ATE484449T1 - Flugzeugflügel mit mehreren abnehmbaren elementen - Google Patents
Flugzeugflügel mit mehreren abnehmbaren elementenInfo
- Publication number
- ATE484449T1 ATE484449T1 AT08761892T AT08761892T ATE484449T1 AT E484449 T1 ATE484449 T1 AT E484449T1 AT 08761892 T AT08761892 T AT 08761892T AT 08761892 T AT08761892 T AT 08761892T AT E484449 T1 ATE484449 T1 AT E484449T1
- Authority
- AT
- Austria
- Prior art keywords
- parts
- wing
- aircraft wing
- detachable elements
- several detachable
- Prior art date
Links
- 230000008878 coupling Effects 0.000 abstract 2
- 238000010168 coupling process Methods 0.000 abstract 2
- 238000005859 coupling reaction Methods 0.000 abstract 2
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/26—Attaching the wing or tail units or stabilising surfaces
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/38—Adjustment of complete wings or parts thereof
- B64C3/56—Folding or collapsing to reduce overall dimensions of aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Connection Of Plates (AREA)
- Tires In General (AREA)
- Retarders (AREA)
- General Details Of Gearings (AREA)
- Adornments (AREA)
- Prostheses (AREA)
- Filling Or Discharging Of Gas Storage Vessels (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Stackable Containers (AREA)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR0700292A FR2911320B1 (fr) | 2007-01-16 | 2007-01-16 | Voilure d'aeronef en plusieurs elements demontables |
| PCT/FR2008/050014 WO2008099097A2 (fr) | 2007-01-16 | 2008-01-07 | Voilure d'aeronef en plusieurs elements demontables |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| ATE484449T1 true ATE484449T1 (de) | 2010-10-15 |
Family
ID=38370466
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| AT08761892T ATE484449T1 (de) | 2007-01-16 | 2008-01-07 | Flugzeugflügel mit mehreren abnehmbaren elementen |
Country Status (9)
| Country | Link |
|---|---|
| US (1) | US8128032B2 (de) |
| EP (1) | EP2121434B1 (de) |
| AT (1) | ATE484449T1 (de) |
| CA (1) | CA2676334A1 (de) |
| DE (1) | DE602008003005D1 (de) |
| FR (1) | FR2911320B1 (de) |
| IL (1) | IL199724A (de) |
| WO (1) | WO2008099097A2 (de) |
| ZA (1) | ZA200904716B (de) |
Families Citing this family (34)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US7975965B2 (en) * | 2008-05-13 | 2011-07-12 | The Boeing Company | Wing tip joint in airfoils |
| FR2939100B1 (fr) * | 2008-12-01 | 2010-12-31 | Airbus France | Ensemble moteur pour aeronef comprenant une structure rigide modulaire de mat d'accrochage |
| GB0910938D0 (en) | 2009-06-25 | 2009-08-05 | Airbus Operations Ltd | Method of manufacturing a structure |
| JP2012245832A (ja) * | 2011-05-26 | 2012-12-13 | Kawada Kogyo Kk | 小型無人飛行機の翼構造 |
| WO2013070296A2 (en) * | 2011-08-19 | 2013-05-16 | Aerovironment, Inc. | Aircraft system for reduced observer visibility |
| US10538307B2 (en) * | 2011-10-01 | 2020-01-21 | The Boeing Company | Hinged raked wing tip |
| US9908612B2 (en) * | 2011-10-01 | 2018-03-06 | The Boeing Company | Fold wing tip having stub spar |
| US20130114994A1 (en) | 2011-11-04 | 2013-05-09 | Robert Erik Grip | Truss end pad fitting |
| US9914523B2 (en) * | 2012-10-30 | 2018-03-13 | The Boeing Company | Wing hinge assembly including hinged torque boxes |
| US9481446B2 (en) | 2012-10-30 | 2016-11-01 | The Boeing Company | System for latching and locking a foldable airfoil |
| US9376207B2 (en) * | 2013-08-23 | 2016-06-28 | Becklin Holdings, Inc. | Fuselage indexing system and method |
| CN103625631A (zh) * | 2013-08-23 | 2014-03-12 | 中国航空工业集团公司西安飞机设计研究所 | 一种垂尾对接结构设计方法 |
| GB2547957A (en) * | 2016-05-24 | 2017-09-06 | Airbus Operations Ltd | Winglet |
| GB2551311A (en) | 2016-05-24 | 2017-12-20 | Airbus Operations Ltd | Winglet |
| US11148781B2 (en) * | 2016-09-09 | 2021-10-19 | Skydio, Inc. | Airframe attachments |
| CN107215451A (zh) * | 2017-06-16 | 2017-09-29 | 中电科芜湖通用航空产业技术研究院有限公司 | 一种通用飞机的机翼连接结构 |
| US10801469B2 (en) * | 2017-11-07 | 2020-10-13 | General Electric Company | Wind blade joints with floating connectors |
