Title:
FLYING VEHICLE
Document Type and Number:
WIPO Patent Application WO/2022/049764
Kind Code:
A1
Abstract:
[Problem] To provide a flying vehicle by which it is possible to simultaneously realize vertical taking-off and landing and improving fuel economy, and realize stable landing. [Solution] This flying vehicle comprises a flight unit to which a plurality of rotary blade parts and a main wing are connected. The main wing is configured such that a lift generated by the main wing during landing is less than the lift generated by the main wing during cruising. Further, the main wing is tilted forward and fixed with respect to the flight unit. Rotary blades are each connected at an angle for generating a thrust and a lift during cruising. Further, the rotary blades are each connected at an angle for generating a thrust during cruising. Further, the flight unit is configured such that the rotary blades do not interfere with the flight unit or the main wing during landing. Further, the main wing is connected to the flight unit through a rotary shaft. The main wing is configured to tilt the angle with respect to the flight unit more forward about the rotary shaft during the landing than during the cruising.
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Inventors:
SUZUKI YOICHI (JP)
Application Number:
PCT/JP2020/033761
Publication Date:
March 10, 2022
Filing Date:
September 07, 2020
Export Citation:
Assignee:
AERONEXT INC (JP)
International Classes:
B64C27/26; B64C3/42; B64C39/02
Foreign References:
| JP2019018623A | 2019-02-07 | |||
| JPH0577789A | 1993-03-30 | |||
| JP2009234551A | 2009-10-15 | |||
| JP2009078745A | 2009-04-16 | |||
| US10131426B2 | 2018-11-20 |
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