JPWO2020225815A5 - - Google Patents

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Publication number
JPWO2020225815A5
JPWO2020225815A5 JP2021566065A JP2021566065A JPWO2020225815A5 JP WO2020225815 A5 JPWO2020225815 A5 JP WO2020225815A5 JP 2021566065 A JP2021566065 A JP 2021566065A JP 2021566065 A JP2021566065 A JP 2021566065A JP WO2020225815 A5 JPWO2020225815 A5 JP WO2020225815A5
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JP
Japan
Prior art keywords
vehicle
vehicle according
wing
fan
axis
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.)
Pending
Application number
JP2021566065A
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English (en)
Japanese (ja)
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JP2022532546A (ja
Publication date
Application filed filed Critical
Priority claimed from PCT/IL2020/050498 external-priority patent/WO2020225815A1/en
Publication of JP2022532546A publication Critical patent/JP2022532546A/ja
Publication of JPWO2020225815A5 publication Critical patent/JPWO2020225815A5/ja
Pending legal-status Critical Current

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JP2021566065A 2019-05-07 2020-05-06 走行及び飛行可能な電気またはハイブリッド型のｖｔｏｌ車両 Pending JP2022532546A (ja)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US201962844188P 2019-05-07 2019-05-07
US62/844,188 2019-05-07
PCT/IL2020/050498 WO2020225815A1 (en) 2019-05-07 2020-05-06 Drive and fly electric and hybrid vtol vehicle

Publications (2)

Publication Number Publication Date
JP2022532546A JP2022532546A (ja) 2022-07-15
JPWO2020225815A5 true JPWO2020225815A5 (es) 2023-03-10

Family

ID=73051638

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2021566065A Pending JP2022532546A (ja) 2019-05-07 2020-05-06 走行及び飛行可能な電気またはハイブリッド型のｖｔｏｌ車両

Country Status (5)

Country Link
US (1) US20220315216A1 (es)
EP (1) EP3966047A4 (es)
JP (1) JP2022532546A (es)
CN (1) CN113840742A (es)
WO (1) WO2020225815A1 (es)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3838752B1 (en) * 2019-12-17 2022-04-27 LEONARDO S.p.A. Convertiplane and associated folding method
DE102020007834A1 (de) 2020-12-21 2022-06-23 BAAZ GmbH Fluggerät und zugehöriges Betriebsverfahren
WO2022187426A2 (en) * 2021-03-04 2022-09-09 Nft Inc. Drive and fly vertical take-off and landing vehicle
CN113799561B (zh) * 2021-09-30 2023-03-17 中北大学 一种收展翼与悬挂复用的eVTOL飞车
US20230234414A1 (en) * 2022-01-27 2023-07-27 Frances Jones Transforming vehicle
WO2023177774A1 (en) * 2022-03-17 2023-09-21 Nft Inc. Hybrid road-air vehicle
CN117262204A (zh) * 2023-08-09 2023-12-22 南京航空航天大学 一种适用于跨介质飞行器的变直径桨叶

Family Cites Families (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6808146B2 (en) * 2002-05-31 2004-10-26 Richard L. Swan Merchandise display
US8162253B2 (en) * 2009-08-19 2012-04-24 Seiford Sr Donald S Convertible vehicle for road, air, and water usage
WO2011146349A2 (en) 2010-05-17 2011-11-24 Piasecki Aircraft Corp. Modular and morphable air vehicle
US8376263B2 (en) * 2010-08-27 2013-02-19 Rolls-Royce Corporation Roadable aircraft
CN103496305A (zh) * 2012-04-24 2014-01-08 赵辉 一种飞行汽车
BG111231A (en) 2012-06-07 2013-12-31 КРЪСТЕВ ИванKrustev Ivan ROAD-AIR VEHICLE
US9156550B2 (en) 2014-02-14 2015-10-13 Toyota Motor Engineering & Manufacturing North America, Inc. Dual channel wing for an aerocar
WO2016018486A2 (en) * 2014-05-07 2016-02-04 XTI Aircraft Company Vtol aircraft
US11027584B1 (en) * 2015-07-22 2021-06-08 Taras Kiceniuk, Jr. Flying car with fore and aft lifting surfaces
CN106564349A (zh) * 2016-10-31 2017-04-19 广东工业大学 一种三栖无人机
US10676187B2 (en) * 2017-03-07 2020-06-09 The Boeing Company Robust amphibious aircraft
US10252798B2 (en) * 2017-04-27 2019-04-09 Pterodynamics Vertical takeoff and landing airframe
CN107757273B (zh) * 2017-09-27 2020-03-10 北京航空航天大学 一种飞行汽车
CN107984992A (zh) * 2017-11-28 2018-05-04 北京航空航天大学 一种可垂直起降的陆空两用运载器
CN108791874A (zh) * 2018-06-21 2018-11-13 南京航空航天大学 一种倾转涵道动力无人飞行器
US20200079492A1 (en) * 2018-09-11 2020-03-12 Swift Engineering, Inc. Systems and methods for aerodynamic deployment of wing structures

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