Numerical analysis of large-scale tip-driving electric motors for thrust fan
Numerical analysis of large-scale tip-driving electric motors for thrust fan
复制标题
大型推力风扇叶尖驱动电机数值分析
DOI：
10.2514/6.2014-3642
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发表时间：
2014
期刊：
影响因子：
--
通讯作者：
T. Tagashira
中科院分区：
文献类型：
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作者：
K. Okai;T. Himeno;Toshinori Watanabe;H. Nomura;T. Tagashira
本文给出了适合于驱动飞机推进风扇的电机配置的数值模拟结果，以阐明电机控制参数的影响。两个实验模型的结果示出了本参数分析与电机概念的定性趋势进行比较。在模拟中确定的参数是脉冲的起始时间，漆包线圈的相移，转速和输入电流。结果揭示了几个重要的控制变量，并强调了通过改变变量的数量来优化性能的可能性。
This paper shows numerical simulation results of a motor configuration suited to driving aircraft propulsion fans to elucidate the effects of the motor control parameters. Two experimental model results are shown to compare the present parametric analysis with the qualitative tendency of the motor concept. The parameters determined in the simulation were onset timing of the pulse, phase shift of the enamoring coils, rotation speed and input current. The results revealed several important control variables and underscored the possibility of optimizing the performance by changing the number of variables.