DE602008006402D1 - Hochauftriebssystem am tragflügel eines flugzeugs - Google Patents

Hochauftriebssystem am tragflügel eines flugzeugs

Info

Publication number
DE602008006402D1
DE602008006402D1 DE602008006402T DE602008006402T DE602008006402D1 DE 602008006402 D1 DE602008006402 D1 DE 602008006402D1 DE 602008006402 T DE602008006402 T DE 602008006402T DE 602008006402 T DE602008006402 T DE 602008006402T DE 602008006402 D1 DE602008006402 D1 DE 602008006402D1
Authority
DE
Germany
Prior art keywords
wing
flap
levers
gap
curvature
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.)
Active
Application number
DE602008006402T
Other languages
English (en)
Inventor
Gerd Heller
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
Airbus Operations 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 Airbus Operations GmbH filed Critical Airbus Operations GmbH
Publication of DE602008006402D1 publication Critical patent/DE602008006402D1/de
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C3/00Wings
    • B64C3/38Adjustment of complete wings or parts thereof
    • B64C3/44Varying camber
    • B64C3/50Varying camber by leading or trailing edge flaps
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Toys (AREA)
  • Blinds (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Other Liquid Machine Or Engine Such As Wave Power Use (AREA)
  • Prostheses (AREA)
DE602008006402T 2007-05-04 2008-05-05 Hochauftriebssystem am tragflügel eines flugzeugs Active DE602008006402D1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102007020870A DE102007020870A1 (de) 2007-05-04 2007-05-04 Hochauftriebssystem am Tragflügel eines Flugzeugs
PCT/EP2008/003595 WO2008135266A1 (en) 2007-05-04 2008-05-05 High lift system on the airfoil of an aircraft

Publications (1)

Publication Number Publication Date
DE602008006402D1 true DE602008006402D1 (de) 2011-06-01

Family

ID=39745663

Family Applications (2)

Application Number Title Priority Date Filing Date
DE102007020870A Ceased DE102007020870A1 (de) 2007-05-04 2007-05-04 Hochauftriebssystem am Tragflügel eines Flugzeugs
DE602008006402T Active DE602008006402D1 (de) 2007-05-04 2008-05-05 Hochauftriebssystem am tragflügel eines flugzeugs

Family Applications Before (1)

Application Number Title Priority Date Filing Date
DE102007020870A Ceased DE102007020870A1 (de) 2007-05-04 2007-05-04 Hochauftriebssystem am Tragflügel eines Flugzeugs

Country Status (7)

Country Link
US (1) US8286921B2 (de)
EP (1) EP2162352B1 (de)
CN (1) CN101674980B (de)
AT (1) ATE506255T1 (de)
DE (2) DE102007020870A1 (de)
RU (1) RU2463211C2 (de)
WO (1) WO2008135266A1 (de)

Families Citing this family (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102007063583A1 (de) 2007-12-28 2009-07-16 Airbus Deutschland Gmbh Hochauftriebssystem für ein Flugzeug
CN102180259B (zh) * 2011-04-15 2014-05-07 天津全华时代航天科技发展有限公司 抗扰流的小型无人机
DE102011105912A1 (de) 2011-06-28 2013-01-03 Airbus Operations Gmbh Tragflügel mit einem Hauptflügel und einem Hochauftriebskörper sowie Verfahren zur Ausführung von Verstellbewegungen eines Hochauftriebskörpers gegenüber einem Hauptflügel
US8622350B1 (en) * 2011-11-14 2014-01-07 The Boeing Company Compound leading edge device for aircraft
CN102642616B (zh) * 2012-05-11 2014-09-17 中国航空工业集团公司西安飞机设计研究所 一种带固定双缝襟翼的飞机增升装置
CN102975849A (zh) * 2012-12-14 2013-03-20 中国航空工业空气动力研究院 一种前探式前翼前缘襟翼结构
CN105008221B (zh) * 2013-03-06 2017-08-08 庞巴迪公司 飞机的高升力控制方法和系统
AU2016278099B2 (en) * 2015-06-18 2020-07-23 Bae Systems Plc Aircraft wing system
WO2016203255A1 (en) * 2015-06-18 2016-12-22 Bae Systems Plc Aircraft wing system
EP3106386A1 (de) * 2015-06-18 2016-12-21 BAE Systems PLC Flugzeugflügelsystem
EP3106385A1 (de) * 2015-06-18 2016-12-21 BAE Systems PLC Flugzeugflügelsystem
ES2797681T3 (es) * 2016-11-25 2020-12-03 Airbus Operations Sl Superficie de elevación de una aeronave para aumentar la fuerza de sustentación generada
EP3339164A1 (de) 2016-12-22 2018-06-27 Airbus Operations GmbH Flügel für ein flugzeug
EP3339163A1 (de) * 2016-12-22 2018-06-27 Airbus Operations GmbH Flügel für ein flugzeug
US10766600B2 (en) * 2017-07-28 2020-09-08 The Boeing Company Articulation assemblies for retracting aircraft flap support fairings and related methods
US10766601B2 (en) * 2017-11-28 2020-09-08 The Boeing Company Aircraft wing flaps having aerodynamic restoration doors
CN109131833A (zh) * 2018-09-28 2019-01-04 成都飞机工业(集团)有限责任公司 一种高增升的大展弦比机翼
JP7210324B2 (ja) * 2019-02-26 2023-01-23 三菱重工業株式会社 翼及びこれを備えた機械
CN110683033B (zh) * 2019-10-31 2023-03-21 哈尔滨工程大学 一种可调距式旋翼
CN111003152B (zh) * 2019-12-25 2023-10-20 中国航空工业集团公司西安飞机设计研究所 一种飞机舵面前缘密封装置
CN111152913A (zh) * 2020-02-28 2020-05-15 中国商用飞机有限责任公司北京民用飞机技术研究中心 一种翼身融合飞机
CN114455067B (zh) * 2021-11-23 2024-02-09 北京航空航天大学 一种适用于超长襟翼的增升装置

