JP2011504149A5 - 航空機翼の後縁フラップを移動させるための装置及び同装置を備えた航空機 - Google Patents
航空機翼の後縁フラップを移動させるための装置及び同装置を備えた航空機 Download PDFInfo
- Publication number
- JP2011504149A5 JP2011504149A5 JP2010534410A JP2010534410A JP2011504149A5 JP 2011504149 A5 JP2011504149 A5 JP 2011504149A5 JP 2010534410 A JP2010534410 A JP 2010534410A JP 2010534410 A JP2010534410 A JP 2010534410A JP 2011504149 A5 JP2011504149 A5 JP 2011504149A5
- Authority
- JP
- Japan
- Prior art keywords
- aircraft
- moving
- trailing edge
- edge flap
- same device
- 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.)
- Withdrawn
Links
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102007055669A DE102007055669A1 (de) | 2007-11-21 | 2007-11-21 | Landeklappenkinematik angetrieben über Ritzelantrieb |
PCT/EP2008/009884 WO2009065597A1 (de) | 2007-11-21 | 2008-11-21 | Landeklappenkinematik angetrieben über ritzelantrieb |
Publications (2)
Publication Number | Publication Date |
---|---|
JP2011504149A JP2011504149A (ja) | 2011-02-03 |
JP2011504149A5 true JP2011504149A5 (ja) | 2012-01-19 |
Family
ID=40585698
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2010534410A Withdrawn JP2011504149A (ja) | 2007-11-21 | 2008-11-21 | ピニオンドライブによって駆動される着陸フラップ運動 |
Country Status (9)
Country | Link |
---|---|
US (1) | US8393570B2 (ja) |
EP (1) | EP2274200B1 (ja) |
JP (1) | JP2011504149A (ja) |
CN (1) | CN101868407B (ja) |
BR (1) | BRPI0819837A2 (ja) |
CA (1) | CA2706413A1 (ja) |
DE (1) | DE102007055669A1 (ja) |
RU (1) | RU2010125100A (ja) |
WO (1) | WO2009065597A1 (ja) |
Families Citing this family (22)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102007009060A1 (de) * | 2007-02-23 | 2008-08-28 | Airbus Deutschland Gmbh | Spoiler für eine aerodynamisch wirksame Fläche eines Luftfahrzeugs |
DE102009052641A1 (de) * | 2009-11-10 | 2011-05-12 | Airbus Operations Gmbh | Hinterkantenklappensystem |
GB0920969D0 (en) | 2009-11-27 | 2010-01-13 | Airbus Operations Ltd | Trailing edge flap |
GB0920968D0 (en) * | 2009-11-27 | 2010-01-13 | Airbus Operations Ltd | Trailing edge flap |
GB0921007D0 (en) * | 2009-11-30 | 2010-01-13 | Airbus Operations Ltd | Trailing edge flap |
CN102787772A (zh) * | 2011-08-05 | 2012-11-21 | 薛广振 | 空间合叶 |
WO2013172914A2 (en) * | 2012-02-27 | 2013-11-21 | Sinhatech | Self adjusting deturbulator enhanced flap and wind deflector |
EP2746151B1 (en) * | 2012-12-19 | 2017-04-12 | Airbus Operations GmbH | Flap system for an aircraft, method for adjusting the lift of an aircraft and aircraft comprising a main wing and at least one flap system |
JP6144487B2 (ja) * | 2012-12-26 | 2017-06-07 | 三菱航空機株式会社 | フラップの展開装置、及び、航空機 |
EP2805879B1 (en) * | 2013-05-22 | 2017-07-05 | Airbus Operations GmbH | Flap arrangement for a wing of an aircraft and an aircraft with a wing comprising such a flap arrangement |
US10017243B2 (en) * | 2013-09-24 | 2018-07-10 | The Boeing Company | Adaptive trailing edge actuator system and method |
CN106005368B (zh) * | 2016-05-16 | 2018-04-13 | 中国航空工业集团公司西安飞机设计研究所 | 一种可变后缘的柔性机翼颤振模型 |
US11046425B2 (en) * | 2016-05-20 | 2021-06-29 | Bombardier Inc. | Apparatus and methods for actuating a double-slotted flap using a slave screw |
BR102016020505B1 (pt) * | 2016-09-05 | 2022-08-02 | Embraer S.A | Mecanismo de deflexão de painéis de flaps de aeronave |
