发明名称 Orientation independent ignitron
摘要 Orientation independent ignitron 10 has a cooled cathode 28 which carries thin mercury film 58 which is held in place by surface tension forces so that it is independent of orientation. Ignitor 48 starts conduction which continues until mercury exhaustion or shut off by an external circuit. During nonconductive portions of the duty cycle, the mercury recondenses on the cooled cathode 30.
申请公布号 US4264839(A) 申请公布日期 1981.04.28
申请号 US19790047672 申请日期 1979.06.12
申请人 HUGHES AIRCRAFT COMPANY 发明人 BAYLESS, JOHN R.
分类号 H01J13/06;(IPC1-7):H01J7/24;H01J13/32 主分类号 H01J13/06
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