ATE492468T1 - Luftfahrzeug - Google Patents
LuftfahrzeugInfo
- Publication number
- ATE492468T1 ATE492468T1 AT08749698T AT08749698T ATE492468T1 AT E492468 T1 ATE492468 T1 AT E492468T1 AT 08749698 T AT08749698 T AT 08749698T AT 08749698 T AT08749698 T AT 08749698T AT E492468 T1 ATE492468 T1 AT E492468T1
- Authority
- AT
- Austria
- Prior art keywords
- flap
- airfoil
- rotation axis
- aircraft
- fuselage
- Prior art date
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
- B64C9/16—Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing
-
- 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
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/30—Wing lift efficiency
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Transmission Devices (AREA)
- Radio Relay Systems (AREA)
- Details Of Aerials (AREA)
- Fluid-Pressure Circuits (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Toys (AREA)
- Steering Controls (AREA)
- Tires In General (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US92606707P | 2007-04-24 | 2007-04-24 | |
PCT/EP2008/054985 WO2008129074A1 (en) | 2007-04-24 | 2008-04-24 | Aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
ATE492468T1 true ATE492468T1 (de) | 2011-01-15 |
Family
ID=39684346
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
AT08749698T ATE492468T1 (de) | 2007-04-24 | 2008-04-24 | Luftfahrzeug |
Country Status (9)
Country | Link |
---|---|
US (1) | US8408499B2 (de) |
EP (1) | EP2148813B1 (de) |
CN (1) | CN101678893B (de) |
AT (1) | ATE492468T1 (de) |
BR (1) | BRPI0811030A2 (de) |
CA (1) | CA2682680C (de) |
DE (1) | DE602008004136D1 (de) |
RU (1) | RU2009140962A (de) |
WO (1) | WO2008129074A1 (de) |
Families Citing this family (18)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102007023394A1 (de) * | 2007-05-18 | 2008-11-20 | Airbus Deutschland Gmbh | Verfahren und Einrichtung zur Fehlerdetektierung im Lastpfad eines Spindelaktuators |
GB0808349D0 (en) * | 2008-05-09 | 2008-06-18 | Airbus Uk Ltd | Spoiler deployment mechanism |
DE102009002222A1 (de) * | 2009-04-06 | 2010-10-07 | Airbus Deutschland Gmbh | Flügel eines Flugzeugs oder eines Raumfahrzeugs mit einem beweglichen Strömungskörper |
CN102905971B (zh) * | 2010-05-21 | 2015-07-15 | 空中客车简易股份公司 | 整流板联动装置 |
DE102010051216A1 (de) * | 2010-11-12 | 2012-05-16 | Airbus Operations Gmbh | Seitenrudersystem an einem Flugzeug |
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 |
US8684316B2 (en) | 2011-09-23 | 2014-04-01 | The Boeing Company | Aircraft flap mechanism having compact large fowler motion providing multiple cruise positions |
GB201117340D0 (en) * | 2011-10-07 | 2011-11-23 | Airbus Uk Ltd | Flat support |
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 |
US10099770B2 (en) * | 2013-07-26 | 2018-10-16 | Icon Aircraft, Inc. | Manuel wing-fold mechanism |
CN103879550A (zh) * | 2014-01-16 | 2014-06-25 | 李竟儒 | 一种在飞机机翼下设置有举力装置的飞机 |
FR3018767B1 (fr) * | 2014-03-21 | 2018-01-12 | Airbus Operations | Ensemble de support pour un systeme de volet d'aile d'un avion. |
CN104400091B (zh) * | 2014-12-01 | 2017-03-08 | 江西洪都航空工业集团有限责任公司 | 用于非水平端面的锪工装 |
