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:
Oct. 17, 2023

Filed:

Mar. 01, 2021
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Jeffrey Douglas Rambo, Mason, OH (US);

Brandon Wayne Miller, Liberty Township, OH (US);

Kevin Robert Feldmann, Mason, OH (US);

Patrick Michael Marrinan, Cincinnati, OH (US);

Robert Jon McQuiston, Cincinnati, OH (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 7/18 (2006.01); F01D 25/12 (2006.01); F02C 7/14 (2006.01);
U.S. Cl.
CPC ...
F02C 7/185 (2013.01); F01D 25/12 (2013.01); F02C 7/14 (2013.01); F05D 2220/323 (2013.01); F05D 2260/20 (2013.01); F05D 2270/112 (2013.01); F05D 2270/301 (2013.01); F05D 2270/3032 (2013.01);
Abstract

A method is provided of controlling a cooled cooling air system for an aeronautical gas turbine engine. The method includes: receiving data indicative of an ambient condition of the aeronautical gas turbine engine, data indicative of a deterioration parameter of the aeronautical gas turbine engine, data indicative of an operating condition of the aeronautical gas turbine engine, or a combination thereof; and modifying a cooling capacity of the cooled cooling air system in response to the received data indicative of the ambient condition of the aeronautical gas turbine engine, data indicative of the deterioration parameter of the aeronautical gas turbine engine, data indicative of an operating condition of the aeronautical gas turbine engine, or the combination thereof.


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