The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Dec. 16, 2025

Filed:

May. 15, 2024
Applicant:

Subaru Corporation, Tokyo, JP;

Inventors:

Kazuhisa Takaki, Tokyo, JP;

Hokuto Yamane, Tokyo, JP;

Assignee:

SUBARU CORPORATION, Tokyo, JP;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64U 10/16 (2023.01); B64D 31/00 (2024.01); B64U 30/297 (2023.01);
U.S. Cl.
CPC ...
B64U 10/16 (2023.01); B64D 31/00 (2013.01); B64U 30/297 (2023.01); B64U 2201/20 (2023.01);
Abstract

An aircraft includes: a main body; arms extending substantially horizontally from the main body; rotors that are located at distal ends of the arms and generate lift by rotating; first motors that are coupled to the rotors and rotate the rotors; motor mounts supporting the first motors; and second motors that rotate the motor mounts relative to the arms. The motor mounts each includes a mount proximal end, a mount distal end, and a bent part. The first motors are each fixed to the mount distal end. The mount proximal end is disposed so as to extend substantially vertically upward from the arm. The motor mounts are each coupled to the distal end. The second motors each rotates the mount proximal end with respect to the arm to switch an orientation of a plane of rotation of the rotor between a radially inclined orientation and a circumferentially inclined orientation.


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