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Pulse detonation assembly and hybrid engineA pulse detonation (PD) assembly includes a number of PD chambers adapted to expel respective detonation product streams and a number of barriers disposed between respective pairs of PD chambers. The barriers define, at least in part, a number of sectors that contain at least one PD chamber. A hybrid engine includes a number of PD chambers and barriers. The hybrid engine further includes a turbine assembly having at least one turbine stage, being in flow communication with the PD chambers and being configured to be at least partially driven by the detonation product streams. A segmented hybrid engine includes a number of PD chambers and segments configured to receive and direct the detonation product streams from respective PD chambers. The segmented hybrid engine further includes a turbine assembly configured to be at least partially driven by the detonation product streams.
Document ID
20110000809
Acquisition Source
Glenn Research Center
Document Type
Other - Patent
Authors
Rasheed, Adam
Dean, Anthony John
Vandervort, Christian Lee
Date Acquired
August 25, 2013
Publication Date
October 26, 2010
Subject Category
Mechanical Engineering
Report/Patent Number
Patent Application Number: US-Patent-Appl-SN-11/129,686
Patent Number: US-Patent-7,818,956
Funding Number(s)
CONTRACT_GRANT: NAS3-01135
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-Patent-7,818,956
Patent Application
US-Patent-Appl-SN-11/129,686
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