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. 17, 2023

Filed:

Nov. 13, 2020
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Alméric Pierre Louis Garnier, Moissy-Cramayel, FR;

Marion Cuny, Moissy-Cramayel, FR;

Tony Alain Roger Joël Lhommeau, Moissy-Cramayel, FR;

Claire Marie Figeureu, Moissy-Cramayel, FR;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
G01M 15/14 (2006.01); F01D 21/00 (2006.01); G01L 3/10 (2006.01);
U.S. Cl.
CPC ...
G01M 15/14 (2013.01); F01D 21/003 (2013.01); G01L 3/109 (2013.01); F05D 2220/323 (2013.01); F05D 2260/83 (2013.01);
Abstract

A method for monitoring the torsion of a rotary shaft on an aircraft turbomachine based on the measurements from at least three sensors distributed along the rotary shaft to divide the shaft into at least two shaft segments, the method comprising: a step of measuring, for each sensor, a parameter dependent on the rotation of the shaft, a step of calculating, for each achievable pair of sensors, a parameter related to the torsion of the shaft, a step of comparing the different calculated parameters related to the torsion of the shaft with references, a step of detecting damage on a shaft segment at the end of the comparison step, and a step of indicating the localization of the damage on the shaft from the shaft segment for which damage has been detected.


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