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:
May. 26, 2020

Filed:

Jan. 09, 2018
Applicant:

The Boeing Company, Chicago, IL (US);

Inventors:

Leo W. Plude, Woodinville, WA (US);

Malcolm S. Bryant, Maple Valley, WA (US);

Gary M. Lindahl, Newcastle, WA (US);

Edward J. Nowakowski, St. Peters, MO (US);

Assignee:

The Boeing Company, Chicago, IL (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 25/22 (2006.01); F15B 11/072 (2006.01); F15B 11/00 (2006.01); B64C 25/60 (2006.01); B64C 25/34 (2006.01); B64C 25/12 (2006.01);
U.S. Cl.
CPC ...
B64C 25/22 (2013.01); B64C 25/60 (2013.01); F15B 11/003 (2013.01); F15B 11/072 (2013.01); B64C 25/34 (2013.01); B64C 2025/125 (2013.01); F15B 2211/30505 (2013.01);
Abstract

Hydraulic systems for shrinking landing gear shrink are described. An example apparatus includes a landing gear strut, a transfer cylinder, aircraft hydraulics, a pressure vessel, and a pressure-operated check valve. The landing gear strut has an outer cylinder and an inner cylinder movable relative to the outer cylinder between a first position and a second position. The landing gear strut has a first length when the inner cylinder is in the first position and a second length less than the first length when the inner cylinder is in the second position. The transfer cylinder exchanges hydraulic fluid with the landing gear strut. The aircraft hydraulics exchange hydraulic fluid with the transfer cylinder. The pressure vessel exchanges gas with the landing gear strut. The pressure-operated check valve controls an exchange of gas between the pressure vessel and the landing gear strut based on hydraulic fluid received from the aircraft hydraulics.


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