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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.

Patent No.:

US 9771166 B1

PDFFull Text
Expired
Date of Patent:
Sep. 26, 2017

Filed:

May. 23, 2013

System, kit and method for indicating the pressure in an aircraft landing gear shock absorber

Applicant:

Airbus Operations Limited, Bristol, GB;

Inventors:

Fraser Wilson, Wotton-Under-Edge, GB;

Stephen Briancourt, Bristol, GB;

Scott Wallis, Bristol, GB;

Assignee:

AIRBUS OPERATIONS LIMITED, Bristol, GB;

Attorney:

Hauptman Ham LLP

Primary Examiner:

Tien Dinh

Assistant Examiner:

Vicente Rodriguez

Int. Cl.
CPC ...
B64D 45/00 (2006.01); B64C 25/58 (2006.01); F16F 9/32 (2006.01); G01L 7/16 (2006.01); G01L 9/00 (2006.01); G01M 17/04 (2006.01); G01B 11/14 (2006.01); B64C 25/02 (2006.01); G01L 19/08 (2006.01); B64F 5/60 (2017.01);
U.S. Cl.
CPC ...
B64D 45/00 (2013.01); B64C 25/02 (2013.01); B64C 25/58 (2013.01); B64F 5/60 (2017.01); F16F 9/3292 (2013.01); G01B 11/14 (2013.01); G01L 7/16 (2013.01); G01L 9/0089 (2013.01); G01L 19/08 (2013.01); G01M 17/04 (2013.01);
Abstract

A system for indicating the pressure in an aircraft landing gear shock absorber is provided, the system comprising a source of collimated light and a target, the source of collimated light being attached to the aircraft, and being operable to emit light onto the target; the position of the point of incidence of the light emitted from the source of collimated light on the target being indicative of the pressure in the aircraft landing gear shock absorber. A kit for making such a system and a method of indicating the pressure in an aircraft landing gear are also provided.

Find Patent Forward Citations

Wilson, Fraser. (2017). System, kit and method for indicating the pressure in an aircraft landing gear shock absorber (U.S. Patent No. 9771166). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/9771166

Data source: USPTO (United States Patent and Trademark Office) public patent records. Weekly synchronization. How IDiyas builds this profile

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