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:
May. 07, 2024

Filed:

Apr. 10, 2023
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Steven Douglas Johnson, Milford, OH (US);

Julius John Montgomery, Mason, OH (US);

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

Robert Proctor, Mason, OH (US);

Bradley W. Fintel, West Chester, OH (US);

Jeffrey Douglas Rambo, Mason, OH (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 11/24 (2006.01); F01D 5/03 (2006.01); F01D 11/18 (2006.01); F02C 6/08 (2006.01); F02C 7/18 (2006.01); F01D 25/12 (2006.01); F01D 25/14 (2006.01);
U.S. Cl.
CPC ...
F01D 11/24 (2013.01); F01D 5/03 (2013.01); F01D 11/18 (2013.01); F02C 6/08 (2013.01); F02C 7/185 (2013.01); F01D 25/12 (2013.01); F01D 25/14 (2013.01); F05D 2220/323 (2013.01); F05D 2240/11 (2013.01); F05D 2240/55 (2013.01); F05D 2260/20 (2013.01); F05D 2260/30 (2013.01);
Abstract

A system for controlling blade clearances within a gas turbine engine includes a rotor disk and a rotor blade coupled to the rotor disk. Additionally, the system includes an outer turbine component positioned outward of the rotor blade such that a clearance is defined between the rotor blade and the outer turbine component. Furthermore, the system includes a heat exchanger configured to receive a flow of cooling air bled from the gas turbine engine and transfer heat from the received flow of the cooling air to a flow of coolant to generate cooled cooling air. Moreover, the system includes a valve configured to control the flow of the coolant to the heat exchanger. In this respect, the cooled cooling air is supplied to at least one of the rotor disk or the rotor blade to adjust the clearance between the rotor blade and the outer turbine component.


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