COMBINED CYCLE SYSTEM INTERACTING COMBUSTION CHAMBER AND NOZZLE Russian patent published in 2011 - IPC F02K7/08 

Abstract RU 2413859 C2

FIELD: engines and pumps.

SUBSTANCE: combined-cycle engine comprises starting booster made up of turbojet engine, double-duty ramjet (DDRJ), and feed line. Double-duty ramjet has assemblage of pylons supporting primary low-thrust ejector engines attached to rear edge of said pylons. Said feed line communicated aforesaid starting booster with dual-duty ramjet son that to allow feeding turbo compressor exhaust air to aforesaid primary ejector engines. Starting booster and double-duty ramjet are integrated to generate thrust varying from 0 to over 4 Mach.

EFFECT: increased thrust.

19 cl, 5 dwg

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RU 2 413 859 C2

Authors

Bulmehn Melvin Dzh.

Dates

2011-03-10Published

2007-12-12Filed