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. 16, 2024

Filed:

Jul. 20, 2022
Applicant:

General Electric Company, Schenectady, NY (US);

Inventor:

David Justin Brady, Rockport, MA (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 9/26 (2006.01); F02C 7/232 (2006.01); F02C 7/236 (2006.01); F02C 9/28 (2006.01); F02C 9/30 (2006.01); F02C 9/32 (2006.01); F02C 9/36 (2006.01); F02C 9/46 (2006.01);
U.S. Cl.
CPC ...
F02C 9/263 (2013.01); F02C 7/232 (2013.01); F02C 7/236 (2013.01); F02C 9/28 (2013.01); F02C 9/30 (2013.01); F02C 9/32 (2013.01); F02C 9/36 (2013.01); F02C 9/46 (2013.01); F05D 2270/09 (2013.01); F05D 2270/3015 (2013.01); F05D 2270/304 (2013.01);
Abstract

A fuel supply system for a turbine engine that provides a modulated thrust control malfunction accommodation (TCMA) is disclosed. An example fuel supply system includes a fuel supply line to supply fuel to a combustion engine, a fuel metering valve coupled to the fuel supply line, the fuel metering valve to control a flow of fuel through the fuel supply line to the combustion engine, a throttle valve coupled to the fuel supply line downstream of the fuel metering valve, the throttle valve to bleed off fuel supplied to the combustion engine based on a pressure difference across the fuel metering valve, and a controllable servo coupled to the throttle valve, the controllable servo to control the throttle valve based on a sensor output indicative of the pressure difference.


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