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:
May. 16, 2023

Filed:

Apr. 05, 2019
Applicant:

Fujitsu Limited, Kawasaki, JP;

Inventor:

Yoshiro Hada, Atsugi, JP;

Assignee:

FUJITSU LIMITED, Kawasaki, JP;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 25/36 (2006.01); B64U 60/00 (2023.01); B64C 39/02 (2023.01); B64D 35/02 (2006.01); B64D 47/08 (2006.01); B64U 30/20 (2023.01); B64U 50/19 (2023.01); B64U 101/00 (2023.01); B64U 101/30 (2023.01); B64U 101/60 (2023.01);
U.S. Cl.
CPC ...
B64C 39/024 (2013.01); B64C 25/36 (2013.01); B64D 35/02 (2013.01); B64D 47/08 (2013.01); B64U 30/20 (2023.01); B64U 50/19 (2023.01); B64U 2101/00 (2023.01); B64U 2101/30 (2023.01); B64U 2101/60 (2023.01); B64U 2201/20 (2023.01);
Abstract

An aircraft includes: an aircraft body including rotating wings and motors that rotates the rotating wings; wheels arranged on both sides of the aircraft body and rotatably supported around an axis that extends in a left and right direction of the aircraft body; rollers that protrude forward and upward with respect to each of the wheels when the aircraft body is in a horizontal state, and are rotatably supported around an axis that extends in a tangential direction of each of the wheels; and a controller that controls a rotation speed of the motors such that, when the aircraft body is moved in the left and right direction along a vertical wall surface, the aircraft body is inclined forward to bring the rollers into contact with the vertical wall surface, and the aircraft body is inclined to a side where the aircraft body moves in the left and right direction.


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