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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F02R 708

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active

057222347

ABSTRACT:
An aircraft ram jet engine for supersonic and/or hypersonic flight, intended to operate over a wide range of speeds, of the type including: (a) an oxidant inlet; (b) at least one fuel injector; (c) a body in which the oxidant and fuel intended to be burned are mixed and the gases resulting from this combustion are channeled; and (d) at least one wall of the body consisting, at least partially, of plates (12) linked together by articulations. The ram jet engine comprises first fluid blowing means (19, 22), mounted in the region of the articulations (13), in order to cool them.

REFERENCES:
patent: 4081137 (1978-03-01), Sutton et al.
patent: 4895378 (1990-01-01), Newquist et al.
patent: 4930309 (1990-06-01), Hartman
patent: 5076590 (1991-12-01), Steinetz et al.
patent: 5165227 (1992-11-01), Grieb
patent: 5214914 (1993-06-01), Billig et al.

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