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:
Aug. 20, 2019

Filed:

Mar. 13, 2015
Applicant:

Airbus Operations Limited, Bristol, GB;

Inventor:

Arnaud Didey, Bristol, GB;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 25/40 (2006.01); B64C 25/34 (2006.01); B64C 25/42 (2006.01);
U.S. Cl.
CPC ...
B64C 25/405 (2013.01); B64C 25/34 (2013.01); B64C 25/42 (2013.01); Y02T 50/823 (2013.01);
Abstract

A drive system for an aircraft landing gear is disclosed having a wheel rotatable about a wheel axis, a driven gear arranged to be attached to the wheel and capable of rotating the wheel about the wheel axis, a drive train comprising an input gear rotatable by an input shaft, an intermediate gear meshed with the input gear and rotatable by an intermediate shaft, and a support member arranged to support the input shaft and intermediate shaft. The support member is arranged to pivot about the input shaft between a neutral configuration in which the drive train is disengaged from the driven gear and a driven configuration in which the drive train is engaged with the driven gear to enable the drive train to rotate the driven gear. The drive system includes brake capable of being engaged with the input shaft to prevent rotation of the input shaft relative to the support member and of being disengaged from the input shaft to permit rotation of the input shaft relative to the support member.


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