BRPI0911484A2 - asa de sustentação para uma aeronave - Google Patents
asa de sustentação para uma aeronaveInfo
- Publication number
- BRPI0911484A2 BRPI0911484A2 BRPI0911484-0A BRPI0911484A BRPI0911484A2 BR PI0911484 A2 BRPI0911484 A2 BR PI0911484A2 BR PI0911484 A BRPI0911484 A BR PI0911484A BR PI0911484 A2 BRPI0911484 A2 BR PI0911484A2
- Authority
- BR
- Brazil
- Prior art keywords
- aircraft
- main wing
- aerodynamic body
- gap
- airfoil
- 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
- B64C9/02—Mounting or supporting thereof
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C7/00—Structures or fairings not otherwise provided for
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Tires In General (AREA)
- Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
- Toys (AREA)
Applications Claiming Priority (5)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US4711808P | 2008-04-23 | 2008-04-23 | |
DE102008020390A DE102008020390A1 (de) | 2008-04-23 | 2008-04-23 | Tragflügel für ein Luftfahrzeug |
SE102008020390.4 | 2008-04-23 | ||
US61/047,118 | 2008-04-23 | ||
PCT/EP2009/002965 WO2009130026A2 (de) | 2008-04-23 | 2009-04-23 | Tragflügel für ein luftfahrzeug |
Publications (1)
Publication Number | Publication Date |
---|---|
BRPI0911484A2 true BRPI0911484A2 (pt) | 2018-03-27 |
Family
ID=41130768
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BRPI0911484-0A BRPI0911484A2 (pt) | 2008-04-23 | 2009-04-23 | asa de sustentação para uma aeronave |
Country Status (9)
Country | Link |
---|---|
US (1) | US8931733B2 (pt) |
EP (1) | EP2280866B1 (pt) |
JP (1) | JP2011518712A (pt) |
CN (1) | CN102015443A (pt) |
BR (1) | BRPI0911484A2 (pt) |
CA (1) | CA2722229A1 (pt) |
DE (1) | DE102008020390A1 (pt) |
RU (1) | RU2494921C2 (pt) |
WO (1) | WO2009130026A2 (pt) |
Families Citing this family (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102008020390A1 (de) * | 2008-04-23 | 2009-11-05 | Airbus Deutschland Gmbh | Tragflügel für ein Luftfahrzeug |
US7938000B2 (en) * | 2008-09-25 | 2011-05-10 | Airbus Operations Gmbh | Method and measuring device for measuring overlap on an aircraft wing |
GB201018924D0 (en) * | 2010-11-09 | 2010-12-22 | Airbus Operations Ltd | Seal |
GB201110493D0 (en) * | 2011-06-21 | 2011-08-03 | Airbus Operations Ltd | Aircraft wing with wing tip device |
US9346533B2 (en) | 2011-10-19 | 2016-05-24 | The Boeing Company | Attachment of aircraft ribs to spars having variable geometry |
US9156559B2 (en) * | 2011-10-19 | 2015-10-13 | The Boeing Company | Segmented aircraft wing having solar arrays |
EP2864195B1 (en) * | 2012-06-21 | 2017-11-01 | Bombardier Inc. | Morphing wing for an aircraft |
US9139284B1 (en) | 2013-10-16 | 2015-09-22 | Sanjay Dhall | Telescopic wing with rotating structural spar |
CN103640689B (zh) * | 2013-11-28 | 2015-08-19 | 江西洪都航空工业集团有限责任公司 | 一种飞机全动舵面安装结构 |
US20150360768A1 (en) * | 2014-06-12 | 2015-12-17 | Troy A. Woodland | Mounting assembly for fully automatic slat |
CA2961872A1 (en) * | 2014-09-25 | 2016-03-31 | Bombardier Inc. | Morphing skin for an aircraft |
CN106143876B (zh) * | 2015-04-24 | 2023-11-24 | 空客(北京)工程技术中心有限公司 | 顶推装置、活动机构和飞行器 |
EP3498596A1 (en) * | 2017-12-14 | 2019-06-19 | Tallinn University of Technology | Actuating mechanism for trailing edge flaps and leading edge slats |
US10800511B2 (en) * | 2018-05-31 | 2020-10-13 | The Boeing Company | End seal device for a high-lift device of an aircraft |
CN112027063B (zh) * | 2020-09-11 | 2022-02-22 | 中国商用飞机有限责任公司 | 一种飞机试验模型的柔性机翼 |
