| 定子磁钢轨道拼接错位对动圈式永磁直线电机性能的影响 |
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| 引用本文： | 吴峻,宋蕾,周文武,黄胜军.定子磁钢轨道拼接错位对动圈式永磁直线电机性能的影响[J].国防科技大学学报,2018,40(1):138-144. |
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| 作者姓名： | 吴峻 宋蕾 周文武 黄胜军 |
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| 作者单位： | 国防科学技术大学 机电工程与自动化学院,国防科学技术大学 机电工程与自动化学院,国防科学技术大学 机电工程与自动化学院,国防科学技术大学 机电工程与自动化学院 |
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| 基金项目： | 国家科技支撑计划资助项目（2012BAG07B01） |
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| 摘 要： | 陆基车载无人机电磁弹射器是一种新型的弹射起飞装置。为了实现高机动性,提出双边动圈式永磁直流直线电机和定子磁钢轨道分段拼接结构方案。为了评估定子磁钢轨道拼接可能对电机性能的影响,建立了永磁直线电机模型。利用有限元分析软件,分析研究了轨道分段拼接上下错位、左右错位以及倾斜错位可能造成的影响,根据分析结果给出了磁钢轨道拼接错位所允许的偏移范围大小。
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| 关 键 词： | 无人机电磁弹射器 动圈式永磁直线电机 磁钢轨道 拼接错位 有限元分析 |
| 收稿时间： | 2016/11/15 0:00:00 |
| 修稿时间： | 2017/4/11 0:00:00 |
Influence of magent track splice dislocation on the performance of moving-coil permanent magnet linear motor |
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| WU Jun,SONG Lei,ZHOU Wenwu and HUANG Shengjun.Influence of magent track splice dislocation on the performance of moving-coil permanent magnet linear motor[J].Journal of National University of Defense Technology,2018,40(1):138-144. |
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| Authors: | WU Jun SONG Lei ZHOU Wenwu and HUANG Shengjun |
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| Institution: | College of Artificial Intelligence, National University of Defense Technology, Changsha 410073, China,College of Artificial Intelligence, National University of Defense Technology, Changsha 410073, China,College of Artificial Intelligence, National University of Defense Technology, Changsha 410073, China and College of Artificial Intelligence, National University of Defense Technology, Changsha 410073, China |
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| Abstract: | Land-based vehicle electromagnetic launcher for unmanned aerial vehicle(UAV) is a new take-off device. In order to realize the high maneuverability, a bilateral moving-coil permanent magnet dc linear motor with the stator magnet track section splicing structure scheme was presented. In order to evaluate the influence of stator magnet track splice on the performance of the motor, the permanent magnet linear motor model was established. The influence of the up and down dislocation, the left and right dislocation and the tilting dislocation of the segmented splice are analyzed by using the finite element analysis software. Based on the analysis results, the allowable magnet track splicing offset range is given. |
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| Keywords: | electromagnetic launcher for unmanned aerial vehicle moving-coil permanent magnet linear motor magent track splice dislocation finite element method |
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