2020
DOI: 10.1109/tte.2020.2979009
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Partial Discharge Investigation of Form-Wound Electric Machine Winding for Electric Aircraft Propulsion

Abstract: Electric machine for aircraft propulsion is required to have high power density and high reliability, but the harsh operating environment, such as low air pressure, will challenge the motor's insulation system. This article presents the partial discharge (PD) investigation of the form-wound winding in high-frequency electric machines for electric aircraft propulsion. Experimental results show that the PD activity is largely enhanced due to the decrease in air pressure. PD inception voltage (PDIV) decreases to … Show more

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Cited by 32 publications
(7 citation statements)
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“…The increasing defects increases the possibility of electrical trees extending to the surroundings, which makes it easier to produce bush-type trees. In addition, the partial discharge under high-frequency AC voltage occurs within a short period of time after the voltage polarity is reversed; hence, higher voltage frequency means that the number of discharges increases proportionally [ 26 , 27 , 28 ]. Although the maximum partial discharge amplitude decreases with the increasing voltage frequency, the average partial discharge amplitude did not decrease when the voltage frequency is below 20 kH [ 26 , 29 ].…”
Section: Discussionmentioning
confidence: 99%
“…The increasing defects increases the possibility of electrical trees extending to the surroundings, which makes it easier to produce bush-type trees. In addition, the partial discharge under high-frequency AC voltage occurs within a short period of time after the voltage polarity is reversed; hence, higher voltage frequency means that the number of discharges increases proportionally [ 26 , 27 , 28 ]. Although the maximum partial discharge amplitude decreases with the increasing voltage frequency, the average partial discharge amplitude did not decrease when the voltage frequency is below 20 kH [ 26 , 29 ].…”
Section: Discussionmentioning
confidence: 99%
“…The critical field strength is drastically reduced due to lower pressures at higher altitudes. Thus, challenges with partial discharges can increase for motor windings as well as cable insulation in aircraft applications [41], [42]. Inside the aircraft body with the environmental control system (ECS) intact, the critical electric field is 25 kV per cm [43], which informs the insulation design of individual power components.…”
Section: ) Basic Mea Requirements and Reliability Concernsmentioning
confidence: 99%
“…The use of WBG devices can also introduce additional challenges for the insulation system design in MEA and HEA applications. Generally, reducing the switching losses by taking advantage of the potential for faster switching of WBG devices, will increase the challenges with EMI and the potential for partial discharge activity in insulation materials [41], [42], [99]. Thus, the utilization of SiC devices in established converter topologies for S/G applications and other electromagnetic actuators, might lead to the need for dedicated dV /dt-filters [100], [101].…”
Section: Prospects and Challenges Of Ongoing Pec Developments For mentioning
confidence: 99%
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“…It should be noted that according to the standard for aircraft power quality, the electric machine on the aircraft should be driven by sinusoidal voltage with distortion factor less than 2% [19]. Therefore, the harmonics caused by pulse‐width modulation (PWM) driver should be filtered by proper filters [20, 21], which means the experiment in this study is performed in a sinusoidal situation. The adoption of filters will inevitably lead to several disadvantages such as weight increase and efficiency decrease.…”
Section: Form‐wound Windings and Accelerated Aging Experimentsmentioning
confidence: 99%