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Assembly Tolerance Analysis Method Based on the Real Machine Model with Three Datum Planes Location

机译:基于三个基准飞机的真正机模型的组装公差分析方法

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An assembly tolerance analysis method based on the real machine model is proposed, aiming to investigate the effect of the geometric errors of datum feature on the result of tolerance chain. The real parts are simulated by the variation of the geometric features, which are represented by the control point variation model and generated by the Monte Carlo simulation. The investigated objective is the assembly success rate of pinhole assembly at the location with the three datum planes, the assembly clearance or interference is calculated according to the assembly requirements and assembly process. The part coordinate system in assembly is constructed firstly by the datum embodiment principles, then the position of the junction planes are determined according to the assembly requirements, and finally, the position of the parts relative to machine are determined by the coordinate transformation. The assembly success rate is represented by the probability distribution of clearance or interference between pin and hole, and the influences of the datum errors on the assembly result are discussed by the example assembly.
机译:提出了一种基于真实机械模型的组装公差分析方法,旨在研究基于公差链的结果的几何误差的影响。通过由控制点变化模型表示的几何特征的变化来模拟实际部分,并由蒙特卡罗模拟产生。调查目标是用三个基准面,装配清除或干扰根据大会要求和装配过程计算的定位器组件的装配成功率。组件中的零件坐标系首先通过基准实施例的原理构造,然后根据组装要求确定结平面的位置,最后,通过坐标变换确定部件相对于机器的位置。装配成功率由引脚和孔之间的间隙或干扰的概率分布表示,并且通过示例组件讨论了对组装结果对组装结果的影响。

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