Heat-recovering-thrust-turbine having rotational flow path

Details Heat-recovering-thrust-turbine having rotational flow path Heat-recovering-thrust-turbine having rotational flow path

1992-04-22

1993-09-07

Casaregola, Louis J.

Power plants

Combustion products used as motive fluid

With dual function turbine

60 39511, 60 3975, 415 79, F02C 3045, F02C 710

Patent

active

052418154

ABSTRACT:
A heat-recovering-thrust-turbine including the rotational flow path has been invented in present work. This thrust turbine consists of a rotating disc having unique shape and functions of compressor and turbine together, a combustion chamber, manifolds for heat recovering and a divergent nozzle having the curved flow path in a different way of conventional gas turbine engines utilizing a straight discharging mechanism of the exhaust gases.
Thus, this invented thrust turbine is able to perform the combined function such as compression of air, cooling of the hot section, recovery of the wasted heats and generation of the thrust and the turbine power being used for the air compression, simultaneously.

REFERENCES:
patent: 2589239 (1952-03-01), Fallon
patent: 2611241 (1952-09-01), Schultz
patent: 3269120 (1966-08-01), Sabatiuk
patent: 3635577 (1972-01-01), Dee

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