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Three dimensional PIC simulations of the transparent and eggbeater cathodes in the Michigan relativistic

机译:密歇根相对论中透明和打蛋器阴极的三维PIC模拟

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Summary form only given. A novel relativistic magnetron priming technique consisting of either a main center cathode and several satellite cathodes (eggbeater design) or just the satellite cathodes (transparent cathode design [Fuks and Schamiloglu, 2005]) is investigated using the three-dimensional electromagnetic, particle in cell code ICEPIC. Both these cathode designs rely on RF field penetration into the cathode region to enhance performance. This priming technique is thought to allow for larger amplitudes of the synchronous Ee field in the electron hub region which in turn hastens the capture of electrons into spokes. This technique effectively eliminates mode competition with the Pi mode amplitude dominating the other modes by at least a factor of 25. The A6-3 Michigan magnetron was used for all simulations [Lopez 2002]. For both cathode designs the number, radial placement and orientation of the satellite strips were allowed to vary over several axial magnetic field values so that an optimization with respect to output power and efficiency could be determined at a given magnetic field. Performance optimization was achieved for both cathode configurations at B=3.2 kG with nine satellite cathodes at a radial placement of 1.75 times the main cathode radius. A power output efficiency of 35% and an output power exceeding 550 MW was measured for both designs at optimum parameters. Efficiency and output power decreased as satellite radial placement was increased from optimum. Moreover, it was observed in some cases that satellite cathode orientation (with respect to the slow wave structure) provided an additional ~50 MW of output power. Transparent and eggbeater cathode designs were simulated with 3, 6 and 9 satellite cathodes. It was found that the number of satellite cathodes did affect the magnetron output performance characteristics. For example, unlike the 6 and 9 satellite cathode simulations, the 3 cathode transparent design was robust with respect to cathode- placement. Power efficiencies for satellite cathode radial placements at 1.75, 2.0 and 2.3 times the cathode radius all yielded efficiencies in the 30% range and output powers ~500 MW. Only after satellite cathode radius exceeded 2.3 times the main cathode radius did efficiencies start to drop off significantly for the transparent 3 cathode design
机译:仅提供摘要表格。使用三维电磁粒子在电池中研究了一种新颖的相对论磁控管启动技术,该技术由一个主中心阴极和几个卫星阴极(eggbeater设计)或仅由卫星阴极(透明阴极设计[Fuks and Schamiloglu,2005])组成。代码ICEPIC。这两种阴极设计均依赖于RF场渗透到阴极区域中以增强性能。人们认为,这种启动技术可以使电子集线器区域中的同步Ee场具有更大的振幅,从而又加快了将电子捕获到辐条中的速度。该技术有效地消除了模式竞争,其中Pi模式振幅至少以其他因素占主导地位25倍。密西根州A6-3磁控管用于所有仿真[Lopez 2002]。对于这两种阴极设计,允许卫星条的数量,径向布置和方向在几个轴向磁场值上变化,从而可以在给定磁场下确定关于输出功率和效率的优化。在B = 3.2 kG时,两个阴极配置均实现了性能优化,其中9个卫星阴极的径向位置是主阴极半径的1.75倍。在最佳参数下,两种设计的功率输出效率均为35%,输出功率超过550 MW。效率和输出功率随着卫星径向布局从最佳状态的增加而降低。此外,在某些情况下,观察到卫星阴极方向(相对于慢波结构)提供了额外的〜50 MW输出功率。用3个,6个和9个卫星阴极模拟了透明和打蛋器阴极的设计。发现卫星阴极的数量确实影响了磁控管的输出性能特性。例如,与6和9卫星阴极模拟不同,3阴极透明设计在阴极放置方面很坚固。卫星阴极径向布置的功率效率分别为阴极半径的1.75、2.0和2.3倍,效率均在30%范围内,输出功率约为500 MW。仅当卫星阴极半径超过主阴极半径的2.3倍之后,透明3阴极设计的效率才开始显着下降

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