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:
Nov. 07, 2023

Filed:

Feb. 19, 2020
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Arnaud Nicolas Negri, Moissy-Cramayel, FR;

Julien Fabien Patrick Becoulet, Moissy-Cramayel, FR;

Michel Gilbert Roland Brault, Moissy-Cramayel, FR;

Romain Guillaume Cuvillier, Moissy-Cramayel, FR;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02C 7/36 (2006.01); F16C 3/02 (2006.01); F16D 9/08 (2006.01);
U.S. Cl.
CPC ...
F02C 7/36 (2013.01); F16C 3/023 (2013.01); F16D 9/08 (2013.01); F05D 2240/60 (2013.01); F16C 2326/43 (2013.01);
Abstract

A drive shaft of an aircraft turbine engine includes a first portion and a second portion, and connecting means connecting the first and second portions and being configured to transmit a torque from the second portion to the first portion. The connecting means has at least one bellows with a first section having a diameter greater than the diameters of the first and second portions and second sections flanking the first section. The first section includes at least one fusible section with at least one through-hole and being configured to break when the value of a torque applied to the first portion exceeds a predetermined threshold value.


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