JP2015164843A5 - - Google Patents
Download PDFInfo
- Publication number
- JP2015164843A5 JP2015164843A5 JP2015038406A JP2015038406A JP2015164843A5 JP 2015164843 A5 JP2015164843 A5 JP 2015164843A5 JP 2015038406 A JP2015038406 A JP 2015038406A JP 2015038406 A JP2015038406 A JP 2015038406A JP 2015164843 A5 JP2015164843 A5 JP 2015164843A5
- Authority
- JP
- Japan
- Prior art keywords
- wing
- shape
- configuration
- deployed
- housing shape
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
- 238000000034 method Methods 0.000 claims description 7
- 239000002131 composite material Substances 0.000 claims description 6
- 239000000956 alloy Substances 0.000 claims description 2
- 238000010438 heat treatment Methods 0.000 claims description 2
- 239000000463 material Substances 0.000 claims description 2
- 229910001092 metal group alloy Inorganic materials 0.000 claims description 2
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000003825 pressing Methods 0.000 description 1
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US14/194,795 | 2014-03-02 | ||
| US14/194,795 US9216814B2 (en) | 2014-03-02 | 2014-03-02 | Stackable wing for an aerocar |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| JP2015164843A JP2015164843A (ja) | 2015-09-17 |
| JP2015164843A5 true JP2015164843A5 (enExample) | 2018-03-22 |
| JP6577207B2 JP6577207B2 (ja) | 2019-09-18 |
Family
ID=54006403
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2015038406A Expired - Fee Related JP6577207B2 (ja) | 2014-03-02 | 2015-02-27 | エアロカーの変形可能な翼及び翼を変形させる方法 |
Country Status (2)
| Country | Link |
|---|---|
| US (2) | US9216814B2 (enExample) |
| JP (1) | JP6577207B2 (enExample) |
Families Citing this family (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP6626366B2 (ja) | 2016-02-26 | 2019-12-25 | 三菱重工業株式会社 | 飛行車両運航システム、管制システム及び飛行車両運航方法 |
| CN110678388B (zh) * | 2017-05-22 | 2023-05-23 | 保罗·奈泽 | 用于与流体相互作用的装置和方法 |
| WO2019148464A1 (zh) * | 2018-02-02 | 2019-08-08 | 浙江吉利控股集团有限公司 | 飞行汽车机翼、承载模块结构、动力系统、飞行汽车、飞行汽车机翼的控制方法 |
| CN108394241B (zh) * | 2018-02-08 | 2019-08-27 | 唐晓明 | 一种直升固定翼滑翔多模式飞车 |
| EP4610166A1 (en) * | 2024-02-29 | 2025-09-03 | Airbus Operations GmbH | An airfoil and adaptable wing with a bionic airfoil surface |
Family Cites Families (23)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US1412455A (en) * | 1922-04-11 | Aeroplane-wingr | ||
| US996456A (en) * | 1909-10-27 | 1911-06-27 | Julius Christiansen | Aeroplane. |
| US4537373A (en) * | 1979-08-16 | 1985-08-27 | Butts Dennis D | Air vehicle having driven wheels and ducted fans |
| JPS5943359B2 (ja) * | 1981-04-07 | 1984-10-22 | 三井造船株式会社 | 帆装置 |
| JPS6377899U (enExample) * | 1986-11-11 | 1988-05-23 | ||
| JPH0228098A (ja) * | 1988-07-18 | 1990-01-30 | Mitsubishi Heavy Ind Ltd | 形状可変翼 |
| GB9116787D0 (en) * | 1991-08-01 | 1991-09-18 | Secr Defence | Article having an aerofoil section with a distensible expansion surface |
| JPH08244689A (ja) * | 1995-03-08 | 1996-09-24 | Mitsubishi Heavy Ind Ltd | ヘリコプタの翼厚可変ロータ |
| WO1998003398A1 (de) | 1996-07-18 | 1998-01-29 | Prospective Concepts Ag | Adaptiver pneumatischer flügel für starrflügel-fluggeräte |
| US6015115A (en) * | 1998-03-25 | 2000-01-18 | Lockheed Martin Corporation | Inflatable structures to control aircraft |
| DE19927359A1 (de) * | 1999-06-16 | 2000-12-21 | Creavis Tech & Innovation Gmbh | Elektrophoretische Displays aus lichtstreuenden Trägermaterialien |
