Invention Application
- Patent Title: TURBINE ENGINE ASSEMBLY INCLUDING A ROTATING DETONATION COMBUSTOR
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Application No.: US15390024Application Date: 2016-12-23
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Publication No.: US20180179950A1Publication Date: 2018-06-28
- Inventor: Andrew Maxwell Peter , Peter Daniel Silkowski , Thomas Michael Lavertu , Venkat Eswarlu Tangirala , Douglas Carl Hofer
- Applicant: General Electric Company
- Main IPC: F02C3/16
- IPC: F02C3/16 ; F02C5/02 ; F23R3/58

Abstract:
A turbine engine assembly including a plurality of rotating detonation combustors configured for a rotating detonation process to occur to produce a flow of combustion gas. The plurality of rotating detonation combustors are oriented such that the flow of combustion gas discharged therefrom flows helically relative to a centerline of the turbine engine assembly. The assembly also includes a turbine coupled downstream from the plurality of rotating detonation combustors. The turbine is configured to receive the flow of combustion gas.
Information query
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