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A TEMPLATE BASED HOLLOW TURBINE BLADE WALL THICKNESS INSPECTION METHOD USING ITS CONE BEAM CT IMAGES AND CAD MODEL

机译:一种基于模板中空涡轮叶片壁厚检查方法,锥梁CT图像和CAD模型

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Hollow turbine blade wall thickness is a critical parameter for ensuring its strength. A template based wall thickness inspection method by using its Cone Beam CT images and CAD model was presented in this paper. Firstly, a modified Marching Cube algorithm was used to generate the blade geometric boundary mesh model from its CBCT images. Then, align the mesh model and the CAD model through the rough alignment method and the Iterative Closest Point based fine alignment method to bring these two models into one common coordinate system. After extracting a wall thickness inspection template from the CAD model and performing the intersecting calculation with the blade mesh model, the wall thickness deviation on the certain section could be generated automatically. The related algorithms was implemented with VC++ programming and verified by a set of simulated blade CBCT images.
机译:中空涡轮叶片壁厚是确保其强度的关键参数。本文提出了一种基于模板基于模板的壁厚检查方法和CAD模型。首先,用于从其CBCT图像生成刀片几何边界网格模型的修改前进的Cube算法。然后,通过粗略对准方法和基于迭代最接近点的精细对准方法对齐网格模型和CAD模型,使这两个模型成为一个公共坐标系。在从CAD模型中提取壁厚度检查模板并用刀片网模型进行交叉计算后,可以自动产生某个部分上的壁厚偏差。相关算法用VC ++编程实现,并由一组模拟刀片CBCT图像验证。

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