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(07A738) Design of permanent magnet eddy current brake for a small scaled electromagnetic launch model

机译:(07A738)用于小型电磁发射模型的永磁涡流制动器的设计

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A variable pole-pitch double-sided permanent magnet (PM) linear eddy current brake (LECB) is proposed for a small scaled electromagnetic launch model. A two-dimensional (2D) analytical steady state model is presented for the double-sided PM-LECB, and the expression for the braking force is derived. Based on the analytical model, the material and eddy current skin effect of the conducting plate are analyzed. Moreover, a variable pole-pitch double-sided PM-LECB is proposed for the effective braking of the moving plate. In addition, the braking force is predicted by finite element (FE) analysis, and the simulated results are in good agreement with the analytical model. Finally, a prototype is presented to test the braking profile for validation of the proposed design.
机译:提出了一种可变极间距双面永磁体(PM)线性涡流制动器(LECB),用于小缩放电磁发射模型。为双面PM-LECB提出了一种二维(2D)分析稳态模型,推导出制动力的表达式。基于分析模型,分析了导电板的材料和涡流皮肤效果。此外,提出了一种可变极间距双面PM-LECB,用于使移动板的有效制动。另外,通过有限元(FE)分析预测制动力,并且模拟结果与分析模型很好。最后,提出了一种原型以测试制动轮廓以验证所提出的设计。

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