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. 14, 2023

Filed:

May. 06, 2020
Applicant:

Safran Landing Systems Canada Inc., Ajax, CA;

Inventor:

Robert Kyle Schmidt, Brooklin, CA;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 25/40 (2006.01); B64C 25/44 (2006.01); F16D 67/02 (2006.01); F16H 25/22 (2006.01); F16D 65/18 (2006.01); F16D 121/24 (2012.01); F16D 125/40 (2012.01); F16D 55/36 (2006.01); F16H 25/20 (2006.01);
U.S. Cl.
CPC ...
B64C 25/405 (2013.01); B64C 25/44 (2013.01); F16D 65/186 (2013.01); F16D 67/02 (2013.01); F16H 25/2204 (2013.01); F16D 55/36 (2013.01); F16D 2121/24 (2013.01); F16D 2125/40 (2013.01); F16H 2025/2075 (2013.01);
Abstract

A landing gear system includes a wheel rotatably coupled to the axle about an axis. A motor is fixedly positioned relative to the axle with a clutch assembly operably coupled to an output shaft of the motor. The landing gear includes an actuator and a drive assembly. The actuator applies a braking force to the wheel. The drive assembly includes a pinion gear and a drive gear rotatably associated with the pinion gear. The drive gear is configured to transfer a rotational force to the wheel in order to provide autonomous taxiing capability. Both the brake assembly and the drive assembly are operably coupled to the clutch assembly so that the output shaft of the motor drives both the brake assembly and the drive assembly.


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