TY - GEN
T1 - PDIV Modeling for Rectangular Wire Turn-to-Turn Insulation of Inverter-Fed Motors at Different Cruising Altitudes
AU - Naderiallaf, Hadi
AU - Gerada, Chris
AU - Degano, Michele
AU - Gerada, David
N1 - Publisher Copyright:
© 2024 IEEE.
PY - 2024
Y1 - 2024
N2 - This study develops a predictive model for partial discharge inception voltage (PDIV) in turn-to-turn insulation of form-wound windings for inverter-fed motors considering a range of altitudes, from ground to cruise levels. Emphasis is placed on the application of rectangular insulated wires (i.e., edgewise insulated wires). Using Schumann's streamer inception criterion (SCSIC), the PDIV predictive model explores six distinct air pressures corresponding to altitudes: 1013 mbar (6.8 ft), 800 mbar (6.4k ft), 600 mbar (13.8k ft), 200 mbar (38.6k ft), 150 mbar (44.3k ft), and 100 mbar (51.8k ft). PDIV estimations are conducted under AC 50 Hz, unipolar positive (UP), and bipolar (BP) steep-fronted square waveform excitations, characterized by a switching frequency of 2.5 kHz, rise time of 80 ns, and pulse width duration of 100 μs. The PDIV model supports aerospace coil winding design by guiding wire geometry decisions, eliminating costly insulation experiments, and ensuring reliability at operational altitudes.
AB - This study develops a predictive model for partial discharge inception voltage (PDIV) in turn-to-turn insulation of form-wound windings for inverter-fed motors considering a range of altitudes, from ground to cruise levels. Emphasis is placed on the application of rectangular insulated wires (i.e., edgewise insulated wires). Using Schumann's streamer inception criterion (SCSIC), the PDIV predictive model explores six distinct air pressures corresponding to altitudes: 1013 mbar (6.8 ft), 800 mbar (6.4k ft), 600 mbar (13.8k ft), 200 mbar (38.6k ft), 150 mbar (44.3k ft), and 100 mbar (51.8k ft). PDIV estimations are conducted under AC 50 Hz, unipolar positive (UP), and bipolar (BP) steep-fronted square waveform excitations, characterized by a switching frequency of 2.5 kHz, rise time of 80 ns, and pulse width duration of 100 μs. The PDIV model supports aerospace coil winding design by guiding wire geometry decisions, eliminating costly insulation experiments, and ensuring reliability at operational altitudes.
KW - Aerospace testing
KW - insulation
KW - inverter-fed machines
KW - modeling
KW - partial discharge inception voltage
KW - partial discharges
KW - pulse width modulation
KW - rectangular wire
UR - http://www.scopus.com/inward/record.url?scp=85207525777&partnerID=8YFLogxK
U2 - 10.1109/ICEM60801.2024.10700449
DO - 10.1109/ICEM60801.2024.10700449
M3 - Conference contribution
AN - SCOPUS:85207525777
T3 - 2024 International Conference on Electrical Machines, ICEM 2024
BT - 2024 International Conference on Electrical Machines, ICEM 2024
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - 2024 International Conference on Electrical Machines, ICEM 2024
Y2 - 1 September 2024 through 4 September 2024
ER -