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作 者:刘希军 刘小涵[1] 高丽霞[1] LIU Xijun;LIU Xiaohan;GAO Lixia(Aviation Engineering Institute, Civil Aviation Flight University of China, Guanghan Sichuan 618307, China)
机构地区:[1]中国民用航空飞行学院航空工程学院,四川广汉618307
出 处:《微电机》2020年第4期27-32,共6页Micromotors
基 金:四川省教育厅科技一般项目(18ZB0687);校面上项目基金(J2019-090)。
摘 要:根据实际弹射指标要求,分析变极距双边直线感应电机的磁场特性和电感特性。在分析极距连续变化的直线感应电机时,将变极距模式拓展为变相宽度的形式,通过分析变极矩长初级双边直线感应电机气隙磁场,求取任意位置所在的区域的磁感应强度表达式。仿真分析极距的变化对电机磁感应强度的影响。计算变极距直线感应电机绕组自感和互感值,仿真分析极距的变化对自感参数和互感参数的影响。According to the actual ejection index requirements,the magnetic field characteristics and inductance characteristics of the variable pole distance double-sided linear induction motor were analyzed.In the analysis of the linear induction motor with continuous variation of the pole distance,the variable pole distance mode was extended to the form of the variable phase width.By analyzing the air gap magnetic field of the variable bipolar long primary bilateral linear induction motor,the magnetic induction intensity expression of the region where the arbitrary position is located was obtained.The effect of the variation of the pole pitch on the magnetic induction of the motor was simulated.The self-inductance and mutual inductance of the winding of the variable-pole linear induction motor were calculated,and the influence of the variation of the pole distance on the self-inductance parameters and the mutual inductance parameters was simulated.
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