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:
May. 09, 2023

Filed:

Mar. 20, 2019
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Nicolas Xavier Trappier, Moissy-Cramayel, FR;

Pierrot Guillou, Moissy-Cramayel, FR;

Caroline Marie Frantz, Moissy-Cramayel, FR;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 5/06 (2006.01); F01D 21/02 (2006.01);
U.S. Cl.
CPC ...
F01D 21/02 (2013.01); F01D 5/06 (2013.01); F05D 2240/60 (2013.01);
Abstract

A turbine shaft of a turbomachine extending along a longitudinal axis (A) includes a main tubular portion with a length Land a maximum outer main diameter. The shaft further includes a secondary tubular segment with a length Land a maximum outer secondary diameter greater than the maximum outer main diameter. The secondary tubular segment extends radially from the shaft such that the main tubular portion extends on either side of the secondary tubular segment along the longitudinal axis (A). The secondary tubular segment includes a weak point that is configured to break the shaft into two distinct parts when the value of a tangential stress applied to the shaft exceeds a predetermined threshold value, and thus cause retraction of the turbine.


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