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An electron source with a multiaperture plasma emitter and beam extraction into the atmosphere

机译:具有多孔径等离子体发射器的电子源,并将电子束提取到大气中

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The results of investigating the emission properties of a multiaperture plasma emitter with grid stabilization of the emission-plasma boundary in an electron source with ejection of a generated electron beam from the accelerating gap into the atmosphere through a thin foil. A stainless-steel foil mask with 344 circular holes is laid on an emission grid with dimensions of 750 x 150 mm. The holes form a discrete emission structure of the plasma emitter, from which electrons are emitted under the action of an accelerating voltage. The alignment of the holes in the mask of the emission structure and in the bearing grid of the output foil window, which has the same number of holes with a larger diameter, and the attainment of a coaxial plane-parallel geometry of the accelerating gap allows minimization of the beam loss in the bearing grid of the output foil window. An electron beam is a superposition of elementary beams that are formed by individual emission structures, whose plasma boundaries are stabilized with a fine-structure metal grid. The coefficient of the current extraction into the atmosphere reached 75% of the emission current. In experiments at an accelerating voltage of 200 kV, an emission current of 16 A, and a pulse duration (FWHM) of 40 mu s, a beam with an average power of similar to 4 kW was ejected into the atmosphere. This value is more than 60% of the beam power in the accelerating gap at a geometrical transparency of the bearing grid of the output foil window of 56%. A further increase in the power was limited by the power of the high-voltage power-supply unit.
机译:研究多孔径等离子发射器的发射特性的结果,该电子发射器在电子源中具有发射等离子体边界,并通过薄箔将电子束从加速间隙喷射到大气中,从而稳定了栅极。将具有344个圆形孔的不锈钢箔掩膜放在尺寸为750 x 150 mm的发射栅格上。这些孔形成等离子体发射器的离散发射结构,在加速电压的作用下,电子从该发射结构发射出去。发射结构的掩模中的孔和输出箔窗口的轴承网格中的孔对齐,该孔具有相同数量的直径较大的孔,并且加速间隙的同轴平面平行几何形状的实现允许使输出箔窗口的轴承网格中的光束损失最小化。电子束是由各个发射结构形成的基本束的叠加,其等离子体边界通过精细结构的金属栅格得以稳定。提取到大气中的电流系数达到了发射电流的75%。在加速电压为200 kV,发射电流为16 A,脉冲持续时间(FWHM)为40μs的实验中,平均功率类似于4 kW的光束被发射到大气中。在输出箔片窗口的支承栅格的几何透明度为56%时,该值大于加速间隙中光束功率的60%。功率的进一步增加受到高压电源单元的功率的限制。

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