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:
Jul. 25, 2023

Filed:

Mar. 01, 2021
Applicant:

The Boeing Company, Chicago, IL (US);

Inventors:

Christopher M. Alley, Seattle, WA (US);

Leanne M. Campbell, Snohomish, WA (US);

Gabriela K. Defrancisci, Edmonds, WA (US);

Gregory J. Vering, Seattle, WA (US);

Aaron P. Knock, Seattle, WA (US);

Mitchell Mellor, Bothell, WA (US);

Justin D. Cottet, Snohomish, WA (US);

Assignee:

The Boeing Company, Chicago, IL (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 25/20 (2006.01); B64C 25/12 (2006.01); B64C 25/60 (2006.01); B64C 25/00 (2006.01);
U.S. Cl.
CPC ...
B64C 25/20 (2013.01); B64C 25/12 (2013.01); B64C 25/60 (2013.01); B64C 2025/008 (2013.01);
Abstract

A shrink mechanism for use with a landing gear of an aircraft. The landing gear includes an outer cylinder rotatably coupled to a frame of an aircraft about a trunnion axis of rotation and a shock strut assembly movably coupled to the outer cylinder so as to reciprocate along a longitudinal axis of the outer cylinder. The shrink mechanism incudes a first shrink link member pivotally coupled to the outer cylinder, a second shrink link member coupling the first shrink link member to the shock strut assembly, a crank member pivotally coupled to the outer cylinder, a drive member coupling the crank member to a walking beam of a landing gear retract mechanism, and a driven member coupling the crank member to the first shrink link member.


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