TY - JOUR
T1 - Effects of Temperature and Pressure on Failure Risk of Electric Motors Based on Partial Discharge Measurements
AU - Hassan, Waqar
AU - Hussain, Ghulam Amjad
AU - Mahmood, Farhan
AU - Shafiq, Muhammad
AU - Montanari, Gian Carlo
N1 - Publisher Copyright:
© 2023 IEEE.
PY - 2023/10/1
Y1 - 2023/10/1
N2 - Typically, partial discharge (PD) diagnostic tests are carried out in laboratories under standard atmospheric conditions. However, during the operation of electric motors (EMs), environmental stresses may increase due to variations in the atmospheric pressure and temperature. This is, for example, the case of electric aircraft and, in general, other aerospace applications. Experimental results show that these stresses may affect the level and phenomenology of PD, thereby compromising the reliability of insulation system. Therefore, neglecting the actual environmental stresses involved in PD testing or monitoring may result in an incorrect interpretation of the health condition of the EMs. This study presents a framework to properly assess the impact of environmental stresses on PD activity and estimate the failure risk of EM insulation. For this purpose, PD diagnostics were carried out by performing a number of experiments on seven EMs in a climate-controlled chamber. PD characteristic features at different levels of environmental stresses are extracted from measurements in order to investigate the PD severity and infer their effect on the resulting insulation degradation. Also, various probability distribution functions are used to estimate the probability of failure and risk assessment corresponding to the PD severity at different levels of environmental stresses. The proposed risk assessment technique can be helpful to plan regular maintenance activities and repair-replacement actions, keeping the reliability at the level requested for most industrial applications involving variable temperature and pressure operations.
AB - Typically, partial discharge (PD) diagnostic tests are carried out in laboratories under standard atmospheric conditions. However, during the operation of electric motors (EMs), environmental stresses may increase due to variations in the atmospheric pressure and temperature. This is, for example, the case of electric aircraft and, in general, other aerospace applications. Experimental results show that these stresses may affect the level and phenomenology of PD, thereby compromising the reliability of insulation system. Therefore, neglecting the actual environmental stresses involved in PD testing or monitoring may result in an incorrect interpretation of the health condition of the EMs. This study presents a framework to properly assess the impact of environmental stresses on PD activity and estimate the failure risk of EM insulation. For this purpose, PD diagnostics were carried out by performing a number of experiments on seven EMs in a climate-controlled chamber. PD characteristic features at different levels of environmental stresses are extracted from measurements in order to investigate the PD severity and infer their effect on the resulting insulation degradation. Also, various probability distribution functions are used to estimate the probability of failure and risk assessment corresponding to the PD severity at different levels of environmental stresses. The proposed risk assessment technique can be helpful to plan regular maintenance activities and repair-replacement actions, keeping the reliability at the level requested for most industrial applications involving variable temperature and pressure operations.
KW - Aerospace
KW - aging estimation
KW - aircraft operation
KW - electric motor (EM)
KW - environmental stresses
KW - partial discharge measurement
KW - pressure and temperature
KW - risk assessment
KW - transportation electrification
UR - http://www.scopus.com/inward/record.url?scp=85151551125&partnerID=8YFLogxK
U2 - 10.1109/TAES.2023.3262622
DO - 10.1109/TAES.2023.3262622
M3 - Article
AN - SCOPUS:85151551125
SN - 0018-9251
VL - 59
SP - 5624
EP - 5633
JO - IEEE Transactions on Aerospace and Electronic Systems
JF - IEEE Transactions on Aerospace and Electronic Systems
IS - 5
M1 - 5
ER -