Gas turbine engines

Rotary kinetic fluid motors or pumps – Means – disposition or arrangement for causing supersonic...

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415208, F01D 102

Patent

active

041992962

ABSTRACT:
A supersonic compressor having an annular array of passages in which each passage comprises a throat portion and a divergent portion downstream of the throat. The passages are bounded by radially inner and outer walls one of which extends further upstream than the other and defines an intake to each passage in the shape of a supersonic compression ramp. The intakes and passages are separated from each other by circumferentially extending side walls.

REFERENCES:
patent: 2631425 (1953-03-01), Nordfurs
patent: 2683962 (1954-07-01), Griffith
patent: 2735612 (1956-02-01), Hausammann
patent: 2839239 (1958-06-01), Stalker
patent: 2918254 (1959-12-01), Hausammann
patent: 2925231 (1960-02-01), Pfaff et al.
patent: 3059834 (1962-10-01), Hausammann
patent: 3080707 (1963-03-01), Vetter
patent: 3128973 (1964-04-01), Dannenberg
patent: 3156407 (1964-11-01), Bourquard
patent: 3363421 (1968-01-01), Ferri
patent: 3422625 (1969-01-01), Harris
patent: 3439692 (1969-04-01), Pike
patent: 3837760 (1974-09-01), Stalker

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