AIRCRAFT AND ROTOR BLADE MODULE

WIPO Patent Application WO/2022/180754

A1

An aircraft 1 that takes off and lands vertically. The aircraft 1 comprises a fuselage 10, at least one pair of fixed wings 20–1–20–4 that extend from the fuselage 10 in the left/right direction, a plurality of first rotor blades 402–1, 402–2, a plurality of first rotating drive units, a plurality of first storage cells 405–1, 405–2, and a plurality of first cables 406–1, 406–2. The plurality of first rotor blades 402–1, 402–2 are supported by at least one pair of fixed wings 20–1–20–4 and, by being rotated and driven, generate thrust that thrusts the aircraft 1 up vertically. The plurality of first rotating drive units use power and rotate and drive each of the plurality of first rotor blades 402–1, 402–2. The plurality of first storage cells 405–1, 405–2 are fixed to at least one pair of fixed wings 20–1–20–4 and charge and discharge power. The plurality of first cables 406-1, 406-2 transmit power from the plurality of first storage cells 405-1, 405-2 to the plurality of first rotating drive units.

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KUWAMURA KOYA (JP)
NAKAI TASUKU (JP)

PCT/JP2021/007225

September 01, 2022

February 25, 2021

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TETRA AVIATION CORP (JP)

B64C27/26; B64C29/00; B64C29/02; B64D27/24

CN209382254U	2019-09-13
US20180215465A1	2018-08-02
JP2017532256A	2017-11-02
US9085354B1	2015-07-21
US20180312251A1	2018-11-01
JP2014231253A	2014-12-11

WAKAYAMA Go (JP)

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