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:
Sep. 20, 2022

Filed:

Oct. 21, 2019
Applicant:

Kawasaki Jukogyo Kabushiki Kaisha, Kobe, JP;

Inventors:

Kenichi Nakashima, Kobe, JP;

Satoshi Ootsuki, Akashi, JP;

Shuma Kobayashi, Kobe, JP;

Kippei Matsuda, Kobe, JP;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64D 41/00 (2006.01); B64D 31/06 (2006.01); B64D 31/14 (2006.01); F16H 15/38 (2006.01); F16H 59/72 (2006.01); F16H 61/664 (2006.01); H02P 9/06 (2006.01); B64C 19/00 (2006.01); F04C 14/22 (2006.01); H02P 101/25 (2016.01); H02P 101/30 (2015.01); B60W 50/00 (2006.01);
U.S. Cl.
CPC ...
B64D 41/00 (2013.01); B64C 19/00 (2013.01); B64D 31/06 (2013.01); B64D 31/14 (2013.01); F04C 14/22 (2013.01); F16H 15/38 (2013.01); F16H 59/72 (2013.01); F16H 61/664 (2013.01); H02P 9/06 (2013.01); B60G 2800/90 (2013.01); B60W 2050/0002 (2013.01); H02P 2101/25 (2015.01); H02P 2101/30 (2015.01);
Abstract

A power generation controller of an aircraft includes a low-temperature start-up control section and a power generation control section. When it is determined that an oil temperature of a hydraulic actuator configured to change an operation position of a speed change element of a hydraulic transmission satisfies a predetermined low-temperature condition when starting up an aircraft engine, the low-temperature start-up control section sets a power generator to a power non-generating state and controls the hydraulic actuator such that the speed change element is positioned at an acceleration side of a median in a speed change range. When it is determined that the oil temperature satisfies a predetermined low-temperature start-up completion condition, the power generation control section sets the power generator to a power generating state and controls the hydraulic actuator in accordance with a rotational frequency of the aircraft engine.


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