Family Cites Families (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1780838A (en) * 1927-07-09 1930-11-04 Handley Page Ltd Means for controlling aeroplanes
US1861318A (en) * 1931-01-23 1932-05-31 Handley Page Ltd Means for controlling aeroplanes
US2137879A (en) * 1935-02-26 1938-11-22 Ksoll Joseph Supporting surface for flying machines
SU73531A2 (ru) * 1948-01-16 1948-11-30 А.И. Болдырев Разрезное крыло с подвижным предкрылком
US4447027A (en) 1979-01-02 1984-05-08 The Boeing Company Upper surface blown powered lift system for aircraft
GB2138756B (en) * 1983-04-26 1986-07-16 Boeing Co Wing leading edge slat
DE3721479A1 (de) * 1987-06-30 1989-01-19 Messerschmitt Boelkow Blohm Betaetigungsanordnung fuer vorfluegel eines luftfahrzeug-tragfluegels
US5544847A (en) * 1993-11-10 1996-08-13 The Boeing Company Leading edge slat/wing combination
JP2800769B2 (ja) * 1996-03-29 1998-09-21 日本電気株式会社 情報フィルタリング方式
US6807531B1 (en) * 1998-04-08 2004-10-19 Sysmex Corporation Support system for making decisions on medical treatment plans or test plans
GB0114634D0 (en) * 2001-06-15 2001-08-08 Broadbent Michael C Contiguous variable camber device
US6915297B2 (en) * 2002-05-21 2005-07-05 Bridgewell, Inc. Automatic knowledge management system
US20050086078A1 (en) * 2003-10-17 2005-04-21 Cogentmedicine, Inc. Medical literature database search tool
WO2006108069A2 (en) * 2005-04-06 2006-10-12 Google, Inc. Searching through content which is accessible through web-based forms
US7406453B2 (en) * 2005-11-04 2008-07-29 Microsoft Corporation Large-scale information collection and mining
US20080091086A1 (en) * 2006-10-12 2008-04-17 Henry Joseph Legere Method and Apparatus for a Constellation-of-Symptoms Approach to Patient-Driven Computer-Assisted Diagnosis
US20080215627A1 (en) * 2007-01-04 2008-09-04 Imetrikus, Inc. Standardized health data hub
US20090241177A1 (en) * 2008-03-21 2009-09-24 Computerized Screening, Inc. Security system for a community based managed health kiosk system

Also Published As

Publication number Publication date
CN101674980A (zh) 2010-03-17
RU2009144844A (ru) 2011-06-10
DE102007020870A1 (de) 2008-11-13
EP2162352A1 (de) 2010-03-17
RU2463211C2 (ru) 2012-10-10
US20100155542A1 (en) 2010-06-24
ATE506255T1 (de) 2011-05-15
CN101674980B (zh) 2012-10-24
EP2162352B1 (de) 2011-04-20
US8286921B2 (en) 2012-10-16
WO2008135266A4 (en) 2009-01-22
WO2008135266A1 (en) 2008-11-13

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