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:
Jun. 25, 2019

Filed:

Dec. 14, 2015
Applicant:

United Technologies Corporation, Farmington, CT (US);

Inventors:

Gabriel L. Suciu, Glastonbury, CT (US);

Brian D. Merry, Andover, CT (US);

Jesse M. Chandler, South Windsor, CT (US);

William K. Ackermann, East Hartford, CT (US);

Matthew R. Feulner, West Hartford, CT (US);

Om P. Sharma, South Windsor, CT (US);

Assignee:

United Technologies Corporation, Farmington, CT (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02C 7/18 (2006.01); F02C 7/143 (2006.01); F02C 9/18 (2006.01); F02C 3/04 (2006.01); F02K 3/06 (2006.01); F01D 5/08 (2006.01); F04D 29/58 (2006.01);
U.S. Cl.
CPC ...
F02C 7/18 (2013.01); F01D 5/08 (2013.01); F02C 3/04 (2013.01); F02C 7/143 (2013.01); F02C 7/185 (2013.01); F02C 9/18 (2013.01); F02K 3/06 (2013.01); F04D 29/5826 (2013.01); F05D 2220/32 (2013.01); F05D 2220/3219 (2013.01); F05D 2240/24 (2013.01); F05D 2260/205 (2013.01); F05D 2260/211 (2013.01); F05D 2260/213 (2013.01);
Abstract

A compressor section for use in a gas turbine engine comprises a compressor rotor having a hub and a plurality of blades extending radially outwardly from the hub and an outer housing surrounding an outer periphery of the blades. A tap taps air at a radially outer first location, passing the tapped air through a heat exchanger, and returning the tapped air to an outlet at a second location which is radially inward of the first location, to provide cooling air adjacent to the hub. A gas turbine engine is also disclosed.


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