The invention belongs to the technical field of
aviation, and particularly relates to an
aviation high-power motor round wire
alternating current copper loss evaluation and reduction method, which comprises the following steps of: based on a
stator after wire embedding, measuring wire resistances at different frequencies and different rotor positions by adopting an
alternating current resistance tester, further calculating
alternating current copper loss again by using simulated phase current, and judging whether the alternating current
copper loss is met or not; if yes, completing the design; and if not, optimizing the alternating current
copper loss again, and repeatedly calculating the alternating current
copper loss until the alternating current
copper loss meets the requirement. MotorCAD
software is adopted to calculate alternating current copper loss through finite elements, modeling is simple, winding
subdivision is refined, and the difference between the calculation result and the actual result is small. The
stator winding mode is optimized, and the
ring current of the groove leakage flux on the same turn of wires located at different groove height positions is reduced; and the
stator slot size is optimized, so that the slot size with relatively low alternating current copper consumption can be obtained. Part of tests prove that the alternating current copper consumption can be greatly reduced, and the
motor efficiency is improved.