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:
Feb. 16, 2021

Filed:

Feb. 05, 2018
Applicant:

Airbus Operations Limited, Bristol, GB;

Inventors:

Christopher Papadopoulos, Bristol, GB;

Matthew Marples, Bristol, GB;

Andy Mounty, Bristol, GB;

Costas Fanourakis, Bristol, GB;

Graham King, Bristol, GB;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64D 45/00 (2006.01); B64C 25/22 (2006.01); B64C 25/34 (2006.01); F15B 15/14 (2006.01); F15B 19/00 (2006.01); B64F 5/60 (2017.01); F15B 1/24 (2006.01); B64C 25/58 (2006.01); B64C 13/48 (2006.01); F15B 1/08 (2006.01);
U.S. Cl.
CPC ...
B64D 45/0005 (2013.01); B64C 13/48 (2013.01); B64C 25/22 (2013.01); B64C 25/34 (2013.01); B64C 25/58 (2013.01); B64D 45/00 (2013.01); B64F 5/60 (2017.01); F15B 1/08 (2013.01); F15B 1/24 (2013.01); F15B 15/14 (2013.01); F15B 19/00 (2013.01); F15B 19/005 (2013.01); B64D 2045/0085 (2013.01); F15B 2201/205 (2013.01); F15B 2201/31 (2013.01); F15B 2211/7051 (2013.01); F15B 2211/857 (2013.01);
Abstract

A landing gear system for an aircraft includes a retractable landing gear assembly, a hydraulic actuator for actuating movement part, for example a bogie of the landing gear assembly, and an accumulator associated with the actuator. The accumulator comprises a volume of pressurised gas separated from hydraulic fluid by a separator piston. Travel of the separator piston beyond a certain position is indicative of a fault. The accumulator includes a snubbing device that acts to slow movement of the separator piston beyond that position. A monitoring system measures the time taken for the movement of the landing gear part effected by the hydraulic actuator. If the measured time is longer than a threshold time, that is indicative of a possible fault in the accumulator, that might, without the snubbing, remain undetected and/or hidden from view.


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