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. 15, 2024

Filed:

Jan. 10, 2022
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Julien Fabien Patrick Becoulet, Moissy-Cramayel, FR;

Olivier Formica, Moissy-Cramayel, FR;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 25/18 (2006.01); F01D 25/16 (2006.01); F02C 3/107 (2006.01); F02C 7/06 (2006.01); F02C 7/28 (2006.01);
U.S. Cl.
CPC ...
F01D 25/183 (2013.01); F01D 25/16 (2013.01); F02C 3/107 (2013.01); F02C 7/06 (2013.01); F02C 7/28 (2013.01); F05D 2220/32 (2013.01); F05D 2240/50 (2013.01); F05D 2240/55 (2013.01); F05D 2240/60 (2013.01); F05D 2260/40 (2013.01); F05D 2260/98 (2013.01);
Abstract

A turbomachine fan module includes a fan shaft and a lubrication chamber traversed axially by at least part of the fan shaft. The module further includes at least one first bearing configured to support and guide the fan shaft in rotation. The fan shaft has a first tubular part closed by a cover, wherein the first tubular part has a distal end and a proximal end that are opposite each other along a longitudinal axis X and an annular squealer cavity, formed in an inner surface of the fan shaft, between the distal end and the proximal end. The cover has a body extending along the longitudinal axis X and mounted in the first tubular portion so as to cover and sealingly close the annular squealer cavity.


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