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.
Patent No.:
Date of Patent:
Feb. 13, 2024
Filed:
Aug. 03, 2021
Applicant:
General Electric Company, Schenectady, NY (US);
Inventors:
Nicholas William Rathay, Rock City Falls, NY (US);
Narendra Digamber Joshi, Schenectady, NY (US);
Venkat Eswarlu Tangirala, Niskayuna, NY (US);
Assignee:
GENERAL ELECTRIC COMPANY, Schenectady, NY (US);
Primary Examiner:
Int. Cl.
CPC ...
F23R 7/00 (2006.01); B64C 23/04 (2006.01); F02C 5/02 (2006.01); B64D 27/02 (2006.01); B64C 3/32 (2006.01); B64C 9/38 (2006.01);
U.S. Cl.
CPC ...
F23R 7/00 (2013.01); B64C 3/32 (2013.01); B64C 23/04 (2013.01); B64D 27/02 (2013.01); F02C 5/02 (2013.01); B64C 9/38 (2013.01);
Abstract
A propulsion system includes at least one rotating detonation actuator comprising: a flow path extending from an inlet end to an outlet end; an inner wall defining a radially inner boundary of the flow path; an outer wall defining a radially outer boundary of the flow path; and at least one aircraft wing. The rotating detonation actuator is disposed in the aircraft wing. At least one rotating detonation wave travels through the flow path from the inlet end to the outlet end.