ZA201301527B - Flying vehicle retractable wing hinge and truss - Google Patents
Flying vehicle retractable wing hinge and trussInfo
- Publication number
- ZA201301527B ZA201301527B ZA2013/01527A ZA201301527A ZA201301527B ZA 201301527 B ZA201301527 B ZA 201301527B ZA 2013/01527 A ZA2013/01527 A ZA 2013/01527A ZA 201301527 A ZA201301527 A ZA 201301527A ZA 201301527 B ZA201301527 B ZA 201301527B
- Authority
- ZA
- South Africa
- Prior art keywords
- truss
- flying vehicle
- wing hinge
- retractable wing
- vehicle retractable
- Prior art date
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C37/00—Convertible aircraft
-
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C5/00—Stabilising surfaces
- B64C5/10—Stabilising surfaces adjustable
- B64C5/12—Stabilising surfaces adjustable for retraction against or within fuselage or nacelle
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Bridges Or Land Bridges (AREA)
- Body Structure For Vehicles (AREA)
- Vehicle Step Arrangements And Article Storage (AREA)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US40089610P | 2010-08-03 | 2010-08-03 | |
| PCT/US2011/001355 WO2012018382A2 (en) | 2010-08-03 | 2011-08-02 | Flying vehicle retractable wing hinge and truss |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| ZA201301527B true ZA201301527B (en) | 2013-11-27 |
Family
ID=45555410
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| ZA2013/01527A ZA201301527B (en) | 2010-08-03 | 2013-02-27 | Flying vehicle retractable wing hinge and truss |
Country Status (5)
| Country | Link |
|---|---|
| US (2) | US10293935B2 (enExample) |
| JP (1) | JP5960139B2 (enExample) |
| BR (1) | BR112013002735B1 (enExample) |
| WO (1) | WO2012018382A2 (enExample) |
| ZA (1) | ZA201301527B (enExample) |
Families Citing this family (28)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB201018185D0 (en) * | 2010-10-28 | 2010-12-08 | Airbus Operations Ltd | Wing tip device attachment apparatus and method |
| US9296469B2 (en) * | 2011-10-01 | 2016-03-29 | The Boeing Company | Horizontal folding wingtip |
| US9211946B2 (en) | 2011-10-01 | 2015-12-15 | The Boeing Company | Wing fold system with latch pins through multiple mating lugs |
| US9499252B2 (en) | 2011-10-01 | 2016-11-22 | The Boeing Company | Wing fold controller |
| US9290260B2 (en) | 2011-10-01 | 2016-03-22 | The Boeing Company | Wing fold controller |
| US9469392B2 (en) | 2012-10-30 | 2016-10-18 | The Boeing Company | Wing fold system rotating latch |
| US9415857B2 (en) | 2012-10-30 | 2016-08-16 | The Boeing Company | Wing fold system |
| US9296471B2 (en) * | 2013-10-06 | 2016-03-29 | The Boeing Company | Swing wing tip system, assembly and method with dual load path structure |
| CN103692873B (zh) * | 2013-12-20 | 2015-11-18 | 胡新如 | 一种水陆飞行汽车 |
| AU2015200677B2 (en) * | 2014-04-25 | 2019-01-17 | The Boeing Company | System for latching and locking a foldable airfoil |
| GB2530578A (en) | 2014-09-29 | 2016-03-30 | Airbus Operations Ltd | Interface for control of a foldable wing on an aircraft |
| CN107107690B (zh) * | 2014-10-08 | 2019-10-08 | 航空移动有限公司 | 用于飞行式运载工具的中央翼板及其控制方法 |
| US11027584B1 (en) * | 2015-07-22 | 2021-06-08 | Taras Kiceniuk, Jr. | Flying car with fore and aft lifting surfaces |
| US12122203B1 (en) * | 2014-10-17 | 2024-10-22 | Taras Kuciniek, Jr. | Flying car with multiple wheels |
| CN105857573B (zh) * | 2016-04-23 | 2017-12-26 | 广州市绿化公司 | 一种市政园林绿化用智能无人机 |
| SK500352017A3 (sk) * | 2017-05-11 | 2018-12-03 | Štefan Klein | Spôsob transformácie motorového dopravného prostriedku na transport na zemskom povrchu a vo vzduchu a motorový dopravný prostriedok |
| CN110891859B (zh) * | 2017-07-27 | 2023-03-10 | 株式会社辰巳菱机 | 悬浮型移动装置 |
| GB2573120A (en) * | 2018-04-24 | 2019-10-30 | Airbus Operations Ltd | Improved secondary locking mechanism |
| US11370526B2 (en) * | 2018-05-31 | 2022-06-28 | Airbus Operations Gmbh | Latching device for a wing arrangement for an aircraft |
| US11319054B2 (en) * | 2018-05-31 | 2022-05-03 | Airbus Operations Gmbh | Wing arrangement for an aircraft |
| US11214353B2 (en) * | 2018-06-01 | 2022-01-04 | Airbus Operations Gmbh | Wing arrangement for an aircraft and aircraft |
| EP3587252A1 (en) * | 2018-06-28 | 2020-01-01 | Airbus Operations GmbH | Arresting system for arresting a first aircraft component relative to a second aircraft component |
