Power plants – Internal combustion engine with treatment or handling of... – Material from exhaust structure fed to engine intake
Patent
1996-06-27
1998-03-17
Freay, Charles G.
Power plants
Internal combustion engine with treatment or handling of...
Material from exhaust structure fed to engine intake
60271, 23926519, 244 74, F02K 710, F02K 708
Patent
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
Avrachkov Valery
Bouchez Marc
Chevalier Alain
Davidenko Dimitri
Levine Vadim
Aerospatiale - Societe Nationale Industrielle
Freay Charles G.
Kim Ted
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