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. 12, 2024

Filed:

Oct. 16, 2020
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Vivien Mickaël Courtier, Moissy-Cramayel, FR;

Christophe Paul Jacquemard, Moissy-Cramayel, FR;

Vincent Joudon, Moissy-Cramayel, FR;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 5/30 (2006.01); B64C 11/04 (2006.01); F01D 5/32 (2006.01); B64D 27/00 (2006.01);
U.S. Cl.
CPC ...
F01D 5/3015 (2013.01); B64C 11/04 (2013.01); F01D 5/326 (2013.01); B64D 2027/005 (2013.01); F05D 2220/323 (2013.01); F05D 2260/31 (2013.01);
Abstract

The invention relates to an assembly for a turbine engine blade, the assembly comprising a fastener defining a well for receiving a blade root, and a clamping device for clamping the blade root against the fastener when the blade root is received in the well, wherein the clamping device comprises: at least one clamping member suitable for bearing simultaneously on the blade root and on the fastener in the well so as to exert a clamping force on the blade root, the clamping member defining a threaded hole, and a resilient layer arranged to bear in the well on the blade root, a rod comprising a thread engaging with the threaded hole so that a rotation of the rod with respect to the clamping member causes a variation in the clamping force exerted by the clamping member on the root.


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