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:
Oct. 18, 2022

Filed:

Feb. 26, 2018
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Sibtosh Pal, Mason, OH (US);

Steven Clayton Vise, Loveland, OH (US);

Arthur Wesley Johnson, Cincinnati, OH (US);

Clayton Stuart Cooper, Loveland, OH (US);

Joseph Zelina, Waynesville, OH (US);

Assignee:

GENERAL ELECTRIC COMPANY, Schenectady, NY (US);

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
F23R 7/00 (2006.01); F02K 7/08 (2006.01); F02K 7/10 (2006.01); F02K 7/16 (2006.01); F23R 3/18 (2006.01); F23R 3/34 (2006.01);
U.S. Cl.
CPC ...
F23R 7/00 (2013.01); F02K 7/08 (2013.01); F02K 7/10 (2013.01); F02K 7/16 (2013.01); F05D 2220/10 (2013.01); F05D 2250/90 (2013.01); F23R 3/18 (2013.01); F23R 3/34 (2013.01);
Abstract

A Brayton cycle engine and method for operation. The engine includes an inner wall assembly and an upstream wall assembly each extended from a longitudinal wall into a gas flowpath. An actuator adjusts a depth of the detonation combustion region into the gas flowpath between the inner wall assembly and the upstream wall assembly. The engine flows an oxidizer through the gas flowpath and the inner wall captures a portion of the oxidizer. The engine further adjusts the captured flow of oxidizer via the upstream wall and flows a first flow of fuel to the captured flow of oxidizer to produce rotating detonation gases. The engine flows the detonation gases downstream and to mix with the flow of oxidizer, and flows and burns a second flow of fuel to the detonation gases/oxidizer mixture to produce thrust.


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