Family Cites Families (27)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2526929A (en) * | 1948-05-29 | 1950-10-24 | Curtiss Wright Corp | Airplane flap extension |
GB797376A (en) * | 1955-09-29 | 1958-07-02 | Ml Aviation Co Ltd | Improvements in aircraft wings |
DE3149629C1 (de) * | 1981-12-15 | 1983-04-21 | Messerschmitt-Bölkow-Blohm GmbH, 8000 München | Einrichtung zum Abdichten eines Luftspaltes an einer Flugzeugklappe |
US4706907A (en) * | 1985-01-29 | 1987-11-17 | Eduard Kopylov | Aircraft |
US4739954A (en) * | 1986-12-29 | 1988-04-26 | Hamilton Terry W | Over-lap rib joint |
FR2609275B1 (fr) * | 1987-01-07 | 1989-03-31 | Riout Roland | Aile profilee a deformation commandee et applications en particulier aux aeronefs a ailes battantes |
US5356094A (en) * | 1987-03-04 | 1994-10-18 | Rick Sylvain | Scorpion wing |
US4824053A (en) * | 1987-08-27 | 1989-04-25 | Branko Sarh | Telescopic wing |
JPH03118897U (pt) * | 1990-03-16 | 1991-12-09 | ||
FR2670177B1 (fr) * | 1990-12-05 | 1993-01-22 | Snecma | Joint d'etancheite entre l'arriere du fuselage d'un avion et les volets exterieurs de son turboreacteur. |
US5176339A (en) * | 1991-09-30 | 1993-01-05 | Lord Corporation | Resilient pivot type aircraft mounting |
US5845877A (en) * | 1993-06-10 | 1998-12-08 | Lockheed Martin Corporation | Sealing assembly for reducing gaps between movable control surfaces of an aircraft |
US5645250A (en) * | 1993-08-26 | 1997-07-08 | Gevers; David E. | Multi-purpose aircraft |
US5695154A (en) * | 1995-08-21 | 1997-12-09 | Northrop Grumman Corporation | Gap filler device |
DE29706823U1 (de) | 1997-04-18 | 1997-10-02 | Lancken Fredrik Von Der | Vorrichtung zur Abdichtung eines Seitenspaltes an Klappen und Steuerflächen an Flügeln, Leitwerken und anderen umströmten Körpern |
US6209824B1 (en) | 1997-09-17 | 2001-04-03 | The Boeing Company | Control surface for an aircraft |
US6145791A (en) * | 1998-01-09 | 2000-11-14 | Northrop Grumman Corporation | Elastomeric transition for aircraft control surface |
US6076766A (en) * | 1998-07-01 | 2000-06-20 | Mcdonnell Douglas Corp. | Folding wing for an aircraft |
RU2187445C1 (ru) | 2000-12-15 | 2002-08-20 | Открытое акционерное общество "Туполев" | Устройство для соединения закрылков |
DE102004035921B4 (de) | 2004-07-23 | 2006-08-03 | Airbus Deutschland Gmbh | Klappen-Kopplungssystem für Luftfahrzeuge |
US7708231B2 (en) | 2005-11-21 | 2010-05-04 | The Boeing Company | Aircraft trailing edge devices, including devices having forwardly positioned hinge lines, and associated methods |
ES2301359B1 (es) | 2006-05-16 | 2009-05-01 | Airbus España, S.L. | Sistema de sellado del hueco existente entre el fuselaje y el timon de altura de un avion con estabilizador horizontal orientable. |
DE102006036389B4 (de) | 2006-08-02 | 2013-08-08 | Eads Deutschland Gmbh | Spaltfreies aerodynamisches Profil, insbesondere Rotorblatt |
US7789343B2 (en) * | 2007-07-24 | 2010-09-07 | The Boeing Company | Morphing aircraft with telescopic lifting and control surfaces |
US7866610B2 (en) * | 2007-12-28 | 2011-01-11 | Samuel Hall Bousfield | Telescoping wing and airfoil control mechanism |
DE102008020390A1 (de) * | 2008-04-23 | 2009-11-05 | Airbus Deutschland Gmbh | Tragflügel für ein Luftfahrzeug |
GB0807395D0 (en) * | 2008-04-23 | 2008-05-28 | Airbus Uk Ltd | Flight surface seal |
-
2008
- 2008-04-23 DE DE102008020390A patent/DE102008020390A1/de not_active Withdrawn
-
2009
- 2009-04-23 CN CN2009801146385A patent/CN102015443A/zh active Pending
- 2009-04-23 RU RU2010147708/11A patent/RU2494921C2/ru not_active IP Right Cessation
