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:
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.
Study on Aircraft Skin Cross Surface Hole Repair with Feature Region Classification
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.