Advanced Partial Discharge Testing of 540V Aeronautic Motors Fed by SiC Inverter under Altitude Conditions

The present paper reports non-electrically intrusive partial discharge investigations on an aeronautic motor fed by SiC inverter drive under variable environmental conditions. A representative test procedure and experimental set-up based on operating aeronautic conditions are essential to ensure the accuracy and reliability of partial discharge test on aircraft systems to make informed decisions on insulation system design choice. The aim of this paper is to demonstrate the feasibility of partial discharge test of the insulation system on a typical aeronautic motor under such conditions, both electrically and environmentally. To do so, the paper will start by detailing the innovative experimental set-up to be used in the study. It mainly consists in a high-voltage (1000V) inverter drive using SiC components to provide fast rise time surges and associated with phase-by-phase surge filtering. A vacuum chamber is used to simulate altitude while the association of non-intrusive sensors and wavelet based signal processing provided partial discharge detection. Optical detection is also used to reinforce partial discharge inception level accuracy. Then, an analysis is carried out on a 540V motor to find out which combination of switching frequency, harness length, rise time by phase and voltage magnitude is the worst case scenario. The study helps to realize the benefits of using an inverter based test method to find the limits of the insulation system under various pressure and electrical conditions. It is shown that a representative insulation system performance diagram could be built experimentally and used to enhance insulation design and manufacturing choices. This paper will also review the ability of the non-intrusive test method and the associated numerical signal processing to detect partial discharge in a motor fed by fast-rise time surge and under different pressures. The paper concludes with an analysis of results and thoughts about future work regarding advanced test procedure.

[1]  Ian Moir,et al.  Aircraft Systems: Mechanical, Electrical, and Avionics Subsystems Integration , 2008 .

[3]  T. Lebey,et al.  Partial discharge in electric motor fed by a PWM inverter: off-line and on-line detection , 2014, IEEE Transactions on Dielectrics and Electrical Insulation.

[4]  Thierry Lebey,et al.  Partial discharges measurements at the constituents' level of aerospace power electronics converters , 2014, 2014 International Conference on Advances in Communication and Computing Technologies (ICACACT 2014).

[5]  Hao Zhang,et al.  A novel wavelet transform technique for on-line partial discharge measurements. 1. WT de-noising algorithm , 2007, IEEE Transactions on Dielectrics and Electrical Insulation.

[6]  Thibaut Billard,et al.  Non-intrusive partial discharges investigations on aeronautic motors , 2016 .

[7]  Xavier Roboam New trends and challenges of electrical networks embedded in “more electrical aircraft” , 2011, 2011 IEEE International Symposium on Industrial Electronics.

[8]  R. Bartnikas,et al.  Engineering Dielectrics Volume I Corona Measurement and Interpretation , 1979 .

[9]  P. Subburaj,et al.  An improved threshold estimation technique for partial discharge signal denoising using Wavelet Transform , 2013, 2013 International Conference on Circuits, Power and Computing Technologies (ICCPCT).

[10]  Ozcan Kalenderli,et al.  Wavelet base selection for de-noising and extraction of partial discharge pulses in noisy environment , 2015 .

[11]  P. Subburaj,et al.  Partial discharge signal denoising using wavelet techniques-on site measurements , 2013, 2013 International Conference on Circuits, Power and Computing Technologies (ICCPCT).

[12]  Thierry Lebey,et al.  Numerical signal processing methods for partial discharge detection in more electrical aircraft , 2016, 2016 IEEE International Conference on Dielectrics (ICD).

[13]  I. Cotton,et al.  Higher voltage aircraft power systems , 2008, IEEE Aerospace and Electronic Systems Magazine.

[14]  J.A. Ortega,et al.  Moving towards a more electric aircraft , 2007, IEEE Aerospace and Electronic Systems Magazine.

[15]  Hui Ma,et al.  Probabilistic wavelet transform for partial discharge measurement of transformer , 2015, IEEE Transactions on Dielectrics and Electrical Insulation.

[16]  Thierry Lebey,et al.  Recent advances in on-line PDs'detection in power conversion chains used in aeronautics , 2017, 2017 IEEE Workshop on Electrical Machines Design, Control and Diagnosis (WEMDCD).

[17]  Bruno Sareni,et al.  Trade-off between losses and EMI issues in three-phase SiC inverters for aircraft applications , 2017 .