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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.

Patent No.:

US 12579339 B1

PDFFull Text
Date of Patent:
Mar. 17, 2026

Filed:

Mar. 14, 2022

Aircraft maneuvering system for single propeller aircraft and single propeller aircraft

Applicant:

Subaru Corporation, Tokyo, JP;

Inventors:

Shunichiro Hara, Tokyo, JP;

Takeshi Fukurose, Tokyo, JP;

Koji Ikeda, Tokyo, JP;

Assignee:

SUBARU CORPORATION, Tokyo, JP;

Attorney:

Rimon P.C.

Primary Examiner:

Nithya J Moll

Int. Cl.
CPC ...
G06F 7/48 (2006.01); B64C 9/32 (2006.01); B64C 13/16 (2006.01); B64D 31/04 (2006.01); G06F 30/20 (2020.01); G09B 9/16 (2006.01); G09B 9/44 (2006.01);
U.S. Cl.
CPC ...
G06F 30/20 (2020.01); B64C 9/323 (2013.01); B64C 13/16 (2013.01); B64D 31/04 (2013.01); G09B 9/165 (2013.01); G09B 9/44 (2013.01);
Abstract

A jet aircraft maneuvering characteristic simulation system for a single propeller aircraft includes a power lever, speed brakes, and a controller. The power lever is configured to change a thrust of the single propeller aircraft. The speed brakes are provided on respective right and left sides of the single propeller aircraft. The controller is configured to, in response to an operation of the power lever to raise the thrust of the single propeller aircraft, deploy both the right and the left speed brakes to cause an increase in speed of the single propeller aircraft to be moderate, and control the speed brakes to cause a force in a yaw direction and a force in a roll direction to be generated that act against a turning tendency of the single propeller aircraft by making amounts of the deployment of the right and the left speed brakes different from each other.

Find Patent Forward Citations

Hara, Shunichiro. (2026). Aircraft maneuvering system for single propeller aircraft and single propeller aircraft (U.S. Patent No. 12579339). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/12579339

Data source: USPTO (United States Patent and Trademark Office) public patent records. Weekly synchronization. How IDiyas builds this profile

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