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. 19, 2021

Filed:

Aug. 15, 2019
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Thomas Nolwenn Emmanuel Delahaye, Courtomer, FR;

Kamel Benderradji, Livry-sur-Seine, FR;

Delphine Hermanee Maxime Parent, Montrouge, FR;

Sandrine Hélène Quevreux, Ballainvilliers, FR;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 9/04 (2006.01); F01D 5/03 (2006.01); F01D 5/20 (2006.01); B64F 5/10 (2017.01);
U.S. Cl.
CPC ...
F01D 9/042 (2013.01); B64F 5/10 (2017.01); F01D 5/03 (2013.01); F01D 5/20 (2013.01);
Abstract

A ring for guiding variable-pitch blades and supporting an abradable coating for an aircraft turbomachine ring extends about an axis (X) and includes substantially radial orifices for mounting guiding sleeves intended each to receive a pivot of one of the blades. The ring may include a radially inner crown divided into sectors and supports the abradable coating. A radially outer annular ferrule may be divided into sectors and include the orifices for mounting the sleeves. In some embodiments, each ferrule sector is mounted about a crown sector by a circumferential sliding connection. The crown sector may include an immobilizer for rotationally immobilizing the sleeves of this ferrule sector about the axis.


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