CN110072773B (zh) * | 2016-12-12 | 2022-10-21 | 庞巴迪公司 | 飞机缝翼 |
EP3339164A1 (de) * | 2016-12-22 | 2018-06-27 | Airbus Operations GmbH | Flügel für ein flugzeug |
CA3046256A1 (en) * | 2018-06-18 | 2019-12-18 | Bombardier Inc. | Aircraft wing with deployable flap |
US11518496B2 (en) | 2019-08-27 | 2022-12-06 | The Boeing Company | Flap actuation systems for aircraft |
CN112357055B (zh) * | 2020-11-23 | 2022-03-18 | 西湖大学 | 一种用于航行器的翼片结构、机翼结构以及航行器 |
Family Cites Families (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2246116A (en) * | 1937-10-28 | 1941-06-17 | Messerschmitt Boelkow Blohm | Airplane wing structure |
US2284519A (en) * | 1939-09-14 | 1942-05-26 | Bell Aircraft Corp | Airplane |
GB559546A (en) * | 1942-05-18 | 1944-02-24 | Phillips & Powis Aircraft Ltd | Improvements in aircraft flap actuating gear |
US2524605A (en) | 1944-11-23 | 1950-10-03 | Sncaso | Arrangement for securing and controlling a movable flap at the trailing edge of an airplane wing |
US2670909A (en) * | 1950-03-01 | 1954-03-02 | Bell Aircraft Corp | Actuating mechanism for aircraft extensible flaps |
US4470569A (en) * | 1981-12-28 | 1984-09-11 | Mcdonnell Douglas Corporation | Locking, redundant slat drive mechanism |
US4498647A (en) * | 1982-03-15 | 1985-02-12 | Mcdonnel Douglas Corporation | Surface hold-down mechanism |
US4614320A (en) * | 1984-03-27 | 1986-09-30 | Rutan Elbert L | Aircraft wing flap |
US4784355A (en) | 1986-11-10 | 1988-11-15 | The United States Of America As Represented By The Secretary Of The Air Force | Flap system for short takeoff and landing aircraft |
US5836550A (en) * | 1996-11-27 | 1998-11-17 | Boeing Company | Mechanism for streamwise fowler deployment of the wing trailing or leading edge |
US6464176B2 (en) * | 2000-07-26 | 2002-10-15 | Honda Giken Kogyo Kabushiki Kaisha | Flap operating device |
-
2008
- 2008-04-24 AT AT08749698T patent/ATE492468T1/de not_active IP Right Cessation
- 2008-04-24 CA CA2682680A patent/CA2682680C/en active Active
- 2008-04-24 EP EP08749698A patent/EP2148813B1/de active Active
- 2008-04-24 CN CN2008800134494A patent/CN101678893B/zh active Active
- 2008-04-24 US US12/595,886 patent/US8408499B2/en active Active
- 2008-04-24 WO PCT/EP2008/054985 patent/WO2008129074A1/en active Application Filing
- 2008-04-24 DE DE602008004136T patent/DE602008004136D1/de active Active
- 2008-04-24 RU RU2009140962/11A patent/RU2009140962A/ru not_active Application Discontinuation
- 2008-04-24 BR BRPI0811030A patent/BRPI0811030A2/pt not_active IP Right Cessation
Also Published As
Publication number | Publication date |
---|---|
CA2682680C (en) | 2015-11-03 |
CA2682680A1 (en) | 2008-10-30 |
US8408499B2 (en) | 2013-04-02 |
CN101678893A (zh) | 2010-03-24 |
DE602008004136D1 (de) | 2011-02-03 |
CN101678893B (zh) | 2013-05-22 |
EP2148813A1 (de) | 2010-02-03 |
WO2008129074A1 (en) | 2008-10-30 |
EP2148813B1 (de) | 2010-12-22 |
WO2008129074B1 (en) | 2008-12-24 |
RU2009140962A (ru) | 2011-05-27 |
BRPI0811030A2 (pt) | 2017-05-09 |
US20100116928A1 (en) | 2010-05-13 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
RER | Ceased as to paragraph 5 lit. 3 law introducing patent treaties |