发明名称 Circular beam deflection in gyrocons
摘要 A gyrocon deflection system can provide circular beam deflection using a single RF coupler, without providing a phase difference between the two beam deflection signals to account for electron beam transit time between the two sets of deflection plates. The two sets of deflection plates are internally connected pairwise together so that both deflection regions are in RF phase, and the midplanes of the two sets are spaced 90 DEG apart electrically at the desired operating voltage and frequency.
申请公布号 US4445071(A) 申请公布日期 1984.04.24
申请号 US19820372520 申请日期 1982.04.28
申请人 HUGHES AIRCRAFT COMPANY 发明人 WESSEL-BERG, TORE;TAMMARU, IVO
分类号 H01J25/78;(IPC1-7):H01J25/00 主分类号 H01J25/78
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