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Aircraft Load-Bearing Component Structure Measurement Point Cloud Processing and Error Automatic Evaluation |
PENG Qingyu, TIAN Yaming, JIANG Cheng, WANG Gang, LI Wenlong |
State Key Laboratory of Digital Manufacturing Equipment and Technology, Huazhong University of Science and Technology, Wuhan 430074, China |
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Abstract Aircraft bearing component is the key bearing component of large passenger aircraft and fighter aircraft, which is prone to dimensional deformation during the forming process. However, the current caliper, plug gauge testing method has some problems, such as low efficiency and poor consistency of results. To this end, this paper intends to solve above problems by three-dimensional measurement technology. This paper proposes a crude registration method based on standard spherical characteristics and a fine registration method based on the shaft hole key characteristics. Meanwhile, studies the size/shade error systematic automatic calculation method of the aircraft support member, and conducts digital detection experiment of a model aircraft holder member based on autonomous software modules. The results show that the proposed method has significantly improved the detection efficiency and stability compared with the manual detection method.
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