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. 10, 2024

Filed:

Nov. 29, 2019
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Soufiane Herda, Moissy-Cramayel, FR;

Vincent Michel Cabret, Moissy-Cramayel, FR;

Cedrik Djelassi, Moissy-Cramayel, FR;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02C 9/28 (2006.01); F02C 9/20 (2006.01); F04D 27/00 (2006.01); F04D 27/02 (2006.01);
U.S. Cl.
CPC ...
F02C 9/28 (2013.01); F02C 9/20 (2013.01); F04D 27/001 (2013.01); F04D 27/0246 (2013.01); F05D 2220/323 (2013.01); F05D 2270/083 (2013.01); F05D 2270/101 (2013.01); F05D 2270/3011 (2013.01); F05D 2270/303 (2013.01);
Abstract

A method for detecting a rotating stall includes: determining a level of variation of a static pressure in a combustion chamber of the turbojet engine around an average value of this static pressure; comparing the level of variation of the static pressure relative to a first threshold; comparing a temperature measured at the outlet of a turbine of the turbojet engine relative to a second threshold; and if the level of variation of the static pressure is greater than the first threshold and the temperature at the outlet of the turbine is greater than the second threshold, detecting a presence of a rotating stall.


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