External Partial Discharge Analysis in Design Process of Electrical Space Components

Martin T. Arentsen, C. Bak, F. D. da Silva, S. Lorenzen
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Abstract

External Partial discharges (PDs) can occur in strong non-uniform electrical fields on electrical equipment. Usually, PDs are only considered in the design process of high voltage applications, where ionization is more likely to occur. Under certain ambient conditions, i.e. under low gaseous pressures, the dielectric strength of an insulation might be weakened, leading to onset of partial discharges - even at voltages below 1 kV. PDs are responsible of insulation deterioration, due to bombardment of ions formed by PDs, as well as chemical reactions by compounds formed during discharge process. Additionally, PDs can cause interference in communication systems. Therefore, PDs are also highly unwanted on electronics for space applications, where reliability is utmost important. The European Cooperation for Space Standardization issued a design handbook for electronics for space applications, in which PD magnitude limits are given. It discards the importance of external PDs, since it argues that no atmosphere will be present in outer space. While that is true, equipment that is under operation during launch of the space vessel, will experience a pressure drop from standard atmospheric pressure to near vacuum. Given a corona onset, an enhancement of the field in the vicinity of the cathode might occur, due to the relative low mobility of the formed positive ions, thereby transitioning the corona into a self-sustained PD. This paper therefore presents both predictive analytical tools for external PDs, applicable in the design process of equipment, as well as an experimental measurement setup to measure PDs in compliance with IEC 60270. Flux A/S design and manufacture magnetic components for space applications. They were unable to analyze a prototype design for PDs before manufacturing, and unable to measure PDs on manufactured prototypes. Collaboration was established between Flux A/S and Aalborg University to enable Flux to do so.
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电气空间元件设计过程中的外局部放电分析
在非均匀强电场条件下,电气设备会发生局部放电。通常,pd只在高压应用的设计过程中考虑,在高压应用中电离更容易发生。在某些环境条件下,即在低气体压力下,绝缘材料的介电强度可能会减弱,甚至在低于1kv的电压下也会导致局部放电。由于钯形成的离子轰击以及放电过程中形成的化合物的化学反应,钯会导致绝缘恶化。此外,pd会对通信系统造成干扰。因此,在可靠性至关重要的空间应用电子设备上,pd也是非常不需要的。欧洲空间标准化合作组织发布了一份空间应用电子设计手册,其中给出了PD量级限制。它抛弃了外部pd的重要性,因为它认为外层空间不存在大气。虽然这是事实,但在宇宙飞船发射期间运行的设备将经历从标准大气压降至接近真空的压力。当电晕开始时,由于形成的正离子的迁移率相对较低,阴极附近的电场可能会增强,从而将电晕转变为自我维持的PD。因此,本文提出了适用于设备设计过程的外部pd的预测分析工具,以及符合IEC 60270的测量pd的实验测量装置。Flux A/S为空间应用设计和制造磁性元件。他们无法在制造前分析pd的原型设计,也无法在制造的原型上测量pd。Flux A/S和奥尔堡大学之间建立了合作,使Flux能够做到这一点。
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