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:
Aug. 15, 2017

Filed:

Jan. 19, 2015
Applicant:

United Technologies Corporation, Farmington, CT (US);

Inventor:

Chaohong Cai, Westogue, CT (US);

Assignee:

UNITED TECHNOLOGIES CORPORATION, Hartford, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 21/00 (2006.01); F01D 17/10 (2006.01); F01D 17/06 (2006.01); G05B 13/04 (2006.01);
U.S. Cl.
CPC ...
F01D 21/003 (2013.01); F01D 17/06 (2013.01); F01D 17/105 (2013.01); G05B 13/048 (2013.01); F05D 2220/32 (2013.01); F05D 2240/12 (2013.01); F05D 2270/304 (2013.01); F05D 2270/335 (2013.01); F05D 2270/52 (2013.01); F05D 2270/62 (2013.01);
Abstract

A control system for a gas turbine engine including a power turbine is disclosed. The control system may include a control module to receive engine operating goals and an estimated current engine state, wherein the estimated current engine state is produced by a model-based estimation module using a bandwidth signal produced by an adaptation logic module. The control module is operative to determine fuel flow, inlet guide vane schedules and stability bleed schedules based at least in part on the received engine operating goals and the estimated current engine state, and to send signals to a gas generator of the gas turbine engine in order to control the gas generator according to the determined fuel flow, inlet guide vane schedules and stability bleed schedules.


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