热核聚变用2mw 170 GHZ连续波同轴回旋管硬激励机制的一些特点

V. Shcherbinin, G. Zaginaylov
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引用次数: 0

摘要

同轴腔回旋管是目前非常有前途的毫米波辐射源,可以成功地用于热核融合和其他一些应用。同轴腔回旋管工业样机的研制正在进行中。模式竞争是影响回旋管性能提高的主要障碍之一,这种竞争是由于毫瓦级回旋管的模式频谱密度大而产生的。通常在达到所需模式下效率最高的工作点之前,加速电压从零值(启动场景)随时间增加。在启动过程中,可以激发不同的腔模式。在最后的实验中,运行的TE34,19模式在很大的加速电压范围内(67 - 90kV)被稳定地激发,并在激励区域的上界附近(~ 90kV)达到了1.8 MW的最大输出功率[1]。在较高电压下,工作模式的激励效率急剧下降,维持了多波产生状态。然而,在我们的代码[2]和代码SELFT[3]进行的数值模拟中,激励区域明显更宽(根据我们的结果,直至加速电压~ 97 kV)。预计最大输出功率可达到~ 2.5 MW。实验测量结果与模拟结果之间的差异归因于模式竞争,然而,将几个最危险的竞争模式纳入模拟并没有导致更一致的结果。在[4]中提出了一种可操作回旋管模式振荡范围减小的可能机制。根据[4],对工作模式(TE34、18、TE34、20)的径向卫星的激励可以使TE34、19模式的振荡区域上界发生移位,从而降低其功率。然而,我们的代码进行的模拟并没有证实[4]中得到的结果。此外,我们还可以提出实验中观察到的输出功率降低的另一种机制。
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Some peculiarities of hard excitation regime in 2 MW 170 GHZ CW coaxial gyrotron for iter
Nowadays coaxial cavity gyrotrons are very promising sources of millimeter wave radiation which can be successfully used in thermonuclear fusion and some other applications. Development of industrial prototype of coaxial cavity gyrotron is in progress. One of the main obstacles in the enhancement of gyrotron performances is mode competition, which appears due to high density of mode spectrum in MW-class gyrotrons. Usually before reaching the operational point with maximal efficiency in the desired mode the accelerating voltage increases in time from zero value (start-up scenario). During start-up different cavity modes can be excited. In the last experiments the operational TE34,19 mode was excited stably over a wide range of the accelerating voltage (67 – 90kV) and has achieved the maximal output power of 1.8 MW near the upper boundary of the excitation region (∼90kV) [1]. At the higher voltage the efficiency of excitation for the operational mode sharply dropped and the multi-wave generation regime was sustained. However, in numerical simulations performed by our code [2] and the code SELFT [3] the excitation region is notably wider (up to the accelerating voltage ∼ 97 kV according to our results). The predicted maximal output power can achieve ∼ 2.5 MW. The discrepancy between experimental measurements and simulation results were attributed to the mode competition, however including several of the most dangerous competing modes into simulation did not lead to the more consistent results. One of the possible mechanisms of the oscillation range decreasing for the operational gyrotron mode was proposed in [4]. According to [4] excitation of the radial satellites of the operational mode (TE34,18, TE34,20) can shift the upper boundary of oscillation region for the TE34,19 mode and thereby reduces its power. However simulations performed by our code did not confirmed the results obtained in [4]. Moreover, we can propose another mechanism of the reduced output power observed in the experiments.
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