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. 01, 2022

Filed:

Feb. 25, 2019
Applicant:

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

Inventor:

Robert T. Duge, Carmel, IN (US);

Assignee:

ROLLS-ROYCE CORPORATION, Indianapolis, IN (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 7/12 (2006.01); F02C 7/18 (2006.01); F02C 6/16 (2006.01); F02K 3/02 (2006.01); F02K 7/14 (2006.01); F02K 7/16 (2006.01); F01D 25/14 (2006.01); F01D 25/26 (2006.01);
U.S. Cl.
CPC ...
F02C 7/125 (2013.01); F02C 6/16 (2013.01); F02C 7/18 (2013.01); F02K 3/025 (2013.01); F02K 7/14 (2013.01); F01D 25/145 (2013.01); F01D 25/26 (2013.01); F02K 7/16 (2013.01);
Abstract

A hybrid propulsion system is provided. The system may comprise a gas turbine engine and a secondary engine, an inlet, an exhaust, a pressurized tank, and an expansion valve. The inlet may be in fluid communication with the ambient environment. The gas turbine engine may have a core passage including a compressor, a combustion chamber, and a turbine. The core passage may be in selective fluid communication with the inlet. The exhaust may be in fluid communication with the ambient environment and the core passage. The pressurized tank may be located upstream of the core passage. The pressurized tank may contain a cooling fluid. The expansion valve may be in fluid communication with the pressurized tank and the core passage. The pressurized tank may provide cooling fluid to the core passage to cool the gas turbine engine during operation of the secondary engine.


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