Cooling system for ramjet engine

Details Cooling system for ramjet engine Cooling system for ramjet engine

1979-11-05

1981-06-30

Capossela, Ronald C.

Aeronautics and astronautics

Aircraft power plants

60 3918C, 60266, 60728, 62 5, 62239, 62241, 137 151, 244117A, B64D 3302

Patent

active

042758572

ABSTRACT:
A ramjet powered vehicle having a bleed slot in the subsonic diffuser, for the ramjet combustor, which supplies air to a turbine for supplying power to vehicle accessories. A vortex tube is provided between the bleed slot and the turbine to provide a cool air supply. Radar absorbing material is positioned adjacent ramjet inlet with a cooling duct provided to supply cooling air from the vortex tube to the ramjet inlet cowl lip to provide cooling for the radar absorbing material.

REFERENCES:
patent: 1952281 (1934-03-01), Ranque
patent: 2644315 (1953-07-01), Jamieson
patent: 2669101 (1954-02-01), Shields
patent: 2786341 (1957-03-01), Green
patent: 2839900 (1958-06-01), Green
patent: 2839901 (1958-06-01), Green
patent: 2858698 (1958-11-01), Hickey
patent: 2873582 (1959-02-01), Green
patent: 2893204 (1959-07-01), Anderson et al.
patent: 3090208 (1963-05-01), Munakata
patent: 3361336 (1968-01-01), Foa
patent: 3461676 (1969-08-01), Toelke et al.
patent: 3703146 (1972-11-01), Kovats
patent: 3973396 (1976-08-01), Kronogard

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