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:
Sep. 19, 2023

Filed:

Jan. 08, 2021
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Antoine Hervé Dos Santos, Moissy-Cramayel, FR;

Joao Antonio Amorim, Moissy-Cramayel, FR;

Pascal Grégory Casaliggi, Moissy-Cramayel, FR;

Nicolas Xavier Trappier, Moissy-Cramayel, FR;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 21/04 (2006.01); F01D 5/02 (2006.01);
U.S. Cl.
CPC ...
F01D 21/045 (2013.01); F01D 5/025 (2013.01); F01D 5/026 (2013.01); F05D 2260/31 (2013.01); F05D 2260/36 (2013.01); F05D 2270/021 (2013.01); F05D 2270/09 (2013.01);
Abstract

An assembly for a turbine engine turbine includes a turbine rotor disc centered on a longitudinal axis and a turbine shaft centered on the longitudinal axis and driven in rotation by the rotor disc. Torque from the rotor disc is transmitted to the shaft, wherein the rotor disc is locked in translation relative to the shaft in the direction of the longitudinal axis by a screwed member on the shaft. Torque from the rotor disc is transmitted from the rotor disc to the screwed member when the torque ceases being transmitted from the rotor disc to the shaft. The screwed member has an unscrewing direction identical to the direction of rotation of the rotor disc in operation.


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