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:
Jul. 12, 2022

Filed:

Jun. 02, 2020
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Ilhan Bayraktar, West Chester, OH (US);

Tuba Bayraktar, West Chester, OH (US);

Mohamed Elbibary, West Chester, OH (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02C 7/18 (2006.01); F02C 7/12 (2006.01); F01D 21/00 (2006.01); B64D 33/08 (2006.01); F01D 25/24 (2006.01); F02C 9/18 (2006.01); F04D 27/00 (2006.01); F02C 6/08 (2006.01); F04D 19/02 (2006.01);
U.S. Cl.
CPC ...
F02C 7/18 (2013.01); B64D 33/08 (2013.01); F01D 21/00 (2013.01); F01D 25/24 (2013.01); F02C 7/125 (2013.01); F02C 9/18 (2013.01); F04D 27/009 (2013.01); F02C 6/08 (2013.01); F04D 19/02 (2013.01); F05D 2220/32 (2013.01); F05D 2240/24 (2013.01); F05D 2260/232 (2013.01); Y02T 50/60 (2013.01);
Abstract

A cooling system configured to reduce a temperature within a gas turbine engine in a shutdown mode of operation includes a first gas turbine engine including a compressor having a bleed port. In a first operating mode of the gas turbine engine, the compressor bleed port is configured to channel a high pressure flow of air from the compressor. During a shutdown mode of operation, the compressor bleed port is configured to channel an external flow of cooling air into the compressor. The cooling system also includes a source of cooling air and a conduit coupled in flow communication between the compressor bleed port and the source of cooling air. The source of cooling air configured to deliver a flow of cooling air into the compressor through the compressor bleed port.


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