The air-gap flux density formula and thrust expression of long primary double sided linear induction machine(DLIM)in the secondary motion reference frame are deduced by using the Maxwell equations firstly.Then,by anal...The air-gap flux density formula and thrust expression of long primary double sided linear induction machine(DLIM)in the secondary motion reference frame are deduced by using the Maxwell equations firstly.Then,by analyzing the factors that affect the thrust ripple in the thrust expression,a shuttle type secondary structure of long primary DLIMs is proposed,and its thrust performances of the machine with different shuttle size combinations are simulated and compared with that of plate secondary long primary DLIM.Comparison results show that the new secondary structure can suppress the thrust ripple and improve the stability of system acceleration.展开更多
针对电磁弹射及空间实验系统用双边型长初级直线感应电机(double sided long primary linear induction motor,DSLPLIM)的电磁推力特性,首先根据电磁场理论,通过对初级行波电流层和次级电流的微分运算,推导出计及端部效应的直线感应电...针对电磁弹射及空间实验系统用双边型长初级直线感应电机(double sided long primary linear induction motor,DSLPLIM)的电磁推力特性,首先根据电磁场理论,通过对初级行波电流层和次级电流的微分运算,推导出计及端部效应的直线感应电机气隙磁密的解析表达式,同时,依据洛伦兹力公式,推导出直线感应电机平均电磁推力的解析计算表达式;其次,为削弱端部效应引起的推力波动,采用发卡式全填充绕组以改善直线感应电机气隙磁密分布的正弦性(减小推力波动),同时为提升电机的电磁推力,改进现有次级板开槽结构,实现涡流路径的优化;最后,针对发卡式绕组和次级板开槽2种改进,利用推导的解析计算公式和3D有限元仿真软件,分别计算双边型直线感应电机的气隙磁密分布和电磁推力特性曲线。对比分析表明:发卡式全填充绕组的使用不仅能削弱直线感应电机的推力波动,还能有效提升电磁推力的大小,提高直线感应电机的运行性能;改进次级开槽结构可有效提升电机的电磁推力,增大推力密度。展开更多
基金supported by the Research Project of Electromagnetic Simulation Research and Development of Induction Motor of Beijing Jiaotong University (No.E18L00100)
文摘The air-gap flux density formula and thrust expression of long primary double sided linear induction machine(DLIM)in the secondary motion reference frame are deduced by using the Maxwell equations firstly.Then,by analyzing the factors that affect the thrust ripple in the thrust expression,a shuttle type secondary structure of long primary DLIMs is proposed,and its thrust performances of the machine with different shuttle size combinations are simulated and compared with that of plate secondary long primary DLIM.Comparison results show that the new secondary structure can suppress the thrust ripple and improve the stability of system acceleration.
文摘针对电磁弹射及空间实验系统用双边型长初级直线感应电机(double sided long primary linear induction motor,DSLPLIM)的电磁推力特性,首先根据电磁场理论,通过对初级行波电流层和次级电流的微分运算,推导出计及端部效应的直线感应电机气隙磁密的解析表达式,同时,依据洛伦兹力公式,推导出直线感应电机平均电磁推力的解析计算表达式;其次,为削弱端部效应引起的推力波动,采用发卡式全填充绕组以改善直线感应电机气隙磁密分布的正弦性(减小推力波动),同时为提升电机的电磁推力,改进现有次级板开槽结构,实现涡流路径的优化;最后,针对发卡式绕组和次级板开槽2种改进,利用推导的解析计算公式和3D有限元仿真软件,分别计算双边型直线感应电机的气隙磁密分布和电磁推力特性曲线。对比分析表明:发卡式全填充绕组的使用不仅能削弱直线感应电机的推力波动,还能有效提升电磁推力的大小,提高直线感应电机的运行性能;改进次级开槽结构可有效提升电机的电磁推力,增大推力密度。