基于非均匀B-Spine小波算法的飞机发动机叶片边缘重构

Hao Wang, Liwen Wang, Tao Wang, Wei Zhao, T. Dong
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引用次数: 1

摘要

本文对飞机发动机进行了边缘重建。首先,利用视觉测量设备采集粗糙点云数据。然后对点云数据进行平滑滤波,进行合理的简化,完成点云数据的预处理。最后,采用非均匀b样条小波算法获取叶片边缘特征点,并建立数字模型。结果表明,该方法减少了建模和加工时间,提高了模型的平滑度。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Aeroplane engine blade edge reconstruction based on non-uniform B-Spine wavelet algorithm
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.
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