1. 西南交通大学 唐山研究院,河北,唐山,063000
2. 西南交通大学 机械工程学院,成都,610031
3. 成都航空职业技术学院 机构 成航智能飞行器工程技术创新研究院,成都,600100
4. 唐山学院 机构 河北省智能装备数字化原始及过程仿真重点实验室,河北,唐山,063000
[ "赵兴,硕士研究生," ]
[ "郭彩玲,教授,硕士生导师," ]
纸质出版:2025
移动端阅览
赵兴, 李旭瑞, 李吉, 等. 结合特征区域分类的飞机蒙皮跨面孔洞修补研究[J]. 机械科学与技术, 2025,44(8):1371-1380.
赵兴, 李旭瑞, 李吉, et al. Study on Aircraft Skin Cross Surface Hole Repair with Feature Region Classification[J]. Mechanical Science and Technology for Aerospace Engineering, 2025, 44(8): 1371-1380.
赵兴, 李旭瑞, 李吉, 等. 结合特征区域分类的飞机蒙皮跨面孔洞修补研究[J]. 机械科学与技术, 2025,44(8):1371-1380. DOI: 10.13433/j.cnki.1003-8728.20230306.
赵兴, 李旭瑞, 李吉, et al. Study on Aircraft Skin Cross Surface Hole Repair with Feature Region Classification[J]. Mechanical Science and Technology for Aerospace Engineering, 2025, 44(8): 1371-1380. DOI: 10.13433/j.cnki.1003-8728.20230306.
应用激光扫描仪扫描飞机蒙皮时,由于支撑飞机的型架遮挡导致获取的点云数据产生跨面孔洞,逆向软件难以修补,影响了飞机三维重建精度,为了修补跨面孔洞,提出一种基于特征区域分类的飞机蒙皮跨面孔洞修补方法。首先利用特征值定义特征区域跨面孔洞类型,检测提取跨面孔洞种子点云;然后利用点云区域生长法分割跨面孔洞,得到小面积孔洞;最后采用最小二乘孔洞修补方法进行修复,实现跨面孔洞修补。在公共数据集上测试结果表明该算法能有效恢复缺失区域,基于以上验证,以工程实例飞机蒙皮跨面孔洞数据为实验对象,实验结果与逆向软件和径向基算法修补效果对比表明,该方法修补区域与原始模型重合度最高,为98.52%,保持了孔洞的曲率特征,实现了较好的修补效果,为飞机损伤检测提供了技术基础。
When using a laser scanner to scan the aircraft skin
the cross surface hole defects may occur due to the occlusion caused by the aircraft frame
which makes it difficult for reverse software to repair and affects the accuracy of the 3D reconstruction. In order to repair the cross surface hole defects
a method based on feature region classification for repairing cross surface hole defects in aircraft skin is proposed. Firstly
feature regions are defined based on the feature values to classify cross surface hole types and detect seed point clouds of cross surface holes. Then
the point cloud region growth method is used to segment the cross surface holes to obtain small area holes. Finally
the least squares hole filling method is used to repair the cross surface holes. The test results of the cross surface hole repair on public datasets show that the algorithm can effectively restore the missing regions. Based on the above verification
the experiment is conducted on the actual data of cross surface holes in the engineering example of aircraft skin. By comparing with the repair effects of reverse soft-ware and radial basis function algorithm
the experimental results show that the present method has the highest overlap degree of 98.52% with the original model in the repair area
maintains the curvature characteristics of the holes
and achieves good repair effect
providing a technical basis for detect the damaged regions on airplane.
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