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Error compensation for machining of large thin-walled part with sculptured surface based on on-machine measurement

机译:基于机上测量的雕刻表面加工大型薄壁部件的误差补偿

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摘要

Large thin-walled parts are widely used in aerospace. Due to its low rigidity, force- and thermal-induced cutting deformation immediately affects the dimensional accuracy of machined parts. Multilayer milling strategy is usually utilized due to its low rigidity, which results in reduction of machining efficiency. In this work, a typical large thin-walled part, tank bottom of the rocket, is selected as an application object and an adaptive deformation error compensation method for large thin-walled part is proposed. An integrated on-machine measurement (OMM) system is developed to acquire the part's geometry. Geometry of outer surface is directly measured and constructed by a touch-trigger probe installed on machine tool's spindle, while the geometry of inner surface is determined by measuring the thickness at each probe point, using an ultrasonic thickness gage. As such, machining error for each layer cutting is identified by comparing with the designed geometry. A deformation prediction model is established to predict the cutting deformation of the next layer based on the calibrated error in previous layer cutting, so as to compute the compensation value. A machining error compensation algorithm is then developed to eliminate the deformation error by modifying the machining toolpath. At last, machining experiment is conducted to verify the feasibility of the proposed methodology.
机译:大型薄壁零件广泛用于航空航天。由于其低刚性,力和热诱导的切割变形立即影响加工零件的尺寸精度。由于其低刚性,通常使用多层铣削策略,从而导致加工效率降低。在这项工作中,选择典型的大薄壁部分,火箭的罐底部作为应用对象,提出了大薄壁部分的自适应变形误差补偿方法。开发了一个集成的机床测量(OMM)系统以获取部分的几何形状。外表面的几何形状由安装在机床主轴上的触发探针直接测量和构造,而使用超声厚度计,通过测量每个探头点处的厚度来确定内表面的几何形状。这样,通过与设计的几何形状进行比较来识别每个层切割的加工误差。建立变形预测模型以基于先前层切割中的校准误差来预测下一层的切割变形,以计算补偿值。然后开发了一种加工误差补偿算法来通过修改加工刀具路径来消除变形误差。最后,进行加工实验以验证所提出的方法的可行性。

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