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:
Dec. 07, 2021

Filed:

Mar. 23, 2016
Applicant:

Airbus Helicopters, Marignane, FR;

Inventors:

Pierre Prud'Homme-Lacroix, Vitrolles, FR;

Patrice Garcin, Ensues, FR;

Assignee:

AIRBUS HELICOPTERS, Marignane, FR;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 25/52 (2006.01); B64C 25/60 (2006.01); B64C 25/58 (2006.01); F16F 9/20 (2006.01); B64C 25/32 (2006.01);
U.S. Cl.
CPC ...
B64C 25/52 (2013.01); B64C 25/58 (2013.01); B64C 25/60 (2013.01); F16F 9/20 (2013.01); B64C 2025/325 (2013.01);
Abstract

Landing gear for an aircraft, the landing gear having at least one pair of shock absorbers comprising a first shock absorber and a second shock absorber, each shock absorber comprising a cylinder defining an inside space and a rod carrying a piston, the inside space being subdivided at least into a 'primary' chamber and into a 'secondary' chamber, the shock absorber including at least one throttling orifice putting the secondary chamber into fluid flow communication with the primary chamber. The primary chamber of the first shock absorber is connected to the secondary chamber of the second shock absorber of the pair by a first pipe, and the secondary chamber of the first shock absorber of the pair is connected to the primary chamber of the second shock absorber of the pair by a second pipe.


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