| US11046416B2 (en) * | 2018-08-03 | 2021-06-29 | Aurora Flight Sciences Corporation | Combination flight and ground apparatus for a vehicle |
| US11524780B2 (en) | 2021-01-07 | 2022-12-13 | Faruk Hossain | Fan powered folding wing bicycle apparatus |
| US20240239485A1 (en) * | 2021-09-17 | 2024-07-18 | Jetzero, Inc. | Blended wing body aircraft with a fuel cell and method of use |
| US12377995B2 (en) * | 2022-11-22 | 2025-08-05 | Embraer S.A. | Aircraft tail mounted fuel cell power train and thermal management systems |
| US20250269956A1 (en) * | 2024-02-27 | 2025-08-28 | Brett Cryer | Compact Aircraft and Novel Methods of Manufacture Thereof |
| US20250375991A1 (en) * | 2025-08-22 | 2025-12-11 | Guanhao Wu | Dual-Mode Vehicle with Selectively Attachable Flight Module and Energy Transmission Control |
Family Cites Families (23)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US1998148A (en) * | 1934-04-18 | 1935-04-16 | Vieriu Daniel | Auto-aeroplane |
| US2573271A (en) * | 1947-06-30 | 1951-10-30 | Adolph R Perl | Roadable aircraft |
| US3285540A (en) * | 1964-06-15 | 1966-11-15 | Lee Shao-Tang | Shiftable variable area wing construction |
| GB1135946A (en) * | 1965-04-01 | 1968-12-11 | British Aircraft Corp Ltd | Improvements in aircraft |
| US3489375A (en) * | 1967-11-21 | 1970-01-13 | Richard R Tracy | Variable lifting surface craft |
| FR1601027A (enExample) * | 1968-12-30 | 1970-08-03 | ||
| US3606978A (en) * | 1969-10-16 | 1971-09-21 | Boeing Co | Wing sweep pivot-bearing arrangement |
| IL39260A (en) * | 1972-04-21 | 1975-06-25 | Bouchnik J | Detachable cabin aircraft |
| US4212441A (en) * | 1978-05-11 | 1980-07-15 | The United States Of America As Represented By The Secretary Of The Air Force | Wing pivot assembly for variable sweep wing aircraft |
| US4703905A (en) * | 1985-09-05 | 1987-11-03 | Grumman Aerospace Corporation | Manned entry vehicle system |
| JPS6449899A (en) * | 1987-08-20 | 1989-02-27 | Mitsubishi Electric Corp | Guided missile |
| US4915664A (en) * | 1988-12-22 | 1990-04-10 | Erik Bakker | Toy glider with wing converging mechanism |
| US5050817A (en) * | 1989-10-16 | 1991-09-24 | Miller Harvey R | Combined road and aircraft vehicle |
| US5192037A (en) * | 1991-08-23 | 1993-03-09 | Mcdonnell Douglas Corporation | Double-pivoting deployment system for aerosurfaces |
| US5899410A (en) * | 1996-12-13 | 1999-05-04 | Mcdonnell Douglas Corporation | Aerodynamic body having coplanar joined wings |
| US5984231A (en) * | 1998-06-19 | 1999-11-16 | Northrop Grumman Corporation | Aircraft with variable forward-sweep wing |
| DE19827277B4 (de) * | 1998-06-19 | 2006-08-10 | Diehl Stiftung & Co.Kg | Lageranordnung für die aufschwenkbaren Ruderblätter eines lenkbaren Flugkörpers |
| US6073882A (en) * | 1998-09-21 | 2000-06-13 | Zieger; N. Henning | Flying vehicle with retractable wing assembly |
| US6089503A (en) * | 1999-01-15 | 2000-07-18 | Northrop Grumman Corp | Selectively rotatable and torsionally flexible aerodynamic control apparatus |
| FR2836889B1 (fr) * | 2002-03-11 | 2004-05-28 | Eurocopter France | Procede et dispositif de repliage-depliage des pales d'un rotor de giravion |
| JP4171913B2 (ja) * | 2004-04-13 | 2008-10-29 | 独立行政法人 宇宙航空研究開発機構 | 低ブーム特性と低抵抗特性を両立する可変前進翼超音速航空機 |
| US7559505B2 (en) * | 2005-12-01 | 2009-07-14 | Lockheed Martin Corporation | Apparatus and method for restraining and deploying an airfoil |
| US7946527B2 (en) * | 2007-09-10 | 2011-05-24 | Alan Glen Holmes | Aircraft with fixed, swinging and folding wings |
-
2011
- 2011-08-02 BR BR112013002735-5A patent/BR112013002735B1/pt active IP Right Grant
- 2011-08-02 US US13/136,481 patent/US10293935B2/en active Active
- 2011-08-02 WO PCT/US2011/001355 patent/WO2012018382A2/en not_active Ceased
- 2011-08-02 JP JP2013523150A patent/JP5960139B2/ja active Active
-
2013
- 2013-02-27 ZA ZA2013/01527A patent/ZA201301527B/en unknown
-
2019
- 2019-05-17 US US16/415,623 patent/US11142312B2/en active Active
Also Published As
| Publication number | Publication date |
|---|---|
| US20190300170A1 (en) | 2019-10-03 |
| JP5960139B2 (ja) | 2016-08-02 |
| JP2014503400A (ja) | 2014-02-13 |
| WO2012018382A3 (en) | 2012-06-14 |
| BR112013002735A2 (pt) | 2017-06-27 |
| US11142312B2 (en) | 2021-10-12 |
| WO2012018382A2 (en) | 2012-02-09 |
| US20120032023A1 (en) | 2012-02-09 |
| US10293935B2 (en) | 2019-05-21 |
| BR112013002735B1 (pt) | 2021-02-02 |
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