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:
Nov. 29, 2022

Filed:

Jan. 27, 2021
Applicant:

Raytheon Technologies Corporation, Farmington, CT (US);

Inventors:

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

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

Michael G. McCaffrey, Windsor, CT (US);

Assignee:

Raytheon Technologies Corporation, Farmington, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 9/18 (2006.01); F02C 7/32 (2006.01); F01D 17/10 (2006.01); F01D 25/12 (2006.01); F02C 7/36 (2006.01); F04D 29/28 (2006.01); F02C 7/143 (2006.01); F02C 7/18 (2006.01);
U.S. Cl.
CPC ...
F02C 9/18 (2013.01); F01D 17/105 (2013.01); F01D 25/12 (2013.01); F02C 7/143 (2013.01); F02C 7/185 (2013.01); F02C 7/32 (2013.01); F02C 7/36 (2013.01); F04D 29/284 (2013.01); F05D 2220/32 (2013.01); F05D 2220/3212 (2013.01); F05D 2260/211 (2013.01); F05D 2260/213 (2013.01); F05D 2260/4031 (2013.01); F05D 2260/606 (2013.01); F05D 2270/112 (2013.01); F05D 2270/335 (2013.01);
Abstract

A gas turbine engine includes a main compressor section with a downstream most location. A turbine section has a high pressure turbine. A tap line is connected to tap air from a location upstream of the downstream most location in the main compressor section. The tapped air is connected to a heat exchanger and then to a cooling compressor. The cooling compressor compresses air downstream of the heat exchanger, and is connected to deliver air into the high pressure turbine. A bypass valve is positioned downstream of the main compressor section, and upstream of the heat exchanger. The bypass valve selectively delivers air directly to the cooling compressor without passing through the heat exchanger under certain conditions.


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