- 2009-04-23 BR BRPI0911484-0A patent/BRPI0911484A2/pt not_active IP Right Cessation
- 2009-04-23 EP EP09735269.4A patent/EP2280866B1/de not_active Not-in-force
- 2009-04-23 JP JP2011505431A patent/JP2011518712A/ja active Pending
- 2009-04-23 CA CA2722229A patent/CA2722229A1/en not_active Abandoned
- 2009-04-23 US US12/988,967 patent/US8931733B2/en not_active Expired - Fee Related
- 2009-04-23 WO PCT/EP2009/002965 patent/WO2009130026A2/de active Application Filing
Also Published As
Publication number | Publication date |
---|---|
DE102008020390A1 (de) | 2009-11-05 |
RU2494921C2 (ru) | 2013-10-10 |
CN102015443A (zh) | 2011-04-13 |
EP2280866B1 (de) | 2013-07-03 |
WO2009130026A3 (de) | 2010-01-28 |
US20110101172A1 (en) | 2011-05-05 |
EP2280866A2 (de) | 2011-02-09 |
WO2009130026A2 (de) | 2009-10-29 |
JP2011518712A (ja) | 2011-06-30 |
US8931733B2 (en) | 2015-01-13 |
RU2010147708A (ru) | 2012-05-27 |
CA2722229A1 (en) | 2009-10-29 |
WO2009130026A4 (de) | 2010-03-18 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
BRPI0911484A2 (pt) | asa de sustentação para uma aeronave | |
EP4292921A3 (en) | Aerial vehicle with deployable components | |
BRPI0915207A2 (pt) | dispositivo para formação de vórtices aerodinâmicos, bem como flape de regulagem e asa de sustentação com um dispositivo para formação de vórtices aerodinâmicos | |
WO2009133217A8 (es) | Conjunto soporte-maqueta de mínima interferencia aerodinámica para ensayos en régimen transónico en túnel de viento | |
ATE523424T1 (de) | Flugzeug mit einem trimmbaren höhenleitwerk | |
WO2015007259A3 (de) | Veränderbares flügelprofil | |
WO2008154066A3 (en) | Methods and apparatus for aircraft | |
EP2727826A3 (en) | Hinged raked wing tip | |
WO2010122324A3 (en) | Aircraft assembly and spar | |
WO2014158295A3 (en) | High-wing-aircraft fuselage support structure | |
WO2010063868A3 (es) | Superficie estabilizadora y de control direccional de aeronave. | |
BRPI0914948A2 (pt) | processo para a produção de uma parte estrutural, e componente de uma fuselagem ou de uma superfície de escoamento externa de um aeroplano | |
WO2011147571A3 (en) | A device for an adjustable flap of a wing | |
FR2946013B1 (fr) | Avion comportant une aile mobile suivant l'axe longitudinal du fuselage | |
BRPI0821427A2 (pt) | Componente estrutural de fuselagem da asa para a ligação duas asas de sustentação e uma seção de fuselagem em um avião. | |
ATE531619T1 (de) | Einziehbares fahrwerk für ein drehflügler | |
BRPI0910742A2 (pt) | dispositivo de acoplamento lateral para reter e guiar, pelo menos, um corpo aerodinâmico em relação à asa principal de um avião, asa de sustentação e avião com um dispositivo de acoplamento lateral deste tipo | |
WO2011002530A3 (en) | Reinforced inflatable wings for fitment-constrained air vehicles | |
BR112015020484A2 (pt) | aeronave | |
WO2011106733A3 (en) | Advanced aerodynamic and structural blade and wing design | |
BRPI0810569A2 (pt) | elemento estrutural de fuselagem de uma aeronave | |
WO2013064768A3 (fr) | Pylone d'accrochage pour turbomachine | |
ATE542739T1 (de) | Flugzeugflügel | |
WO2011054532A3 (en) | A wing of an aircraft | |
ATE382014T1 (de) | Fluggerät mit vorwärts ausfahrbarer vorderkante des rumpfes und der tragflügel |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
B08F | Application fees: dismissal - article 86 of industrial property law |
Free format text: REFERENTE AS 5A, 6A, 7A, 8A E 9A ANUIDADES. |
|
B08K | Lapse as no evidence of payment of the annual fee has been furnished to inpi (acc. art. 87) |