王德重,黄翔,李泷杲,李根. 基于双目多线结构光的铆钉齐平度测量方法[J]. 航空制造技术, 2021, 64(23/24): 57-65. WANG Dezhong, HUANG Xiang, LI Shuanggao, LI Gen . Rivet Flatness Measurement Method Based on Binocular Multi-Line Structured Light. Aeronautical Manufacturing Technology, 2021, 64(23/24): 57-65.
WANG Dezhong, HUANG Xiang, LI Shuanggao, et al. Rivet Flatness Measurement Method Based on Binocular Multi-Line Structured Light[J]. Aeronautical Manufacturing Technology, 2021, 64(23/24).
王德重,黄翔,李泷杲,李根. 基于双目多线结构光的铆钉齐平度测量方法[J]. 航空制造技术, 2021, 64(23/24): 57-65. WANG Dezhong, HUANG Xiang, LI Shuanggao, LI Gen . Rivet Flatness Measurement Method Based on Binocular Multi-Line Structured Light. Aeronautical Manufacturing Technology, 2021, 64(23/24): 57-65. DOI: 10.16080/j.issn1671-833x.2021.23/24.057.
WANG Dezhong, HUANG Xiang, LI Shuanggao, et al. Rivet Flatness Measurement Method Based on Binocular Multi-Line Structured Light[J]. Aeronautical Manufacturing Technology, 2021, 64(23/24). DOI: 10.16080/j.issn1671-833x.2021.23/24.057.
Rivet Flatness Measurement Method Based on Binocular Multi-Line Structured Light
the measurement methods using traditional gage measurement or non-contact point cloud scanning have disadvantages such as large limitations
long preparation periods and difficult data processing. In response to the above problems
this paper proposes a method for measuring the flatness of rivets based on binocular multi-line structured light. Firstly
binocular matching and reconstruction are performed on the structured light image collected by the binocular system
and the measured coordinate system is extracted and fitted. Next
discrete point screening proportional coefficient is introduced to optimize the fitting accuracy of local skin plane and then the discrete point screening scale factor is introduced to further optimize the fitting accuracy of the local skin plane
and finally it is substituted into the rivet flatness measurement model to perform calculations to obtain results. Compared with the traditional contact measurement and point cloud scanning
this method saves a lot of time for point cloud data processing and improves the measurement efficiency
and can complete the detection task of narrow cavity such as the aircraft inlet by mechanical arm equipped with a small measurement terminal
which reduces limitations. The experimental results show that this method is applicable to both concave and convex features of the rivet head
and the maximum measurement error of rivet flatness is less than 0.03mm
which meets the requirements of visual measurement of rivet flatness