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:
Oct. 12, 2021

Filed:

Oct. 10, 2017
Applicant:

Airbus Helicopters, Marignane, FR;

Inventors:

Stephane Mazet, Rognac, FR;

Jean-Romain Bihel, Le Rove, FR;

Mathias Fournier, Aix en Provence, FR;

Sylvain Berthalon, Velaux, FR;

Assignee:

AIRBUS HELICOPTERS, Marignane, FR;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 27/51 (2006.01); B64C 27/00 (2006.01); B64C 27/35 (2006.01); B64C 27/48 (2006.01);
U.S. Cl.
CPC ...
B64C 27/51 (2013.01); B64C 27/001 (2013.01); B64C 27/35 (2013.01); B64C 27/48 (2013.01);
Abstract

A lead-lag damper arranged inside a blade of a rotor of a rotary wing aircraft. The lead-lag damper comprises an inner strength member provided with a cage in which a ball-joint connection is arranged, an outer strength member for securing to the blade, and an elastomer material member arranged between the two strength members. The two strength members and the elastomer material member extending beyond the zone around the cage so that the relative movements between two strength members resulting from the movements of the blade are damped by deformations of the elastomer material member, at least a portion of the lead-lag damper being designed to occupy a portion of the inside of the blade that is conventionally filled with foam.


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