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. 14, 2023

Filed:

Feb. 05, 2019
Applicant:

Goodrich Corporation, Charlotte, NC (US);

Inventors:

Amir Fazeli, Mississauga, CA;

Adnan Cepic, Mississauga, CA;

Susanne M. Reber, Strongsville, OH (US);

Assignee:

Goodrich Corporation, Charlotte, NC (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
G01M 17/04 (2006.01); B64F 5/60 (2017.01); B64C 25/60 (2006.01); F16F 9/32 (2006.01);
U.S. Cl.
CPC ...
G01M 17/04 (2013.01); B64C 25/60 (2013.01); B64F 5/60 (2017.01); F16F 9/3292 (2013.01); F16F 2228/002 (2013.01); F16F 2228/004 (2013.01);
Abstract

A method for monitoring a shock strut may comprise measuring a first shock strut pressure, measuring an ambient temperature, measuring a shock strut stroke, measuring a second shock strut pressure, and determining a servicing condition of the shock strut based upon the first shock strut pressure, the ambient temperature, the shock strut stroke, and the second shock strut pressure, wherein the servicing condition indicates whether it is desirable for the shock strut to be serviced with at least one of a liquid and a gas. The first shock strut pressure and the shock strut stroke may be measured before the takeoff event with a weight of an aircraft supported by the shock strut.


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