Power plants – Reaction motor – Method of operation
Patent
1994-06-24
1995-12-12
Casaregola, Louis J.
Power plants
Reaction motor
Method of operation
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.
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T. Bussing and G. Pappas, "An Introduction to Pulse Detonation Engines," 32nd Aerospace Sciences Meeting & Exhibit, Jan. 10-13, 1994 (14 pages).
Hunter, Jr. Louis G.
Winfree Don D.
Bradley James E.
Casaregola Louis J.
Lockheed Corporation
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