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Aeroplane engine blade edge reconstruction based on non-uniform B-Spine wavelet algorithm

机译:基于非均匀B-Spine小波算法的飞机发动机叶片边缘重构

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摘要

This paper made the edge reconstruction of the aircraft engine. First, collected rough point cloud data by using visual measuring equipment. Then, smoothed and filtered the point cloud data, took the reasonable simplification, finished pre-processing the point cloud data. Finally, non-uniform B-spline wavelet algorithm was used for acquisition feature point of blades' edge, and took the digital model. The results proved that this method reduced modeling and machining time, and improved smoothness of the model.
机译:本文对飞机发动机进行了边缘重建。首先,使用视觉测量设备收集粗糙的点云数据。然后,对点云数据进行平滑和过滤,进行合理的简化,完成对点云数据的预处理。最后,采用非均匀B样条小波算法获取叶片边缘特征点,并建立了数字模型。结果证明,该方法减少了建模和加工时间,并提高了模型的平滑度。

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