Title:
ELECTRIC VERTICAL TAKE-OFF AND LANDING AIRCRAFT
Document Type and Number:
WIPO Patent Application WO/2021/039653
Kind Code:
A1
Abstract:
These electric vertical take-off and landing aircrafts (100, 100a-100d) are each provided with: a plurality of electric drive systems (10) each having a plurality of rotary wings (30) and a motor (111) for rotationally driving the rotary wings; a fuselage (20) on which the plurality of rotary wings and the electric drive systems are disposed; and connection parts (29, CP1-CP4, CPb, CPc, CPd1, CPd2) which are provided on at least one among the upper side and the lower side of the fuselage, and which are for connection with another aircraft that is a different electric vertical take-off and landing aircraft.
Inventors:
IWAKAWA AKIRA (JP)
HASHIMOTO MARIKO (JP)
SUGITA SYUN (JP)
TAKEMURA YUUICHI (JP)
HASHIMOTO MARIKO (JP)
SUGITA SYUN (JP)
TAKEMURA YUUICHI (JP)
Application Number:
PCT/JP2020/031691
Publication Date:
March 04, 2021
Filing Date:
August 21, 2020
Export Citation:
Assignee:
DENSO CORP (JP)
International Classes:
B64C27/22; B64D5/00
Foreign References:
| JPH06144390A | 1994-05-24 | |||
| US20190160315A1 | 2019-05-30 | |||
| CN106741958A | 2017-05-31 | |||
| US20170291704A1 | 2017-10-12 |
Attorney, Agent or Firm:
TOKKYO GYOMUHOJIN MEISEI INTERNATIONAL PATENT FIRM (JP)
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