Orientation independent ignitron with grooved cathode
AssigneeHughes Aircraft Company
InventorsWilfried O. Eckhardt, Hayden E. Gallagher, Roland G. Fleig
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AssigneeHughes Aircraft Company
InventorsWilfried O. Eckhardt, Hayden E. Gallagher, Roland G. Fleig
Estimating the term…
An orientation independent ignitron (OII) has an anode, a cathode with a plurality of spaced grooves facing the anode, and a cooling mechanism which causes liquid metal vapor to condense as a film which is retained on the grooved cathode surface by surface tension and forms reservoirs within the grooves. The cathode and anode are preferably cylindrical and coaxial, with the inner surface of the cathode having parallel annular grooves facing the outer anode surface. Igniters are preferably introduced into convex areas between adjacent grooves along radial lines, with individual igniters providing ignition for a pair of adjacent grooves. The igniters can be operated simultaneously or in sequence, depending upon the desired repetition rate and current capacity. A liquid metal film is initially formed by placing the OII on its side, introducing liquid metal into the lower ends of the grooves, and causing arcing between the anode and liquid metal to flow the liquid metal and wet the adjacent groove surface. Some of the liquid metal also evaporates and re-condenses on other portions of the cathode, establishing a continuous film.
An orientation independent ignitron, comprising:
An orientation independent ignitron, comprising:
An orientation independent ignitron, comprising:
A method of wetting the inner surface of a generally cylindrical orientation independent ignitron cathode with a liquid metal film, said inner cathode surface having a plurality of generally annular grooves facing and spaced from an anode which is interior to the cathode, comprising:
An orientation independent ignitron, comprising:
Dependencies are inferred from the claim text.