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Optimization of Cutting Interference Machining for Aircraft Roller Bearing Formation

机译:飞机滚子轴承形成切割干扰加工优化

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In the complex components of aircraft roller bearing forming process, it is influenced by the surface mesh inducing factors, resulting in processing accuracy is not good, the error is large. An optimal roller bearing forming machining cutting method is proposed based on the internal tooth interference interpolation correction. The aircraft roller bearing forming machining constraint parameter model building and control analysis of the objective function are taken, Four single points is selected randomly for forming a curvature correction processing measurements in bearing arc at any point in solving the contact line, Newton vector intersection method is used to get the aircraft bearing roll forming and processing conditions of the contact type, spatial spectrum estimation method is used for the coherent processing, an inner tooth interference interpolation correction method taken for vehicle roller bearing machining optimization. The simulation results show that the new method has higher cutting precision, the error converges to the minimum, and the computation cost is less, and it shows a good application value.
机译:在飞机滚子轴承成型过程的复杂部件中,它受到表面网格诱导因子的影响,导致加工精度不好,误差大。基于内部齿干扰插值校正,提出了一种最佳滚子轴承成形加工切割方法。采取了飞机滚子轴承成型加工约束参数模型建筑物的目标函数,随机选择四个单点,以在求解接触线的任何点处随机选择轴承弧中的曲率校正处理测量,牛顿矢量交叉点方法是用于获得接触型的飞机轴承辊成型和加工条件,用于相干处理的空间谱估计方法,采用车辆滚子轴承加工优化的内齿干扰插值校正方法。仿真结果表明,新方法具有更高的切割精度,误差会聚到最小值,计算成本较少,显示出良好的应用值。

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