Combined air-hydrogen turbo-rocket power plant

Details Combined air-hydrogen turbo-rocket power plant Combined air-hydrogen turbo-rocket power plant

1989-03-13

1991-05-07

Casaregola, Louis J.

Power plants

Reaction motor

Turborocket

60267, 60268, 602701, 415110, 4151736, 4151737, F02M 6700, F02M 208, F01D 520

Patent

active

050126407

ABSTRACT:
A combined air-hydrogen turbo-rocket engine is disclosed having a simplified construction in which the hydrogen driven turbine is formed integrally with the rotor wheel of the axial air compressor stages. The rotor stages are located downstream of a stator vane structure and are driven by gaseous hydrogen passing across the turbine blades. The hydrogen is subsequently injected into an air duct surrounding the axial air compressor and defining an airflow path having an air inlet. The hydrogen-air mixture is ignited and the burned gases are expanded through a converging-diverging exhaust nozzle.

REFERENCES:
patent: 2883828 (1959-04-01), Howell
patent: 2941790 (1960-06-01), Compton et al.
patent: 2994785 (1961-08-01), Mespoulhes
patent: 3002340 (1961-10-01), Landerman
patent: 3145532 (1964-08-01), Moss
patent: 3237401 (1966-03-01), Peters et al.
patent: 3241310 (1966-03-01), Hoadley
patent: 3241311 (1966-03-01), Kuhrt
patent: 3253406 (1966-05-01), Grieb
patent: 3279192 (1966-10-01), Hull, Jr. et al.
patent: 3355890 (1967-12-01), Kappus
patent: 3705496 (1972-12-01), Wolf et al.

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