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. 30, 2025

Filed:

Nov. 23, 2021
Applicant:

Honda Motor Co., Ltd., Tokyo, JP;

Inventors:

Akinori Kita, Wako, JP;

Kenro Udono, Wako, JP;

Takeshi Matsumoto, Wako, JP;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02C 7/36 (2006.01); B64U 50/11 (2023.01); B64U 50/34 (2023.01); F01D 15/10 (2006.01); F02C 7/268 (2006.01); B64U 10/13 (2023.01); B64U 30/20 (2023.01);
U.S. Cl.
CPC ...
B64U 50/11 (2023.01); B64U 50/34 (2023.01); F01D 15/10 (2013.01); F02C 7/268 (2013.01); F02C 7/36 (2013.01); B64U 10/13 (2023.01); B64U 30/20 (2023.01); F05D 2220/323 (2013.01); F05D 2220/76 (2013.01); F05D 2260/85 (2013.01);
Abstract

Provided is a gas turbine system in which electricity consumption of a battery when starting or stopping a gas turbine engine is reduced and sufficient battery power during flight can be secured. The present invention includes a plurality of gas turbine engines, and, generators, and, a battery, and a controller. The controllerdecides at least one main starting gas turbine enginefrom the plurality of gas turbine engines before the plurality of gas turbine engines are started, starts the main starting gas turbine engineusing electricity from the battery, and starts the secondary starting gas turbine enginesandof the plurality of gas turbine engines other than the main starting gas turbine engineusing electricity from the generatorconnected to the main starting gas turbine engineafter the main starting gas turbine enginereaches a steady state.


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