ATE513735T1 - Flügel - Google Patents
FlügelInfo
- Publication number
- ATE513735T1 ATE513735T1 AT08717544T AT08717544T ATE513735T1 AT E513735 T1 ATE513735 T1 AT E513735T1 AT 08717544 T AT08717544 T AT 08717544T AT 08717544 T AT08717544 T AT 08717544T AT E513735 T1 ATE513735 T1 AT E513735T1
- Authority
- AT
- Austria
- Prior art keywords
- wing
- track
- moveable body
- moveable
- roller
- 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
- B64C9/22—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
-
- 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
- Y02T50/40—Weight reduction
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| EP07103891 | 2007-03-09 | ||
| EP07104630A EP1972547A1 (de) | 2007-03-21 | 2007-03-21 | Flügelvorderkantenvorrichtung |
| PCT/EP2008/052797 WO2008110521A1 (en) | 2007-03-09 | 2008-03-07 | Wing |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| ATE513735T1 true ATE513735T1 (de) | 2011-07-15 |
Family
ID=39469487
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| AT08717544T ATE513735T1 (de) | 2007-03-09 | 2008-03-07 | Flügel |
Country Status (4)
| Country | Link |
|---|---|
| US (1) | US8245982B2 (de) |
| EP (1) | EP2134597B1 (de) |
| AT (1) | ATE513735T1 (de) |
| WO (1) | WO2008110521A1 (de) |
Families Citing this family (37)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB0722425D0 (en) * | 2007-11-15 | 2007-12-27 | Airbus Uk Ltd | Slat support funk plate |
| GB0805599D0 (en) * | 2008-03-28 | 2008-04-30 | Airbus Uk Ltd | Slat deployment mechanism |
| BE1018114A5 (fr) * | 2008-05-06 | 2010-05-04 | Sonaca Sociutu Anonyme | Aile d'aeronef comprenant un volet mobile de bord d'attaque equipe d'un rail suiveur contraint en deplacement selon une trajectoire en arc de cercle |
| WO2011143794A1 (en) * | 2010-05-21 | 2011-11-24 | Airbus S.A.S. | Droop panel linkage |
| GB201008773D0 (en) * | 2010-05-26 | 2010-07-14 | Airbus Uk Ltd | Aircraft slat assembly |
| EP2538167A1 (de) * | 2011-06-23 | 2012-12-26 | Nederlandse Organisatie voor toegepast -natuurwetenschappelijk onderzoek TNO | Explosions- und bruchsichere Wandabschnitte zur Verwendung in Strukturen wie Schiffen |
| 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 |
| US8783604B2 (en) * | 2011-10-21 | 2014-07-22 | Raytheon Company | Aircraft wing with knuckled rib structure |
| GB201209686D0 (en) * | 2012-05-31 | 2012-07-18 | Airbus Operations Ltd | A slat support assembly |
| GB201214143D0 (en) * | 2012-08-08 | 2012-09-19 | Airbus Operations Ltd | Slat support and deployment coupling |
| DE102012112405B4 (de) * | 2012-12-17 | 2017-06-08 | Airbus Defence and Space GmbH | Gekrümmter Flügelabschnitt mit einer schwenkbaren Hinterkantenklappe |
| JP6178581B2 (ja) * | 2013-01-29 | 2017-08-09 | 三菱航空機株式会社 | 航空機のスラット、スラットの取り付け位置調整方法、及び、航空機 |
| US9163648B2 (en) | 2013-02-27 | 2015-10-20 | Woodward, Inc. | Rotary piston type actuator with a central actuation assembly |
| US9234535B2 (en) | 2013-02-27 | 2016-01-12 | Woodward, Inc. | Rotary piston type actuator |
| US9593696B2 (en) | 2013-02-27 | 2017-03-14 | Woodward, Inc. | Rotary piston type actuator with hydraulic supply |
| US9631645B2 (en) | 2013-02-27 | 2017-04-25 | Woodward, Inc. | Rotary piston actuator anti-rotation configurations |
| US8955425B2 (en) | 2013-02-27 | 2015-02-17 | Woodward, Inc. | Rotary piston type actuator with pin retention features |
| US9816537B2 (en) | 2013-02-27 | 2017-11-14 | Woodward, Inc. | Rotary piston type actuator with a central actuation assembly |
| US9476434B2 (en) | 2013-02-27 | 2016-10-25 | Woodward, Inc. | Rotary piston type actuator with modular housing |
| GB2533311A (en) * | 2014-12-15 | 2016-06-22 | Airbus Operations Ltd | A track container |
| EP3106386A1 (de) * | 2015-06-18 | 2016-12-21 | BAE Systems PLC | Flugzeugflügelsystem |
| US10633079B2 (en) | 2015-06-18 | 2020-04-28 | Bae Systems Plc | Aircraft wing system |
| ES2746872T3 (es) | 2015-06-18 | 2020-03-09 | Bae Systems Plc | Sistema de ala de una aeronave |
