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NASA NTRS · 20110000809

Pulse detonation assembly and hybrid engine

Abstract

A 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.

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BibTeXRIS

Rasheed, Adam, Dean, Anthony John, Vandervort, Christian Lee. 2010-10-26. Pulse detonation assembly and hybrid engine. https://ntrs.nasa.gov/citations/20110000809

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