ATE506255T1 - Hochauftriebssystem am tragflügel eines flugzeugs - Google Patents

Hochauftriebssystem am tragflügel eines flugzeugs

Info

Publication number
ATE506255T1
ATE506255T1 AT08749323T AT08749323T ATE506255T1 AT E506255 T1 ATE506255 T1 AT E506255T1 AT 08749323 T AT08749323 T AT 08749323T AT 08749323 T AT08749323 T AT 08749323T AT E506255 T1 ATE506255 T1 AT E506255T1
Authority
AT
Austria
Prior art keywords
wing
flap
levers
gap
lift system
Prior art date
Application number
AT08749323T
Other languages
English (en)
Inventor
Gerd Heller
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
Application granted granted Critical
Publication of ATE506255T1 publication Critical patent/ATE506255T1/de

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
    • B64C9/22—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
    • 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

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)
AT08749323T 2007-05-04 2008-05-05 Hochauftriebssystem am tragflügel eines flugzeugs ATE506255T1 (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
ATE506255T1 true ATE506255T1 (de) 2011-05-15

Family

ID=39745663

Family Applications (1)

Application Number Title Priority Date Filing Date
AT08749323T ATE506255T1 (de) 2007-05-04 2008-05-05 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
WO2014135945A1 (en) * 2013-03-06 2014-09-12 Bombardier Inc. High lift control method and system for aircraft
EP3106385A1 (de) * 2015-06-18 2016-12-21 BAE Systems PLC Flugzeugflügelsystem
EP3106386A1 (de) * 2015-06-18 2016-12-21 BAE Systems PLC Flugzeugflügelsystem
EP3310651B1 (de) * 2015-06-18 2019-08-07 BAE Systems PLC Flugzeugflügelsystem
ES2732025T3 (es) * 2015-06-18 2019-11-20 Bae Systems Plc Sistema de ala de aeronave
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
US20090240702A1 (en) * 2008-03-21 2009-09-24 Computerized Screening, Inc. Community based managed health kiosk and research database system

Also Published As

Publication number Publication date
US20100155542A1 (en) 2010-06-24
RU2009144844A (ru) 2011-06-10
WO2008135266A1 (en) 2008-11-13
DE602008006402D1 (de) 2011-06-01
EP2162352B1 (de) 2011-04-20
EP2162352A1 (de) 2010-03-17
DE102007020870A1 (de) 2008-11-13
WO2008135266A4 (en) 2009-01-22
US8286921B2 (en) 2012-10-16
CN101674980B (zh) 2012-10-24
RU2463211C2 (ru) 2012-10-10
CN101674980A (zh) 2010-03-17

Similar Documents

Publication Publication Date Title
ATE506255T1 (de) Hochauftriebssystem am tragflügel eines flugzeugs
ES2562675T3 (es) Superficie de control de aeronave
CA2651927A1 (en) Link mechanisms for gapped rigid krueger flaps, and associated systems and methods
ATE524380T1 (de) Betätigungssystem für vorderkantenhochauftriebsvorrichtung
US7300021B2 (en) Aerospace vehicle fairing systems and associated methods
US9302761B2 (en) High-lift device of flight vehicle
DE602007006808D1 (de) Hochauftriebssystem für ein flugzeug
WO2010124914A3 (en) Wind turbine rotor blade
DE602008004136D1 (de) Luftfahrzeug
ATE483627T1 (de) Flugzeugflügel
ATE393728T1 (de) Bewegliche vorderkantenklappe für einen hauptflügel der tragflächen eines flugzeugs und mit solch einer klappe versehener hauptflügel
BRPI1001262A2 (pt) dispositivo para ponta da asa não planar para asas de aeronave e asa compreendendo tal dispositivo para ponta da asa.
ATE543728T1 (de) Steuerungseinrichtung eines hubschrauber- hauptrotors
US10933976B2 (en) Leading edge high-lift device
EP1942053A3 (de) Pfeilflügel mit geringem Luftwiderstand
WO2011069887A3 (de) Hochauftriebssystem für ein flugzeug, verfahren zum bewegen einer auftriebsklappe und flugzeug mit einem hochauftriebssystem
FR2924681B1 (fr) Element aerodynamique allonge deformable en torsion
ATE542739T1 (de) Flugzeugflügel
US8573542B2 (en) Aerofoil slot blowing
CN110539882B (zh) 一种前缘变弯襟翼和前缘缝翼交界处流动优化方法及装置
WO2008141618A3 (de) Verfahren und einrichtung zur lärmreduzierung an einem hochauftriebssystem am tragflügel eines flugzeugs
WO2008141622A3 (de) Verfahren und einrichtung zur strömungskontrolle an einem hochauftriebssystem am tragflügel eines flugzeugs
CN211543875U (zh) 一种前缘变弯襟翼和前缘缝翼交界处流动优化装置
US20230192274A1 (en) Wingtip
GB2596677A9 (en) Variable-pitch stator blade for an aircraft turbine engine

Legal Events

Date Code Title Description
RER Ceased as to paragraph 5 lit. 3 law introducing patent treaties