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:
Nov. 24, 2015

Filed:

Jan. 11, 2011
Applicants:

Stephane Pierre Guillaume Blanchard, Chartrettes, FR;

Thierry Fachat, Moret sur Loing, FR;

Patrick Joseph Marie Girard, Saint Fargeau Ponthierry, FR;

Clement Roussille, Bordeaux, FR;

Inventors:

Stephane Pierre Guillaume Blanchard, Chartrettes, FR;

Thierry Fachat, Moret sur Loing, FR;

Patrick Joseph Marie Girard, Saint Fargeau Ponthierry, FR;

Clement Roussille, Bordeaux, FR;

Assignees:

SNECMA, Paris, FR;

HERAKLES, Le Haillan, FR;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 5/22 (2006.01); F01D 5/26 (2006.01);
U.S. Cl.
CPC ...
F01D 5/225 (2013.01); F01D 5/26 (2013.01); F05B 2240/33 (2013.01); F05D 2260/96 (2013.01); F05D 2300/2261 (2013.01); F05D 2300/603 (2013.01); Y02T 50/672 (2013.01);
Abstract

A vibration damper between outer platforms of adjacent composite-material blades of a turbine engine rotor wheel, the damper including a peg having a substantially spherical portion at each of its two ends, and two hollow inserts for being received in tangential cavities that are provided facing each other in outer platforms of two adjacent composite-material blades of a turbine engine rotor wheel, each spherical portion of the peg coming to bear with point contact against the inside of one of the inserts.


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