landing
DE102011018907A1 (de) * 2011-04-28 2012-10-31 Airbus Operations Gmbh Hochauftriebskomponente für ein Flugzeug, Hochauftriebssystem, Verfahren zum Beeinflussen der Hochauftriebseigenschaften eines Flugzeugs und Flugzeug
CN102417031A (zh) * 2011-10-20 2012-04-18 南京航空航天大学 大攻角非对称涡合成射流非定常小扰动控制装置
US9016637B2 (en) * 2012-02-10 2015-04-28 The Boeing Company High-positioned 3-position variable camber krueger
JP6426451B2 (ja) * 2014-12-03 2018-11-21 マツダ株式会社 自動車内外装部品
EP3676172B1 (en) * 2017-09-01 2023-01-11 Embraer S.A. Retractable leading edge wing slats having autonomously curvable airflow shield for noise-abatement
US20220111403A1 (en) * 2019-02-20 2022-04-14 Koninklijke Philips N.V. Vortex finder for a cyclonic separator
CN114728690A (zh) * 2019-11-18 2022-07-08 空中客车德国运营有限责任公司 用于飞行器机翼的缝翼装置
CN111924086B (zh) * 2020-07-07 2021-12-10 北京机电工程研究所 一种记忆合金驱动的可变形机构
CN114506460B (zh) * 2022-03-15 2024-05-10 中国商用飞机有限责任公司 用于监测襟翼故障的系统及方法
CN114771809B (zh) * 2022-04-17 2025-11-25 西北工业大学 一种下翼面尖端弧形凸起的缝翼降噪装置
CN114684353B (zh) * 2022-06-02 2022-10-14 中国空气动力研究与发展中心低速空气动力研究所 一种脉冲射流激励器、机翼和飞行器
CN115027663B (zh) * 2022-08-10 2022-11-22 中国空气动力研究与发展中心计算空气动力研究所 一种通过射流实现的机翼融合控制方法
CN120942604A (zh) * 2025-10-16 2025-11-14 北京航空航天大学 一种弦向折叠与快速展开的机翼结构

Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2381678A (en) * 1942-02-11 1945-08-07 Frank R Maxwell Airplane wing
US3129907A (en) * 1960-08-18 1964-04-21 Dornier Werke Gmbh Airplane wing flap
DE1481578A1 (de) * 1966-10-25 1970-01-15 Hamburger Flugzeugbau Gmbh Tragfluegel fuer Luftfahrzeuge mit beweglichem Vorfluegel
GB2096551A (en) * 1981-04-08 1982-10-20 Ver Flugtechnische Werke A method of optimizing the cruising conditions of aircraft with supercritical wings and an arrangement for carrying out the method
US5209438A (en) * 1988-06-20 1993-05-11 Israel Wygnanski Method and apparatus for delaying the separation of flow from a solid surface
US6171056B1 (en) * 1998-12-23 2001-01-09 Sikorsky Aircraft Corporation Technique for providing a signal for controlling blade vortex interaction noise of a rotorcraft
US20040129838A1 (en) * 2003-01-03 2004-07-08 Lisy Frederick J. Flow control device and method of controlling flow
EP1577212A2 (en) * 2004-03-16 2005-09-21 Westland Helicopters Limited Improvements in or relating to aerofoils
EP1714869A1 (de) * 2005-04-21 2006-10-25 Deutsches Zentrum für Luft- und Raumfahrt e.V. Auftriebsfläche mit verbessertem Ablöseverhalten bei stark veränderlichem Anstellwinkel

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2003098B (en) * 1977-07-07 1982-01-27 British Aircraft Corp Ltd Aircraft wings
DE19925560B4 (de) 1999-06-04 2004-04-22 Deutsches Zentrum für Luft- und Raumfahrt e.V. Zusatzflügel für Hauptflügel von Flugzeugen
DE102004056537B4 (de) 2004-11-23 2010-09-09 Eads Deutschland Gmbh Anordnung zur Minderung des aerodynamischen Lärms an einem Zusatzflügel eines Flugzeuges

Patent Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2381678A (en) * 1942-02-11 1945-08-07 Frank R Maxwell Airplane wing
US3129907A (en) * 1960-08-18 1964-04-21 Dornier Werke Gmbh Airplane wing flap
DE1481578A1 (de) * 1966-10-25 1970-01-15 Hamburger Flugzeugbau Gmbh Tragfluegel fuer Luftfahrzeuge mit beweglichem Vorfluegel
GB2096551A (en) * 1981-04-08 1982-10-20 Ver Flugtechnische Werke A method of optimizing the cruising conditions of aircraft with supercritical wings and an arrangement for carrying out the method
US5209438A (en) * 1988-06-20 1993-05-11 Israel Wygnanski Method and apparatus for delaying the separation of flow from a solid surface
US6171056B1 (en) * 1998-12-23 2001-01-09 Sikorsky Aircraft Corporation Technique for providing a signal for controlling blade vortex interaction noise of a rotorcraft
US20040129838A1 (en) * 2003-01-03 2004-07-08 Lisy Frederick J. Flow control device and method of controlling flow
EP1577212A2 (en) * 2004-03-16 2005-09-21 Westland Helicopters Limited Improvements in or relating to aerofoils
EP1714869A1 (de) * 2005-04-21 2006-10-25 Deutsches Zentrum für Luft- und Raumfahrt e.V. Auftriebsfläche mit verbessertem Ablöseverhalten bei stark veränderlichem Anstellwinkel

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2019172072A1 (ja) * 2018-03-07 2019-09-12 三菱重工業株式会社 高揚力装置及び航空機の翼

Also Published As

Publication number Publication date
RU2009126419A (ru) 2011-01-20
DE602007009720D1 (de) 2010-11-18
CN101588964B (zh) 2011-06-08
EP2091812B1 (en) 2010-10-06
CA2672068A1 (en) 2008-06-19
ATE483627T1 (de) 2010-10-15
CN101588964A (zh) 2009-11-25
WO2008071399A1 (en) 2008-06-19
DE102006058650A1 (de) 2008-06-12
WO2008071399B1 (en) 2008-07-31
DE102006058650B4 (de) 2009-11-19
EP2091812A1 (en) 2009-08-26
US20100019095A1 (en) 2010-01-28
BRPI0720267A2 (pt) 2014-01-28
US8191835B2 (en) 2012-06-05

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