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:
Jul. 14, 2020

Filed:

Apr. 08, 2019
Applicant:

United Technologies Corporation, Farmington, CT (US);

Inventors:

Chaohong Cai, Weatogue, CT (US);

Timothy J. Crowley, Tolland, CT (US);

Mark E. Lacour, Glastonbury, CT (US);

David Lei Ma, Avon, CT (US);

Assignee:

RAYTHEON TECHNOLOGIES CORPORATION, Farmington, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02K 1/17 (2006.01); F02C 9/50 (2006.01); F02C 9/54 (2006.01); F02C 9/00 (2006.01);
U.S. Cl.
CPC ...
F02K 1/17 (2013.01); F02C 9/00 (2013.01); F02C 9/50 (2013.01); F02C 9/54 (2013.01); F05D 2270/20 (2013.01); F05D 2270/44 (2013.01); F05D 2270/71 (2013.01);
Abstract

A control system for a gas turbine engine, a method for controlling a gas turbine engine, and a gas turbine engine are disclosed. The control system may include a nozzle scheduler for determining an exhaust nozzle position goal based on a nozzle schedule of exhaust nozzle positions related to flight conditions. The control system may further include a control module for determining a control command for the gas turbine engine. The control command may include, at least, a fuel flow command and an exhaust nozzle position command and the control command may be based on, at least, the exhaust nozzle position goal and an estimated thrust value. The control system may further include an actuator for controlling the gas turbine engine based on the control command.


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