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. 18, 2025

Filed:

Apr. 12, 2022
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Arin Elspeth Lastufka Cross, Waterford, NY (US);

Krishnakumar Venkatesan, Clifton Park, NY (US);

Assignee:

GENERAL ELECTRIC COMPANY, Evendale, OH (US);

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
F02K 7/16 (2006.01); F02C 6/00 (2006.01); F02C 6/08 (2006.01); F02C 7/042 (2006.01); F02C 7/057 (2006.01); F02C 7/18 (2006.01); F02K 1/06 (2006.01); F02K 7/14 (2006.01); F02K 7/20 (2006.01); F23R 7/00 (2006.01);
U.S. Cl.
CPC ...
F02K 7/16 (2013.01); F02C 6/00 (2013.01); F02C 6/08 (2013.01); F02C 7/042 (2013.01); F02C 7/057 (2013.01); F02C 7/18 (2013.01); F02K 1/06 (2013.01); F02K 7/14 (2013.01); F02K 7/20 (2013.01); F23R 7/00 (2013.01); F05D 2220/323 (2013.01); F05D 2220/80 (2013.01); F05D 2240/35 (2013.01);
Abstract

A combined cycle propulsion system for a flight vehicle includes a compressor-fed combustion engine, and a multi-mode supersonic engine. The multi-mode supersonic engine includes an adjustable inlet section, a combustion section arranged downstream of the adjustable inlet section and including a first combustor portion having at least one rotating detonation combustor and a second combustor portion having a supersonic combustion type combustor, and an adjustable exhaust nozzle section arranged downstream of the combustion section. The at least one rotating detonation combustor functions as a pilot for the supersonic combustion type combustor.


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