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. 22, 2021

Filed:

Jun. 21, 2018
Applicants:

Rolls-royce Corporation, Indianapolis, IN (US);

Rolls-royce North American Technologies Inc., Indianapolis, IN (US);

Inventors:

Kenneth L. Graham, Indianapolis, IN (US);

John Joseph Costello, Indianapolis, IN (US);

Richard Joseph Skertic, Carmel, IN (US);

Assignees:

ROLLS-ROYCE CORPORATION, Indianapolis, IN (US);

ROLLS-ROYCE NORTH AMERICAN TECHNOLOGIES INC., Indianapolis, IN (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 9/26 (2006.01); F02C 9/28 (2006.01); F02C 9/40 (2006.01); F02C 7/232 (2006.01);
U.S. Cl.
CPC ...
F02C 9/28 (2013.01); F02C 7/232 (2013.01); F02C 9/26 (2013.01); F02C 9/40 (2013.01); F05D 2270/13 (2013.01);
Abstract

A gas turbine engine fuel additive control system includes a sensor positioned to sense an operational parameter of a gas turbine engine that includes a compressor section, a combustion section, and a turbine section. The system also includes a control valve positioned to supply a fuel additive to a fuel line. The fuel line contains fuel for supply to the combustion section of the gas turbine engine to which the fuel additive is selectively added by injection into the fuel line. The system also includes a controller configured to monitor the operational parameter in real time during operation of the gas turbine engine and adjust the control valve to dynamically modulate an amount of the fuel additive being supplied in the fuel in accordance with operation of the gas turbine engine.


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