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. 09, 2020

Filed:

Apr. 25, 2018
Applicants:

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

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

Inventors:

Michael J. Armstrong, Avon, IN (US);

Igor Vaisman, Carmel, IN (US);

Assignees:

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

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

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02K 3/00 (2006.01); F01K 23/10 (2006.01); F02K 3/077 (2006.01); F02C 1/00 (2006.01); F02C 1/10 (2006.01); F02C 7/08 (2006.01); F02C 7/141 (2006.01); F02C 7/18 (2006.01); F22B 3/08 (2006.01); F01K 25/10 (2006.01); F02C 6/20 (2006.01); F02C 3/10 (2006.01); F02K 99/00 (2009.01); F02C 7/143 (2006.01); F02C 3/13 (2006.01); F02C 3/04 (2006.01);
U.S. Cl.
CPC ...
F02K 3/00 (2013.01); F01K 23/10 (2013.01); F02C 1/007 (2013.01); F02C 1/10 (2013.01); F02C 3/10 (2013.01); F02C 6/206 (2013.01); F02C 7/08 (2013.01); F02C 7/141 (2013.01); F02C 7/18 (2013.01); F02K 3/077 (2013.01); F02K 99/00 (2013.01); F01K 25/103 (2013.01); F02C 3/04 (2013.01); F02C 3/13 (2013.01); F02C 7/143 (2013.01); F05D 2210/10 (2013.01); F05D 2210/13 (2013.01); F05D 2250/311 (2013.01); F05D 2260/213 (2013.01); F22B 3/08 (2013.01); Y02T 50/676 (2013.01);
Abstract

A gas turbine engine includes a first shaft coupled to a first turbine and a first compressor, a second shaft coupled to a second turbine and a second compressor, and a third shaft coupled to a third turbine and a fan assembly. The turbine engine includes a heat rejection heat exchanger configured to reject heat from a closed loop system with air passed from the fan assembly, and a combustor positioned to receive compressed air from the second compressor as a core stream. The closed-loop system includes the first, second, and third turbines and the first compressor and receives energy input from the combustor.


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