Radially staged drag turbine

Rotary kinetic fluid motors or pumps – Smooth runner surface for working fluid frictional contact

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Details

415 66, F01D 136

Patent

active

042015120

ABSTRACT:
The staging or compounding of drag-type turbines having a high energy input is herein accomplished by disposing successive stages of a drag turbine in radially offset relation, i.e., nested relationship with nozzles between radially displaced stages mounted either in fixed spatial position or mounted for rotation with the upstream rotor and providing either like or opposite directions of rotation of successive stages. The successive radial stages of the present invention are separately coupled to coaxial drive shafts which, in turn, may be appropriately coupled to rotary output means in a conventional manner to provide the output power and high efficiency of the multistaged turbine.

REFERENCES:
patent: 1056338 (1913-03-01), Johnsen
patent: 1061142 (1913-05-01), Tesla
patent: 1108831 (1914-08-01), Corthesy
patent: 1179078 (1916-04-01), Dake
patent: 1434336 (1922-10-01), Geiger
patent: 2043788 (1936-06-01), Adair
patent: 3045428 (1962-07-01), McLean
patent: 3487784 (1970-01-01), Kafferty
patent: 3872668 (1975-03-01), Eskeli
patent: 4025225 (1977-05-01), Durant

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