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:
Mar. 03, 2020

Filed:

Apr. 18, 2018
Applicant:

Safran Landing Systems Uk Ltd, Gloucester, GB;

Inventors:

Simone Urbinati, Gloucester, GB;

Matt Hilliard, Gloucester, GB;

Jon Smith, Gloucester, GB;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 25/60 (2006.01); F16F 9/06 (2006.01); B64C 25/00 (2006.01);
U.S. Cl.
CPC ...
B64C 25/60 (2013.01); F16F 9/062 (2013.01); F16F 9/063 (2013.01); B64C 2025/008 (2013.01); F16F 2222/12 (2013.01); F16F 2232/08 (2013.01); F16F 2234/02 (2013.01); F16F 2236/045 (2013.01);
Abstract

An aircraft landing gear shock absorbing strut having an outer cylinder and a sliding tube coupled within the cylinder bore to move between compressed and extended conditions. The cylinder and tube define a variable-volume internal chamber. The internal chamber is divided into a first spring chamber and a second spring chamber. The first spring chamber is a pneumatic chamber containing a first gas that is compressed when the strut moves from the extended condition to the compressed condition to provide compression damping. The second spring chamber contains a second gas and a hydraulic liquid, and is configured to compress the second gas when the strut moves from the extended condition to the compressed condition. The second spring chamber contains one or more damping orifices through which the oil passes as the strut extends to provide recoil damping during extension of the strut.


Find Patent Forward Citations

Urbinati, Simone. (2020). Aircraft landing gear shock absorbing strut (U.S. Patent No. 10577088). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/10577088

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

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