CN107600389B (zh) * | 2017-09-04 | 2020-05-08 | 江西洪都航空工业集团有限责任公司 | 一种导滑架式后缘襟翼运动方法 |
CN108791539A (zh) * | 2018-06-05 | 2018-11-13 | 广东工业大学 | 一种宏微结合的调节装置 |
US10926864B2 (en) * | 2018-07-27 | 2021-02-23 | The Boeing Company | Camber adjustment systems and methods for aircraft wings |
CN109515686B (zh) * | 2018-11-07 | 2021-09-21 | 西安航空学院 | 一种自适应后缘机动襟翼机构 |
CN111907694B (zh) * | 2020-06-22 | 2022-02-22 | 哈尔滨工业大学(深圳)(哈尔滨工业大学深圳科技创新研究院) | 一种可变弯度的机翼后缘与机翼 |
CN112977821B (zh) * | 2021-03-17 | 2023-04-07 | 北京瑞盈智拓科技发展有限公司 | 一种输电线路巡检飞行器 |
CN115817795B (zh) * | 2022-12-27 | 2023-08-01 | 江苏华阳重工股份有限公司 | 一种高性能襟翼舵体 |
CN116176836B (zh) * | 2023-02-17 | 2024-07-19 | 北京科技大学 | 一种基于弧面翼的仿生扑翼飞行器转向机构 |
Family Cites Families (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1868748A (en) | 1931-11-28 | 1932-07-26 | Herbert J Hogan | Variable camber airfoil |
DE605554C (de) | 1932-01-19 | 1934-11-14 | Zap Dev Corp | Vorrichtung zur Erhoehung des Auftriebes von Flugzeugtragfluegeln |
US2146014A (en) * | 1936-05-06 | 1939-02-07 | Charles H Grant | Variable camber wing |
US2222187A (en) * | 1939-03-11 | 1940-11-19 | James S Weatherbee | Split wing flap for airplanes |
US2325548A (en) | 1939-11-20 | 1943-07-27 | Roos Helmut | Control means for rudders and the flaps thereon |
GB558047A (en) | 1942-07-21 | 1943-12-16 | Armstrong Whitworth Co Eng | Improvements relating to the control of aircraft |
US2966808A (en) * | 1958-12-23 | 1961-01-03 | Curtiss Wright Corp | Power actuated hinge device |
GB941904A (en) | 1960-12-27 | 1963-11-13 | Ludwig Bolkow | Improvements relating to aircraft having hinged wings, flaps, fins or like parts with control surfaces |
US3698668A (en) * | 1971-04-08 | 1972-10-17 | Boeing Co | Variable camber airfoil |
US4131253A (en) | 1977-07-21 | 1978-12-26 | The Boeing Company | Variable camber trailing edge for airfoil |
DE2839050A1 (de) | 1977-09-08 | 1979-03-22 | Fritz Mahrer | Flugzeug mit fowler-fluegel |
US4471928A (en) * | 1980-08-13 | 1984-09-18 | The Boeing Company | Extendible airfoil track assembly |
US4742730A (en) * | 1982-09-30 | 1988-05-10 | The Boeing Company | Failsafe rotary actuator |
WO1985000573A1 (en) | 1983-07-15 | 1985-02-14 | Wildensteiner Otto M | Reversible camber airfoil |
US5098043A (en) * | 1990-02-27 | 1992-03-24 | Grumman Aerospace Corporation | Integrated power hinge actuator |
DE19501038C1 (de) * | 1995-01-16 | 1996-05-15 | Christa Michel | Flugzeug-Tragfläche |
US6231012B1 (en) | 1996-05-15 | 2001-05-15 | Michael J. Cacciola | No-back/offset gear box |
-
2007
- 2007-11-21 DE DE102007055669A patent/DE102007055669A1/de not_active Ceased
-
2008
- 2008-11-21 BR BRPI0819837-3A patent/BRPI0819837A2/pt not_active IP Right Cessation
- 2008-11-21 JP JP2010534410A patent/JP2011504149A/ja not_active Withdrawn
- 2008-11-21 CA CA2706413A patent/CA2706413A1/en not_active Abandoned
- 2008-11-21 US US12/743,895 patent/US8393570B2/en active Active
- 2008-11-21 CN CN2008801173049A patent/CN101868407B/zh not_active Expired - Fee Related
- 2008-11-21 WO PCT/EP2008/009884 patent/WO2009065597A1/de active Application Filing
- 2008-11-21 EP EP08852336.0A patent/EP2274200B1/de not_active Not-in-force
- 2008-11-21 RU RU2010125100/11A patent/RU2010125100A/ru not_active Application Discontinuation
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