Apparatus for producing a discharge in a supersonic gas flow

Electric lamp and discharge devices: systems – Combined load device or load device temperature modifying... – Distributed parameter resonator-type magnetron

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31511131, 31511151, 372 64, 372 72, H01J 746, H01J 1980

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active

044144881

ABSTRACT:
Disclosure is directed to an apparatus for producing a microwave discharge n a supersonic gas flow such that the available microwave energy is deposited in the gas as completely and uniformly as possible through a substantial cross-section of the flow channel. The flow channel is provided within a waveguide and microwave energy is caused to be propagated through the waveguide substantially in the direction of the gas flow. A supersonic nozzle is provided in the channel dividing the channel into an upstream plenum and a downstream low pressure region, and the electric discharge occurs in the low pressure region just beyond the nozzle throat.

REFERENCES:
patent: 2762872 (1956-09-01), Dicke
patent: 3083528 (1963-04-01), Brown
patent: 3280364 (1966-10-01), Sugawara et al.
patent: 3313979 (1967-04-01), Landauer
patent: 3418206 (1968-12-01), Hall et al.
patent: 3541372 (1970-11-01), Omura et al.
patent: 3641389 (1972-02-01), Leidigh
patent: 3872349 (1975-03-01), Spero et al.
patent: 3911318 (1975-10-01), Spero et al.
patent: 4004249 (1977-01-01), Kikuchi
patent: 4200819 (1980-04-01), Haslund

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