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. 31, 2021

Filed:

Jan. 04, 2017
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Didier Jean-Louis Yvon, Moissy-Cramayel, FR;

Clementine Charlotte Marie Mouton, Moissy-Cramayel, FR;

Emmanuel Pierre Dimitri Patsouris, Moissy-Cramayel, FR;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 11/38 (2006.01); F01D 7/00 (2006.01); F04D 29/32 (2006.01); F04D 29/36 (2006.01); B64D 27/16 (2006.01); B64D 27/00 (2006.01);
U.S. Cl.
CPC ...
B64C 11/385 (2013.01); B64D 27/16 (2013.01); F01D 7/00 (2013.01); F04D 29/323 (2013.01); B64D 2027/005 (2013.01); F04D 29/36 (2013.01); F05D 2220/323 (2013.01); F05D 2220/36 (2013.01); F05D 2240/14 (2013.01); F05D 2260/57 (2013.01); F05D 2260/70 (2013.01); F05D 2260/74 (2013.01); Y02T 50/60 (2013.01);
Abstract

A system for controlling the pitch of fan blades of a turbine engine propeller, the system including an actuator secured to a casing of the turbine engine, having a movable portion that is movable in translation relative to the casing, the movable portion being mechanically coupled to a load transfer bearing having an outer ring that is coupled to fan blade pivots so that a movement in translation of the movable portion of the actuator leads to a change in the pitch angle of the fan blades, and at least one locking peg secured to the casing of the turbine engine and suitable, in the event of the actuator malfunctioning, for mechanically locking the load transfer bearing in a position wherein the fan blades are feathered.


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