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:
Jul. 14, 2020

Filed:

Aug. 25, 2017
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Clément Cottet, Melun, FR;

Fabrice Michel François René Cretin, La Grande Paroisse, FR;

Christophe Paul Jacquemard, Hericy, FR;

Christophe Marcel Lucien Perdrigeon, Ballainvilliers, FR;

Leny Toribio, Bayonne, FR;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 25/18 (2006.01); B64C 11/06 (2006.01); B64D 27/10 (2006.01); B64C 11/32 (2006.01); B64D 27/00 (2006.01);
U.S. Cl.
CPC ...
F01D 25/18 (2013.01); B64C 11/06 (2013.01); B64C 11/32 (2013.01); B64D 27/10 (2013.01); B64D 2027/005 (2013.01); F05D 2220/323 (2013.01); F05D 2230/70 (2013.01); Y02T 50/66 (2013.01);
Abstract

A turbine engine is provided with a longitudinal rotation axis having at least one shaft with a radial axis, in particular a pitch change system for the blades of a propeller, said shaft traversing a radial passage of a substantially cylindrical case around the longitudinal axis. The turbine engine includes an annular oil guiding device around the radial shaft. The device has first and second annular parts nested in one another and secured to one another by hooping. The first part is secured by hooping to the radial shaft, and the second part is configured so as to be separated from the first part under the action of a force oriented along the radial axis and exerted on the second part by a member of the turbine engine forming a stop during a radial movement of the radial shaft.


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