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Partial Discharges of High Frequency Transformer for Space Application in Near Vacuum

机译:接近真空的空间应用高频变压器的局部放电

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This paper presents partial discharge measurements and a model-based investigation for corona activity on a prototype of a high frequency transformer from Flux A/S, designed to operate on a space travelling vessel. Previous iterations of the prototypes failed external partial discharge tests, and the environment that the transformer was designed to be installed and tested in, was suspected to cause the partial discharge to onset. In normal operation on the space vessel (and during the required design-tests), the transformer has its terminals exposed to the surrounding atmosphere, whose pressure varies from standard atmospheric pressure to near vacuum conditions during the launch of the space vessel. The most critical condition for external partial dielectric breakdown will be encountered under its intended operation, similar to the knee point in the Paschen curve. The conditions at this point yields the largest stresses on the dielectric, in this case the surrounding atmosphere of the transformer. A predictive method for evaluation of corona activity onset is therefore included. This is done based on calculation of the effective ionization coefficient along the critical electrical field line, α obtained by Finite Element Method (FEM) models and is evaluated for a given set of pressure values to emulate the intended operating conditions of the transformer, a itself is a function of the electrical field strength along the critical line, as well as the relative air density. The FEM models of the transformer were therefore designed to calculate the electrical field strength distribution around the transformer, and to locate the critical field line. It was found that 2D models yielded a satisfactory accuracy for the intention of the simulation, and that 3D models would only yield a slightly improved accuracy for a substantially increased computational burden. For the partial discharge measurements, the test voltage was 1 kV at 50 Hz, and the geometry of the transformer and distances to objects in proximity to the transformer will remain constant, leading to the electrical field strength distribution also being constant. The only varying parameter which is affecting a is the variation of the atmospheric pressure. The corona activity onset condition is evaluated by evaluating the integral value of α over its region that yields a net positive ionization and compare this value with the criteria for the Townsend mechanism. The simulated pressure range includes only values that are realizable with the available equipment in the HV-laboratory of Aalborg University, which is 1.0 to 0.2 bars of absolute pressure. This is done with the intention to compare the predictive method for corona onset with actual partial discharge measurements. The PD measurements showed that no external partial discharge activity was present for the given experimental conditions and pressure range, and the new design of the transformer prototype was therefore improved.
机译:本文介绍了部分流量测量和基于模型的Flux A / S高频变压器原型的电晕活动研究,该原型设计用于在太空旅行船上运行。原型的先前迭代未通过外部局部放电测试,并且怀疑是设计要在其中安装和测试变压器的环境导致局部放电开始。在航天器的正常运行中(以及在进行所需的设计测试期间),变压器的端子暴露于周围的大气中,在航天器发射期间,其压力会从标准大气压变化到接近真空的状态。外部部分介质击穿的最关键条件将在其预期操作下遇到,类似于Paschen曲线中的拐点。此时的条件会在电介质(在这种情况下为变压器的周围环境)上产生最大的应力。因此,包括用于评估电晕活性开始的预测方法。这是基于沿临界电场线的有效电离系数的计算完成的,α是通过有限元方法(FEM)模型获得的,并针对给定的一组压力值进行了评估,以模拟变压器本身的预期工作条件是沿临界线的电场强度以及相对空气密度的函数。因此,设计了变压器的FEM模型,以计算变压器周围的电场强度分布,并确定临界场线。已经发现,出于仿真目的,2D模型产生了令人满意的精度,而3D模型将仅由于稍微增加的计算负担而产生了稍微提高的精度。对于局部放电测量,测试电压为50 Hz时的1 kV,变压器的几何形状以及与变压器附近物体的距离将保持恒定,从而导致电场强度分布也恒定。影响a的唯一变化参数是大气压力的变化。通过评估在产生纯正电离的区域中α的积分值,并将该值与Townsend机理的标准进行比较,可以评估电晕活性开始条件。模拟压力范围仅包含可以使用奥尔堡大学高压实验室的可用设备实现的值,绝对压力为1.0至0.2 bar。这样做是为了将电晕发作的预测方法与实际的局部放电测量值进行比较。 PD测量表明,在给定的实验条件和压力范围内,没有外部局部放电活动,因此改进了变压器原型的新设计。

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