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.:
Date of Patent:
Aug. 20, 2019
Filed:
Mar. 06, 2017
Applicant:
Goodrich Corporation, Charlotte, NC (US);
Inventor:
William E Luce, Colleyville, TX (US);
Assignee:
Goodrich Corporation, Charlotte, NC (US);
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
G01P 5/00 (2006.01); B64C 25/60 (2006.01); B64D 45/00 (2006.01); F16F 9/32 (2006.01); F16F 15/023 (2006.01); F16F 9/18 (2006.01); B64C 25/22 (2006.01);
U.S. Cl.
CPC ...
B64C 25/60 (2013.01); B64C 25/22 (2013.01); B64D 45/0005 (2013.01); F16F 9/18 (2013.01); F16F 9/3214 (2013.01); F16F 9/3235 (2013.01); F16F 9/3292 (2013.01); F16F 15/023 (2013.01); G01P 5/00 (2013.01); B64D 2045/008 (2013.01);
Abstract
A landing detection system for a landing gear assembly of an aircraft may comprise a moveable member mechanically coupled between an aircraft wheel and a strut piston, wherein the moveable member is in communication with a strut chamber pressure of the landing gear assembly, wherein the moveable member moves relative to the strut piston in response to a first force applied to the aircraft wheel and the strut piston strokes in response to a second force applied to the aircraft wheel.