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. 30, 2019

Filed:

Mar. 13, 2017
Applicants:

Rolls-royce Corporation, Indianapolis, IN (US);

Rolls-royce North American Technologies Inc., Indianapolis, IN (US);

Inventors:

Igor Vaisman, Carmel, IN (US);

Michael James Armstrong, Avon, IN (US);

Thomas E. Bastnagel, Danville, IN (US);

Assignees:

Rolls-Royce Corporation, Indianapolis, IN (US);

Rolls-Royce North American Technologies Inc., Indianapolis, IN (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 6/18 (2006.01); F02C 7/10 (2006.01); F01D 15/12 (2006.01); F02C 1/04 (2006.01); F02C 3/04 (2006.01); F02K 3/06 (2006.01); F25B 9/00 (2006.01); F25B 9/06 (2006.01); F02C 1/00 (2006.01); F02C 1/10 (2006.01); F02C 7/08 (2006.01);
U.S. Cl.
CPC ...
F02C 6/18 (2013.01); F01D 15/12 (2013.01); F02C 1/007 (2013.01); F02C 1/04 (2013.01); F02C 1/10 (2013.01); F02C 3/04 (2013.01); F02C 7/08 (2013.01); F02C 7/10 (2013.01); F02K 3/06 (2013.01); F25B 9/008 (2013.01); F25B 9/06 (2013.01); F05D 2220/32 (2013.01); F05D 2240/35 (2013.01); F05D 2260/213 (2013.01); F25B 2309/061 (2013.01); Y02T 50/675 (2013.01);
Abstract

A gas turbine engine may include a deep heat recovery system, such as a deep heat recovery super critical carbon dioxide (sCO2) system. The deep heat recovery system may include two-stage cooling of the working fluid (such as carbon dioxide—CO2) where at least one of cooling stages is recuperative by transferring heat from the working fluid to a flow of compressed air being supplied to a combustor included in the gas turbine engine. The deep heat recovery system may operate in a supercritical cycle, or in a transcritical cycle depending on the temperature to which the working fluid is cooled during a second stage of the two-stage cooling. The second stage of the two-stage cooling includes working fluid-to-air heat rejection where the air is ambient air.


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