| DE10055961B4 (de) * | 2000-11-11 | 2004-09-09 | Eads Deutschland Gmbh | Variabler Flügelbereich mit einstellbarer, sich in Spannweiten-Richtung erstreckender Profilform |
| US6786450B1 (en) * | 2001-03-09 | 2004-09-07 | Harry Einstein | Rapidly-convertible roadable aircraft |
| EP1620953B1 (en) * | 2003-04-17 | 2009-04-15 | Nokia Corporation | Bi-stable hinge and mobile station using the same |
| DE102004056537B4 (de) * | 2004-11-23 | 2010-09-09 | Eads Deutschland Gmbh | Anordnung zur Minderung des aerodynamischen Lärms an einem Zusatzflügel eines Flugzeuges |
| DE102004062998B4 (de) * | 2004-12-22 | 2010-09-09 | Airbus Deutschland Gmbh | Flügel, insbesondere Tragflügel eines Flugzeugs, mit veränderlicher Profilform |
| US7874512B2 (en) * | 2006-07-12 | 2011-01-25 | Junfeng Xu | System and method for a flyable and roadable vehicle |
| GB0624580D0 (en) | 2006-12-08 | 2007-01-17 | Imp Innovations Ltd | Aerofoil member |
| US8262032B2 (en) | 2008-11-13 | 2012-09-11 | Raytheon Company | Collapsible wing beams and method |
| US20110300358A1 (en) * | 2010-06-04 | 2011-12-08 | The Boeing Company | Shape memory alloy/fiber reinforced polymeric composite structures and method for forming |
| US8376263B2 (en) * | 2010-08-27 | 2013-02-19 | Rolls-Royce Corporation | Roadable aircraft |
| JP5871508B2 (ja) * | 2011-08-02 | 2016-03-01 | 隆徳 土屋 | 平行回転翼を利用した流体機械 |
| US8500406B2 (en) * | 2011-12-22 | 2013-08-06 | General Electric Company | Wind turbine rotor blades with shape memory polymer composites and methods for deploying the same |
-
2014
- 2014-03-02 US US14/194,795 patent/US9216814B2/en active Active
-
2015
- 2015-02-27 JP JP2015038406A patent/JP6577207B2/ja not_active Expired - Fee Related
- 2015-10-01 US US14/872,415 patent/US9580167B2/en active Active
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| JP2015164843A5 (enExample) | ||
| USD907547S1 (en) | Rear spoiler for a vehicle | |
| JP2019142507A5 (enExample) | ||
| Kaul et al. | Drag optimization study of variable camber continuous trailing edge flap (VCCTEF) using OVERFLOW | |
| US10933976B2 (en) | Leading edge high-lift device | |
| CN104704233B (zh) | 燕尾型翼 | |
| WO2011069887A3 (de) | Hochauftriebssystem für ein flugzeug, verfahren zum bewegen einer auftriebsklappe und flugzeug mit einem hochauftriebssystem | |
| CN107074350A (zh) | 一种用于飞行器的机翼以及包括这种机翼的飞行器 | |
| WO2011010155A3 (en) | Steering vehicles through control of aerofoils | |
| EP2808541A3 (en) | Wind turbine blade having a tensile-only stiffener for passive control of flap movement | |
| US20060226283A1 (en) | Hybrid transonic-subsonic aerofoils | |
| RU2009105144A (ru) | Ребро атаки детали газотурбинного двигателя, выполненное из сверхупругого материала | |
| CN105564632A (zh) | 一种高升力自然层流翼型 | |
| CN101885381A (zh) | 带凹坑的机翼 | |
| FR2971540B1 (fr) | Ensemble pale-plateforme pour ecoulement supersonique | |
| CN106542081A (zh) | Nasa ms(1)-0313翼型的一种单缝富勒式襟翼设计 | |
| EP2765065A3 (en) | Rear axle beam cover | |
| WO2014199371A8 (en) | Aerofoil and wings for air vehicles | |
| CN204937477U (zh) | 一种低阻、低俯仰力矩的翼型 | |
| JP6577207B2 (ja) | エアロカーの変形可能な翼及び翼を変形させる方法 | |
| WO2018080699A8 (en) | Propeller assembly | |
| JP7038404B2 (ja) | 遷音速翼型、翼及び航空機 | |
| CN204937472U (zh) | 一种针对于低速飞机的翼型 | |
| ZHANG et al. | Trajectory planning of welded repair for aero-engine blades based on NURBS curve | |
| CN205256472U (zh) | 一种提高赛车操纵稳定性的空气动力学套件 |