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:
Mar. 10, 2015

Filed:

Sep. 14, 2012
Applicants:

Yasuto Onomichi, Hyogo, JP;

Taku Kondo, Hyogo, JP;

Shogo Hagihara, Hyogo, JP;

Ryo Takaki, Hyogo, JP;

Takaaki Onishi, Hyogo, JP;

Inventors:

Yasuto Onomichi, Hyogo, JP;

Taku Kondo, Hyogo, JP;

Shogo Hagihara, Hyogo, JP;

Ryo Takaki, Hyogo, JP;

Takaaki Onishi, Hyogo, JP;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 25/22 (2006.01); F15B 21/04 (2006.01); F15B 7/00 (2006.01); B64C 13/50 (2006.01); F15B 1/26 (2006.01);
U.S. Cl.
CPC ...
B64C 25/22 (2013.01); F15B 7/006 (2013.01); F15B 21/042 (2013.01); B64C 2013/506 (2013.01); F15B 2211/20515 (2013.01); F15B 2211/20538 (2013.01); F15B 2211/20561 (2013.01); F15B 2211/27 (2013.01); F15B 2211/3058 (2013.01); F15B 2211/411 (2013.01); F15B 2211/4159 (2013.01); F15B 2211/8752 (2013.01); F15B 1/26 (2013.01); F15B 2211/6343 (2013.01); F15B 2211/6651 (2013.01);
Abstract

A landing gear retraction/extension device includes a hydraulic actuator, a hydraulic circuit, a hydraulic pump, an electric motor, and a driver. Part of the hydraulic circuit is provided such that heat is exchangeable between operation oil and each of the electric motor and the driver. The driver supplies power to the electric motor before landing of an aircraft such that an operation oil temperature is higher than a predetermined temperature upon the landing of the aircraft.


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