Short-Circuit Ruggedness and Partial Discharge Evaluation of a 3.3 kV SiC MOSFET Power Module

Ke Wang, Yizhou Cong, Pengyu Fu, Xiao Li, Qianyi Cheng, Boxue Hu, Jin Wang, Ashish Kumar, K. Olejniczak, Daniel Pelletier, Z. Cole, A. Deshpande, Amit Goyal
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Abstract

This paper presents the initial evaluation of a 3.3-kV, SiC MOSFET power module (not fully populated) from Wolfspeed, including static, short circuit (SC), and partial discharge (PD) test results. Static characterization results are presented first. The module performance change after repetitive pulse SC tests is provided by comparing the original static characterization test results to the one performed after the SC stress tests. More electric aircrafts (MEA) require an increased electric system voltage level (e.g., 230 VAC constant or variable frequency, ± 270 VDC or 540 VDC) and make PD a very relevant and urgent issue. Thus, PD evaluation tests for the module package are included for different air pressures from Sea Level (i.e., 760 Torr) to 50,000 feet (i.e., 87 Torr) altitude. The PD inception voltage (PDIV) and extinction voltage (PDEV) obtained via experimentation are presented in this paper.
3.3 kV SiC MOSFET功率模块的短路耐用性和局部放电评估
本文介绍了Wolfspeed公司的3.3 kv SiC MOSFET功率模块(未完全填充)的初步评估,包括静态,短路(SC)和局部放电(PD)测试结果。首先给出静态表征结果。通过将原始静态特性测试结果与SC应力测试结果进行比较,可以得出重复脉冲SC测试后的模块性能变化情况。更多的电动飞机(MEA)需要更高的电气系统电压水平(例如,230 VAC恒定或变频,±270 VDC或540 VDC),并使PD成为一个非常相关和紧迫的问题。因此,模块包的PD评估测试包括从海平面(即760托尔)到50,000英尺(即87托尔)高度的不同气压。本文给出了实验得到的放电起始电压(PDIV)和消光电压(PDEV)。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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