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:
Dec. 31, 2024

Filed:

Feb. 01, 2019
Applicant:

Rtx Corporation, Farmington, CT (US);

Inventors:

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

Ramesh Rajagopalan, Glastonbury, CT (US);

Sorin Bengea, Glastonbury, CT (US);

Assignee:

RTX CORPORATION, Farmington, CT (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02C 7/057 (2006.01); G05B 13/02 (2006.01); G06N 3/08 (2023.01);
U.S. Cl.
CPC ...
F02C 7/057 (2013.01); G05B 13/027 (2013.01); G06N 3/08 (2013.01); F05D 2220/321 (2013.01); F05D 2260/81 (2013.01); F05D 2270/20 (2013.01); F05D 2270/30 (2013.01);
Abstract

A system for neural network compensated aero-thermodynamic gas turbine engine parameter/inlet condition synthesis. The system includes an aero-thermodynamic engine model configured to produce a real-time model-based estimate of engine parameters, a machine learning model configured to generate model correction errors indicating the difference between the real-time model-based estimate of engine parameters and sensed values of the engine parameters, and a comparator configured to produce residuals indicating a difference between the real-time model-based estimate of engine parameters and the sensed values of the engine parameters. The system also includes an inlet condition estimator configured to iteratively adjust an estimate of inlet conditions based on the residuals and adaptive control laws configured to produce engine control parameters for control of gas turbine engine actuators based on the inlet conditions.


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