Pulse detonation engine

Power plants – Reaction motor – Method of operation

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60247, 60 3978, 431 1, F02K 706

Patent

active

054738857

ABSTRACT:
A pulse detonation engine has a detonation chamber with a sidewall. At least two fuel ports are located in the sidewall, spaced longitudinally apart from each other. An oxygen fuel mixture is introduced into the forward port and detonated. This creates a detonation wave which propagates with an air fuel mixture introduced into the rearward fuel port. After the detonation, purge air passes through the chamber before the next detonation. A rotating sleeve valve mounted around the detonation opens and closes the fuel ports as well the purge ports.

REFERENCES:
patent: 2518002 (1950-08-01), Goddard
patent: 2930196 (1960-03-01), Hertzberg
patent: 3473879 (1969-10-01), Berberich
patent: 3634778 (1972-01-01), Melikian et al.
patent: 3812783 (1974-05-01), Yang et al.
patent: 4741154 (1988-05-01), Eidelman
patent: 4870903 (1989-10-01), Carel et al.
patent: 5280705 (1994-01-01), Epstein et al.
patent: 5345758 (1994-09-01), Bussing
T. Bussing and G. Pappas, "An Introduction to Pulse Detonation Engines," 32nd Aerospace Sciences Meeting & Exhibit, Jan. 10-13, 1994 (14 pages).

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