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:
Jan. 07, 2020

Filed:

Apr. 30, 2019
Applicant:

Hideo Suzuki, Chibashi, Chiba, JP;

Inventors:

Hideo Suzuki, Chibashi, JP;

Sachihiro Suzuki, Takigun, JP;

Kotaro Matsushita, Tokyo, JP;

Masaki Hanada, Tokyo, JP;

Toru Shinohara, Chibashi, JP;

Noriko Niijima, Tokyo, JP;

Tadao Nakamura, Sendai, JP;

Assignee:

Other;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 9/06 (2006.01); B64D 27/02 (2006.01); B64C 19/02 (2006.01); B64C 17/00 (2006.01); B64C 29/00 (2006.01);
U.S. Cl.
CPC ...
B64C 9/06 (2013.01); B64C 17/00 (2013.01); B64C 19/02 (2013.01); B64C 29/0016 (2013.01); B64D 27/02 (2013.01); B64C 2201/14 (2013.01);
Abstract

An aircraft encompasses a main-body, a frame-structure to support the main-body, main and auxiliary rotors provided to the frame-structure and a controller for controlling rotations of the main and auxiliary rotors. In a first mode, the controller delivers a same control signal for rotating the set of the main and auxiliary rotors, and when one of the main and auxiliary rotors becomes abnormal, the controller delivers the same control signal for compensating a decrease of the lift. In a second mode, the controller delivers a control signal only to the normal rotor for increasing the rotation of the normal rotor. Sets of the main and auxiliary rotors in divided regions adjacent to a subject divided region are rotated in a direction counter to the subject divided region. By the first and second modes, the lifts are equalized for balancing the aircraft.


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