基于三维点云的固体火箭发动机裙端面对接孔位置信息检测技术

    Position information detection technology of SRM skirt end face joint hole based on 3D point cloud

    • 针对固体火箭发动机裙端面对接螺纹孔缺乏有效空间位置检测手段、精度仅靠加工工艺保证而影响装配质量的问题,提出了一种基于三维激光扫描技术的裙端面对接螺纹孔位置信息快速检测方法。首先,构建了基于三维激光扫描仪的自动跟踪扫描系统,以获取裙端面高精度三维点云;其次,利用基于KD-tree的改进移动最小二乘法(Moving Lest Squares,MLS)对点云进行优化处理,以提高特征拟合的精度;最后,利用三维点云进行逆向建模,将裙端面逆向模型与三维点云进行配准后对相关尺寸进行快速自动化检测。结果表明,6次重复性检测试验数据的极差在0.029 3°以内,以6次检测数据平均值为真值,数据偏差皆在0.021 1°以内,相对标准偏差RSD均小于1%。

       

      Abstract: To address the issue of insufficient high-precision detection approaches for the spatial geometric coordinates of docking threaded holes on the skirt end face of solid rocket motor (SRM), which affects the assembly quality because the accuracy is solely ensured by the machining process, a rapid detection method for the position information of the docking threaded holes on the skirt end face based on 3D laser scanning technology is proposed. Firstly, an automatic tracking and scanning system was constructed by using a robot-driven 3D laser scanner to obtain the high-precision 3D point cloud of the skirt end face. Secondly, an improved moving least-squares (MLS) method based on KD-tree was used to optimize and process the point cloud to improve the accuracy of feature fitting. Finally, reverse modeling was carried out on the skirt end face of the 3D point cloud. After registering the reverse model of the skirt end face with the 3D point cloud, the relevant dimensions were quickly and automatically detected. The results show that the range of the six repeated test data is within 0.0293°. Taking the average value of the six groups of test data as the true value, the data deviation is within 0.0211°, and the RSD is less than 1%, which meets the requirements of engineering applications.

       

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