Title:
航空機
Document Type and Number:
Japanese Patent JP7442907
Kind Code:
B2
Abstract:
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.
Inventors:
Koya Kuwamura
Yu Nakai
Yu Nakai
Application Number:
JP2023502078A
Publication Date:
March 05, 2024
Filing Date:
November 28, 2021
Export Citation:
Assignee:
Tetra Aviation Co., Ltd.
International Classes:
B64C27/26; B64C29/00; B64U10/13
Domestic Patent References:
| JP2018070155A | ||||
| JP201036874A |
Foreign References:
| US20180215465 | ||||
| US20200115045 | ||||
| CN109305357A | ||||
| CN206511121U | ||||
| CN205819564U | ||||
| US10377488 | ||||
| CN109476373A |
Attorney, Agent or Firm:
Go Wakayama