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:
Feb. 18, 2025

Filed:

Mar. 03, 2022
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Julien Fabien Patrick Becoulet, Moissy-Cramayel, FR;

Olivier Belmonte, Moissy-Cramayel, FR;

Vincent François Georges Millier, Moissy-Cramayel, FR;

Jean Charles Olivier Roda, Moissy-Cramayel, FR;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02C 7/06 (2006.01); F01D 7/00 (2006.01); F01D 25/16 (2006.01); F16H 57/04 (2010.01); F16H 57/08 (2006.01);
U.S. Cl.
CPC ...
F02C 7/06 (2013.01); F01D 7/00 (2013.01); F01D 25/16 (2013.01); F16H 57/043 (2013.01); F16H 57/0471 (2013.01); F16H 57/0486 (2013.01); F16H 57/082 (2013.01); F05D 2220/36 (2013.01); F05D 2230/60 (2013.01); F05D 2240/50 (2013.01); F05D 2260/40311 (2013.01); F05D 2260/70 (2013.01);
Abstract

A fan module for an aircraft turbine engine includes a fan having variable pitch blades and an oil transfer device configured to provide a transfer of oil between a stator and a rotor. The oil transfer device includes a stator ring having internal oil ducts, a shaft inserted into the ring and having internal oil ducts, and an annular support of the ring configured to deform elastically to allow movements of the ring in the radial direction. A plain bearing is located between the ring and the shaft, and roller bearings are mounted between the ring and the shaft on either side of the plain bearing.


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