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. 20, 2019

Filed:

Jan. 13, 2016
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Lilian Yann Dumas, Moissy-Cramayel, FR;

Kamel Benderradji, Moissy-Cramayel, FR;

Alain Marc Lucien Bromann, Moissy-Cramayel, FR;

Suzanne Madeleine Coustillas, Moissy-Cramayel, FR;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 17/16 (2006.01);
U.S. Cl.
CPC ...
F01D 17/162 (2013.01); F05D 2220/323 (2013.01); F05D 2240/128 (2013.01); F05D 2260/50 (2013.01); Y02T 50/671 (2013.01);
Abstract

The invention relates to a system for controlling variable pitch blades for a turbine engine, comprising an annular row of variable pitch blades extending about an axis (A) and each comprising a blade connected at the radially outer end thereof to a pivot () that defines a substantially radial axis of rotation of the blade and which is connected by a lever () to control means (,) extending about said axis. The invention is characterized in that said control means include first links () supported by said pivots and second links () extending between said first links, said first and second links extending substantially along a same circumference of said axis and being connected to one another and to actuation means ().


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