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:
Mar. 03, 2020

Filed:

Jun. 20, 2013
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Christophe Javelot, Rungis, FR;

Cedrik Djelassi, Marolles en Hurepoix, FR;

Bruno Robert Gaully, Marolles en Hurepoix, FR;

Ismail Sylla, Toulouse, FR;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02C 9/00 (2006.01); F02C 9/26 (2006.01); F02C 9/32 (2006.01);
U.S. Cl.
CPC ...
F02C 9/26 (2013.01); F02C 9/263 (2013.01); F02C 9/32 (2013.01); F05D 2220/323 (2013.01); F05D 2270/044 (2013.01); F05D 2270/114 (2013.01); F05D 2270/306 (2013.01); F05D 2270/309 (2013.01);
Abstract

A method of adjusting a fuel flow rate in a turbine engine propelling an aircraft, including: obtaining a first estimate of a flow rate of fuel injected into a combustion chamber of the turbine engine propelling an aircraft and as delivered by a fuel metering device of the turbine engine; obtaining a second estimate of the fuel flow rate, which second estimate is more accurate than the first estimate for at least one range of fuel flow rate values and being delivered by an estimator device having a flow meter; and adjusting the fuel flow rate threshold value with help of a difference evaluated between the first estimate and the second estimate, the threshold value being for use in an open loop for regulating the turbine engine.


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