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. 02, 2021

Filed:

Dec. 06, 2019
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Fabrice Michel Francois Rene Aubert, Moissy-Cramayel, FR;

Suzanne Madeleine Coustillas, Moissy-Cramayel, FR;

Paul Antoine Foresto, Moissy-Cramayel, FR;

Didier Pierre Mozer, Moissy-Cramayel, FR;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 5/06 (2006.01); F02C 7/04 (2006.01); F01D 11/00 (2006.01); B29L 31/08 (2006.01); F01D 5/30 (2006.01); F02K 3/06 (2006.01); F04D 29/32 (2006.01);
U.S. Cl.
CPC ...
F02C 7/04 (2013.01); F01D 11/008 (2013.01); B29L 2031/08 (2013.01); F01D 5/066 (2013.01); F01D 5/3007 (2013.01); F02K 3/06 (2013.01); F04D 29/329 (2013.01); F05D 2220/36 (2013.01); F05D 2240/80 (2013.01); F05D 2260/31 (2013.01); F05D 2300/43 (2013.01); F05D 2300/44 (2013.01); F05D 2300/603 (2013.01);
Abstract

A turbine engine fan having an axis of revolution wherein a fan disk having an upstream face and a radial face is configured to receive a series of fan blades. An inter-blade platform wherein an upstream end, a blocking ferrule, are applied and attached on the one hand to the upstream end of the platform and on the other hand to the upstream face of the fan disk, and an inlet cone. The blocking ferrule includes a radial ring and a lug, extending axially from the radial ring and configured to form a radial abutment for the inlet cone.


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