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:
Sep. 12, 2023

Filed:

Jul. 03, 2018
Applicant:

Raytheon Technologies Corporation, Farmington, CT (US);

Inventors:

Daniel A. Snyder, Manchester, CT (US);

David J. Yudichak, Tolland, CT (US);

Kurt R. Heinemann, East Hampton, CT (US);

Perry Bowes, Manchester, CT (US);

Evan Selin, Rocky Hill, CT (US);

Assignee:

RTX Corporation, Farmington, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
G06F 30/20 (2020.01); G06F 30/17 (2020.01); G06F 30/15 (2020.01); G06N 20/00 (2019.01);
U.S. Cl.
CPC ...
G06F 30/20 (2020.01); G06F 30/15 (2020.01); G06F 30/17 (2020.01); F05D 2260/81 (2013.01); G06N 20/00 (2019.01);
Abstract

A qualification system for gas turbine engine components includes a computer system configured to receive a set of measured parameters for each gas turbine engine component in a plurality of substantially identical gas turbine engine components, and determine a variation model based on the set of measured parameters. The computer system includes at least one simulated engine model configured to determine a predicted operation of each gas turbine engine component in the plurality of substantially identical gas turbine engine components, a correlation system configured to correlate variations in the set of parameters for each of the gas turbine engine components with a set of the predicted operations of each gas turbine engine, thereby generating a predictive model based on the variations. The computer system also includes a qualification module configured to generate a qualification formula based on the predictive model. The qualification formula is configured to receive a set of measured parameters of an as-manufactured gas turbine engine component and determine when the as manufactured gas turbine engine component is qualified for inclusion in at least one engine.


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