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. 21, 2025

Filed:

May. 07, 2024
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Clément Cottet, Moissy-Cramayel, FR;

Vivien Mickaël Courtier, Moissy-Cramayel, FR;

Vincent Joudon, Moissy-Cramayel, FR;

Thierry Georges Paul Papin, Moissy-Cramayel, FR;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 11/06 (2006.01); F01D 7/00 (2006.01); F04D 29/32 (2006.01); F04D 29/64 (2006.01);
U.S. Cl.
CPC ...
B64C 11/06 (2013.01); F01D 7/00 (2013.01); F04D 29/323 (2013.01); F04D 29/644 (2013.01); F05D 2260/70 (2013.01);
Abstract

An assembly for an aircraft turbine engine is provided. The assembly generally includes an un-ducted propeller blade of which the root has a bulbous portion; a system for setting the pitch of the blade about a pitch setting axis, the pitch setting system including a cup configured to be placed inside the outer casing, has a flared open top end for axial insertion of the root and in which the root of the blade can be axially affixed by a locking member; and at least one radial retention prong in a radial space reserved between the wall of the cup and the root.


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