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:
Aug. 25, 2020

Filed:

Jul. 11, 2016
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Pierre-Alain Francis Claude Sebrecht, Moissy-Cramayel, FR;

Damien Joseph Cellier, Moissy-Cramayel, FR;

Cédric Michel Claude Chretien, Moissy-Cramayel, FR;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 17/16 (2006.01); F04D 29/56 (2006.01); F04D 29/056 (2006.01); F04D 29/64 (2006.01); F04D 29/08 (2006.01);
U.S. Cl.
CPC ...
F04D 29/563 (2013.01); F01D 17/162 (2013.01); F04D 29/056 (2013.01); F04D 29/644 (2013.01); F04D 29/083 (2013.01); F05D 2220/323 (2013.01); F05D 2220/3219 (2013.01); F05D 2240/129 (2013.01); F05D 2240/50 (2013.01); F05D 2250/232 (2013.01);
Abstract

A stage of variable-pitch vanes for a turbine engine includes a plurality of vanes. Each vane has a blade with a first radially internal frusto-conical surface. The cone angle of the first frusto-conical surface is radially flared inwards and is configured to interact with an internal frusto-conical surface of a first frusto-conical bushing. The vane further includes a second radially external frusto-conical surface with cone angle that is radially flared outwards and is configured to interact with an internal frusto-conical surface of a second substantially frusto-conical bushing.


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