Aerodynamic heated steam generating apparatus

Aeronautics and astronautics – Aircraft power plants – Auxiliary

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Details

165 42, 165 44, 60 3953, B64D 4100

Patent

active

046051848

ABSTRACT:
An aerodynamic heated steam generating apparatus having an aerodynamic heat immersion coil steam generator adapted to be located on the leading edge of an airframe of a hypersonic aircraft and being responsive to aerodynamic heating of water by a compression shock airstream to produce the steam pressure, expansion shock air-cooled condenser adapted to be located in the airframe rearward of and operatively coupled to the aerodynamic heat immersion coil steam generator to receive and condense the steam pressure, a steam pressure reacting device operatively coupled between the aerodynamic heat immersion coil steam generator and the expansion shock air-cooled condenser for driving a load and an aerodynamic heated steam injector manifold adapted to distribute heated steam into the airstream flowing through an exterior thrust generating channel of an air-breathing, ducted power plant is shown.

REFERENCES:
patent: 3015461 (1962-01-01), Fineblum
patent: 3090212 (1963-05-01), Anderson et al.
patent: 3093348 (1963-06-01), Schelp et al.
patent: 3101588 (1963-08-01), Perry
patent: 3369782 (1968-02-01), Billig et al.
patent: 3929305 (1975-12-01), Sabol
patent: 4273304 (1981-06-01), Frosch et al.

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