Pulse detonation engine

作者: Louis G. Hunter , Don D. Winfree

DOI:

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

参考文章(10)
Hertzberg Abraham, Jr Joseph G Logan, Valved intermittent combustion reaction engine ,(1951)
Bertold Berberich, Shock wave burner ,(1968)
Michael J. Epstein, Paul H. Kutschenreuter, Fuel injection system for scramjet engines ,(1992)
L Yang, V Menichelli, Optically detonated explosive device ,(1972)
Shmuel Eidelman, Rotary detonation engine ,(1982)
Frank R Biancardi, Gorkcr Melikian, Closed-cycle gas laser system ,(1969)
T. Bussing, G. Pappas, An introduction to pulse detonation engines 32nd Aerospace Sciences Meeting and Exhibit. ,(1994) , 10.2514/6.1994-263