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:
Apr. 12, 2022

Filed:

Dec. 13, 2018
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Adel Cédric Abir Widemann, Moissy-Cramayel, FR;

Nicolas Raillard, Moissy-Cramayel, FR;

Cedrik Djelassi, Moissy-Cramayel, FR;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 7/264 (2006.01); F01D 19/02 (2006.01);
U.S. Cl.
CPC ...
F02C 7/264 (2013.01); F01D 19/02 (2013.01); F05D 2260/80 (2013.01); F05D 2260/85 (2013.01); F05D 2260/99 (2013.01); F05D 2270/301 (2013.01); F05D 2270/303 (2013.01); F05D 2270/304 (2013.01);
Abstract

The invention relates to a method (E) for detecting the ignition of a turbine engine combustion chamber, the method (E) comprising the steps of: receiving (E) a first measurement of the exhaust gas temperature downstream from the combustion chamber, before an attempt to ignite said combustion chamber; receiving (E) a temperature threshold; receiving (E) a secondary detection criterion; updating (E) the received temperature threshold as a function of the secondary detection criterion received; receiving (E) a second measurement of the exhaust gas temperature, after the attempt to ignite the combustion chamber; comparing (E) the updated temperature threshold with the difference between the first and second exhaust gas temperature measurements; and determining (E) the state of ignition of the combustion chamber.


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