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:
Jun. 18, 2024

Filed:

Apr. 13, 2022
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Hejie Li, Mason, OH (US);

Michael A. Benjamin, Cincinnati, OH (US);

Nicholas Ryan Overman, Sharonville, OH (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02C 9/28 (2006.01); F02C 7/224 (2006.01);
U.S. Cl.
CPC ...
F02C 9/28 (2013.01); F02C 7/224 (2013.01); F05D 2220/323 (2013.01); F05D 2240/35 (2013.01); F05D 2270/20 (2013.01); F05D 2270/301 (2013.01); F05D 2270/303 (2013.01);
Abstract

A fuel temperature control system and a method of controlling a fuel temperature for a turbine engine including supplying an aviation fuel to a fuel nozzle fluidly coupled to a combustion chamber. A fuel temperature sensor for determining at least one input parameter to define an inlet fuel temperature of the aviation fuel in the fuel nozzle. A controller for receiving the at least one input parameter and for calculating a calculated flow number in the fuel nozzle. The controller capable of comparing the calculated flow number and a reference flow number associated with a threshold during a steady state condition to determine if the aviation fuel is boiling inside the fuel nozzle.


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