Aircraft ram jet engine for supersonic and/or hypersonic flight

Power plants – Internal combustion engine with treatment or handling of... – Material from exhaust structure fed to engine intake

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60271, 23926519, 244 74, F02K 710, F02K 708

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active

057273820

ABSTRACT:
The present invention relates to an aircraft ram jet engine for supersonic and/or hypersonic flight, intended to operate over a wide range of speeds.
According to the invention, the ram jet engine comprises a ram jet engine body (5) including a combustion cheer portion (6) and a jet pipe portion (7), and, in the vicinity of the transition region (8) between the combustion chamber (6) and the jet pipe (7), having a changing geometry passing progressively from a convergent then divergent longitudinal section, for speeds corresponding to a low Mach number, to an at least substantially constant then divergent longitudinal section for speeds corresponding to a high Mach number.

REFERENCES:
patent: 3279194 (1966-10-01), Chapman
patent: 5072581 (1991-12-01), Harshman
patent: 5226455 (1993-07-01), duPont

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