Variable diffuser element

Rotary kinetic fluid motors or pumps – Runner or blade selectively adjustable relative to casing – Axially adjusted

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415157, F04D 2928

Patent

active

047267330

ABSTRACT:
A moveable, ovoid body for incorporation in and with the conventional elements of a turbo jet and possessing compressor and diffuser shape characteristics that are found in turbo jet machines. The invention is designed to take the place of conventional diffusers which are employed in both compressor and turbine stages of turbojets. When used with the hydrovapor engine, developed by the inventor, the moveable diffuser shell which operates in conjunction with impeller and turbine propeller blades offers a wide range of selectable operational parameters such as inlet flow velocity, compression chamber pressure and exhaust velocity.

REFERENCES:
patent: 2693677 (1954-11-01), Stalker
patent: 2792983 (1957-05-01), Stalker
patent: 2986218 (1961-05-01), Wagner et al.
patent: 3561883 (1971-02-01), Berry
patent: 4070132 (1978-01-01), Lynch
patent: 4375939 (1983-03-01), Mount et al.

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