发明名称 Combustion chambers operating on a supersonic stream chiefly for jet engines
摘要 A method for producing a permanent combustion under detonating or substantially detonating conditions within a stream flowing at supersonic speed, consisting in subdividing a stream of combustion-sustaining fluid into two parallel streams, modifying the speed of at least one of said streams, causing said streams flowing at different speeds to meet again inside an area wherein a diabolo-shaped system of shock waves is formed and injecting fuel into the stream flowing at the higher speed, the combustion starting on the downstream side of a flat surface extending perpendicularly to the direction of flow and forming the surface of minimum cross-sectional area of the diabolo-shaped system.
申请公布号 US4214442(A) 申请公布日期 1980.07.29
申请号 US19680752451 申请日期 1968.08.08
申请人 NAT ETUDE CONSTRUCTION MOTEURS AVIAT 发明人 REINGOLD, LUCIEN
分类号 F02K7/10;(IPC1-7):F02K7/10 主分类号 F02K7/10
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