Target point cloud segmentation method applied to turbine blade film hole detection
A technology of turbine blades and gas film holes, which is applied in image analysis, measuring devices, optical devices, etc., can solve problems such as large impact on edge detection accuracy, over-segmentation, and difficulty in ensuring segmentation accuracy, so as to avoid unstable segmentation results Effect
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[0026] Such as Image 6 As shown, this embodiment involves an application such as figure 1 In the shown target point cloud segmentation method applied to the detection of air film holes in aeroengine turbine blades, the air film holes on the blades are the target point cloud regions of the segmentation method in the present invention.
[0027] This embodiment includes the following steps:
[0028] Step 1) Turbine blade laser point cloud scanning: through the five-axis laser measurement platform, the three-dimensional point cloud of the turbine blade space is collected by multi-position scanning, such as figure 2 shown.
[0029] Step 2) Scan point cloud slice: based on the laser sensor measurement trajectory and the distribution characteristics of the laser point cloud, slice the scanned point cloud in the forward direction, and project it on the XZ plane into a two-dimensional point cloud slice unit d with a length of 16 mm in the X direction i (i=1,2,3,...,n), initialize ...
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