| PL241373B1 (pl) * | 2017-12-13 | 2022-09-19 | Flaris Spolka Z Ograniczona Odpowiedzialnoscia | Połączenie struktur metalowo-kompozytowych samolotu |
| CN108750072A (zh) * | 2018-06-06 | 2018-11-06 | 东汉太阳能无人机技术有限公司 | 一种无人机的机翼及无人机 |
| CN108639307A (zh) * | 2018-06-22 | 2018-10-12 | 西安飞机工业(集团)有限责任公司 | 一种飞机外挂接头的连接结构 |
| CN108910016A (zh) * | 2018-07-23 | 2018-11-30 | 上海歌尔泰克机器人有限公司 | 快拆机翼和无人飞行器 |
| US11066148B2 (en) * | 2018-08-06 | 2021-07-20 | The Boeing Company | Folding wing hinge, aircraft and method therefor |
| CN108791808A (zh) * | 2018-08-23 | 2018-11-13 | 西安三翼航空科技有限公司 | 一种快装式旋翼撑杆组件 |
| CN109050875A (zh) * | 2018-08-23 | 2018-12-21 | 西安三翼航空科技有限公司 | 一种尾翼连接机构 |
| US11254412B2 (en) | 2019-03-29 | 2022-02-22 | The Boeing Company | Foldable raked wing tips having aerodynamic devices |
| GB2583465A (en) * | 2019-04-18 | 2020-11-04 | Airbus Operations Ltd | Wingtip device attachment |
| CN110588952A (zh) * | 2019-10-11 | 2019-12-20 | 复旦大学 | 一种机翼可快速拆装的固定翼飞行器及机翼快速安装、拆除方法 |
| CN110775248A (zh) * | 2019-10-21 | 2020-02-11 | 深圳市道通智能航空技术有限公司 | 一种无人机 |
| CN110615097A (zh) * | 2019-10-23 | 2019-12-27 | 深圳市道通智能航空技术有限公司 | 一种无人飞行器 |
| TR2021015233A1 (tr) * | 2021-09-29 | 2023-04-24 | Tusas Tuerk Havacilik Ve Uzay Sanayii Anonim Sirketi | Bir sabit kanat kontrol mekanizması. |
| KR102897777B1 (ko) * | 2023-06-14 | 2025-12-10 | 주식회사 아크로사 | 하이브리드 무인항공기의 동체와 고정익과 회전익 장치 간에 탈착식 결합을 실현하는 구조물 |
| CN119503113A (zh) * | 2023-08-25 | 2025-02-25 | 峰飞航空科技(昆山)有限公司 | 飞行器及其鸭翼与机臂连接结构 |
| CN119503146A (zh) * | 2023-08-25 | 2025-02-25 | 峰飞航空科技(昆山)有限公司 | 飞行器及其鸭翼与机臂连接方法 |
| EP4570646A1 (de) * | 2023-12-14 | 2025-06-18 | Airbus Operations, S.L.U. | Strukturelle verbindung zur befestigung einer abnehmbaren flugzeugplatte an einem rumpfabschnitt |
Family Cites Families (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| BE369829A (de) * | ||||
| US3093075A (en) * | 1960-07-29 | 1963-06-11 | Edgar J Garrett | Fin latch assembly |
| DE2005372A1 (de) * | 1970-02-06 | 1971-08-19 | Schempp-Hirth KG, 7312 Kirchheim | Verbindung von Tragflügelteilen bei drei- oder mehrteiligen Tragflügeln für Segel- oder Motorsegelflugzeuge ohne Oberflächenöffnungen |
| US3640492A (en) * | 1970-02-19 | 1972-02-08 | Northrop Corp | Modular aircraft structures |
| US5035382A (en) * | 1989-04-17 | 1991-07-30 | Aerovironment, Inc. | Rapid assembly aircraft for ground surveillance |
| US6224451B1 (en) * | 1999-09-13 | 2001-05-01 | Thunder Tiger Corp. | Assembling structure for main wing of a model airplane |
| US6425794B1 (en) * | 1999-10-05 | 2002-07-30 | Alejandro Velasco Levy | Impact-absorbing wing connection system for model aircraft |
| US7237750B2 (en) * | 2004-10-29 | 2007-07-03 | L3 Communications | Autonomous, back-packable computer-controlled breakaway unmanned aerial vehicle (UAV) |
-
2007
- 2007-01-16 FR FR0700292A patent/FR2911320B1/fr not_active Expired - Fee Related
-
2008
- 2008-01-07 CA CA002676334A patent/CA2676334A1/fr not_active Abandoned
- 2008-01-07 AT AT08761892T patent/ATE484449T1/de active
- 2008-01-07 ZA ZA200904716A patent/ZA200904716B/xx unknown
- 2008-01-07 US US12/523,486 patent/US8128032B2/en not_active Expired - Fee Related
- 2008-01-07 DE DE602008003005T patent/DE602008003005D1/de active Active
- 2008-01-07 EP EP08761892A patent/EP2121434B1/de not_active Not-in-force
- 2008-01-07 WO PCT/FR2008/050014 patent/WO2008099097A2/fr not_active Ceased
-
2009
- 2009-07-07 IL IL199724A patent/IL199724A/en not_active IP Right Cessation
Also Published As
| Publication number | Publication date |
|---|---|
| EP2121434A2 (de) | 2009-11-25 |
| IL199724A0 (en) | 2010-04-15 |
| FR2911320A1 (fr) | 2008-07-18 |
| US8128032B2 (en) | 2012-03-06 |
| FR2911320B1 (fr) | 2009-04-10 |
| US20090302159A1 (en) | 2009-12-10 |
| CA2676334A1 (fr) | 2008-08-21 |
| WO2008099097A3 (fr) | 2008-10-09 |
| IL199724A (en) | 2014-03-31 |
| DE602008003005D1 (de) | 2010-11-25 |
| EP2121434B1 (de) | 2010-10-13 |
| ZA200904716B (en) | 2010-09-29 |
| WO2008099097A2 (fr) | 2008-08-21 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| UEP | Publication of translation of european patent specification |
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