| EP3326909B1 (de) * | 2016-11-23 | 2019-10-02 | Airbus Operations GmbH | Vorflügelanordnung |
| EP3378762A1 (de) | 2017-03-24 | 2018-09-26 | Airbus Operations GmbH | Flügel für ein flugzeug |
| EP3378760A1 (de) | 2017-03-24 | 2018-09-26 | Airbus Operations GmbH | Flugzeugflügel |
| EP3395678B1 (de) | 2017-04-26 | 2021-05-26 | Asco Industries NV | Führungsanordnung für eine hochauftriebsvorrichtungsträgerbahn einer tragflächenvorderkante |
| ES2886667T3 (es) | 2017-12-19 | 2021-12-20 | Asco Ind Nv | Sistema de despliegue para un dispositivo de borde de ataque de sustentación elevada de perfil aerodinámico |
| EP3501978B1 (de) | 2017-12-21 | 2021-03-10 | Airbus Operations GmbH | Flügel für ein flugzeug |
| US11845550B2 (en) * | 2019-02-28 | 2023-12-19 | Airbus Operations Gmbh | Wing leading-edge device and a wing having such a wing leading-edge device |
| US11383821B2 (en) | 2019-03-22 | 2022-07-12 | Airbus Operations Gmbh | Wing leading-edge device and a wing having such a wing leading-edge device |
| US11199248B2 (en) | 2019-04-30 | 2021-12-14 | Woodward, Inc. | Compact linear to rotary actuator |
| CN113950445B (zh) | 2019-07-09 | 2025-05-23 | 空中客车德国运营有限责任公司 | 用于飞行器的前缘布置结构 |
| CN115667734A (zh) | 2020-04-08 | 2023-01-31 | 伍德沃德有限公司 | 带有中心致动组件的旋转活塞型致动器 |
| EP4112450A1 (de) * | 2021-06-30 | 2023-01-04 | Airbus Operations GmbH | Flügel für ein flugzeug |
| EP4140878B1 (de) * | 2021-08-31 | 2025-04-23 | Airbus Operations GmbH | Anordnung für eine hochauftriebsvorrichtung einer tragflächenvorderkante und flügel für ein flugzeug |
| US12179919B2 (en) * | 2023-04-12 | 2024-12-31 | The Boeing Company | Slat movement system for aircraft |
Family Cites Families (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4399970A (en) * | 1980-11-13 | 1983-08-23 | The Boeing Company | Wing leading edge slat |
| US4470569A (en) * | 1981-12-28 | 1984-09-11 | Mcdonnell Douglas Corporation | Locking, redundant slat drive mechanism |
| US4650140A (en) * | 1985-12-30 | 1987-03-17 | The Boeing Company | Wind edge movable airfoil having variable camber |
| US5544847A (en) * | 1993-11-10 | 1996-08-13 | The Boeing Company | Leading edge slat/wing combination |
| US5927656A (en) | 1996-06-26 | 1999-07-27 | The Boeing Company | Wing leading edge flap and method therefor |
| GB0410375D0 (en) | 2004-05-10 | 2004-06-16 | Airbus Uk Ltd | High lift device for an aircraft |
| US7264206B2 (en) * | 2004-09-30 | 2007-09-04 | The Boeing Company | Leading edge flap apparatuses and associated methods |
| DE102005027749B4 (de) * | 2005-06-16 | 2011-07-28 | Airbus Operations GmbH, 21129 | Auftriebserhöhende Klappe, insbesondere Nasenklappe, für einen aerodynamisch wirksamen Flügel |
| DE102005044549B4 (de) * | 2005-09-17 | 2008-04-17 | Eads Deutschland Gmbh | Flugzeugflügel mit ausfahrbarer Nasenklappe |
| US20070102587A1 (en) * | 2005-11-07 | 2007-05-10 | The Boeing Company | Wing leading edge slat system |
| EP2021243B1 (de) * | 2006-04-27 | 2018-10-24 | Flexsys, Inc. | Anpassungsfähiges strukturkonzept für veränderliche oberflächenkonturen |
| US7578484B2 (en) * | 2006-06-14 | 2009-08-25 | The Boeing Company | Link mechanisms for gapped rigid krueger flaps, and associated systems and methods |
-
2008
- 2008-03-07 US US12/449,886 patent/US8245982B2/en not_active Expired - Fee Related
- 2008-03-07 EP EP08717544A patent/EP2134597B1/de not_active Not-in-force
- 2008-03-07 AT AT08717544T patent/ATE513735T1/de not_active IP Right Cessation
- 2008-03-07 WO PCT/EP2008/052797 patent/WO2008110521A1/en not_active Ceased
Also Published As
| Publication number | Publication date |
|---|---|
| EP2134597B1 (de) | 2011-06-22 |
| US20100163685A1 (en) | 2010-07-01 |
| EP2134597A1 (de) | 2009-12-23 |
| US8245982B2 (en) | 2012-08-21 |
| WO2008110521A1 (en) | 2008-09-18 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| RER | Ceased as to paragraph 5 lit. 3 law introducing patent treaties |