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:
Mar. 24, 2020

Filed:

Apr. 02, 2015
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Sanji Ekanayake, Mableton, GA (US);

Thomas Edward Wickert, Greenville, SC (US);

Alston Ilford Scipio, Mableton, GA (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorneys:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02C 7/00 (2006.01); F02C 7/14 (2006.01); F28D 15/02 (2006.01); F02C 6/18 (2006.01); F01D 5/08 (2006.01); F02C 7/224 (2006.01); F01D 9/06 (2006.01); F02C 7/143 (2006.01); F01D 5/18 (2006.01); F02C 7/18 (2006.01); F01D 25/12 (2006.01); F02C 3/04 (2006.01); F02C 7/06 (2006.01); F28F 23/00 (2006.01); F28D 21/00 (2006.01);
U.S. Cl.
CPC ...
F02C 7/14 (2013.01); F01D 5/082 (2013.01); F01D 5/088 (2013.01); F01D 5/181 (2013.01); F01D 9/065 (2013.01); F01D 25/125 (2013.01); F02C 3/04 (2013.01); F02C 6/18 (2013.01); F02C 7/06 (2013.01); F02C 7/143 (2013.01); F02C 7/18 (2013.01); F02C 7/185 (2013.01); F02C 7/224 (2013.01); F28D 15/0233 (2013.01); F28D 15/0275 (2013.01); F28F 23/00 (2013.01); F05D 2260/208 (2013.01); F05D 2260/213 (2013.01); F05D 2300/5024 (2013.01); F28D 2021/0026 (2013.01);
Abstract

A turbomachine includes a compressor configured to compress air received at an intake portion to form a compressed airflow that exits into an outlet portion. A combustor is operably connected with the compressor, and receives the compressed airflow. A turbine is operably connected with the combustor, and receives the combustion gas flow. The turbine has a plurality of wheels and a plurality of buckets. The turbine receives compressor bleed off air to cool the wheels and buckets. A cooling system is operatively connected to the turbine. The cooling system includes a plurality of heat pipes located axially upstream of at least one of the wheels. The heat pipes are operatively connected to a bearing cooler system. The heat pipes and the bearing cooler system are configured to transfer heat from the compressor bleed off air to one or more heat exchangers.


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