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Research on Modeling Turbine Blade in Reverse Engineering

机译:逆向工程中涡轮叶片建模的研究

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摘要

With the development of aero manufacturing, turbine blade is required to be reconstructed quickly and accurately. Precise description is the premise for turbine blade machining. In order to model the blade accurately, a fitting algorithm based on the principle of least square and polar line properties of ellipse is presented to extract the important parameters of leading edge and trailing edge. Validation with experimental results demonstrates the accuracy and the robustness of this parameters extraction method.
机译:随着航空制造业的发展,需要快速而准确地重建涡轮叶片。精确的描述是涡轮叶片加工的前提。为了对叶片进行精确建模,提出了一种基于最小二乘和极线椭圆特性的拟合算法,提取了前缘和后缘的重要参数。实验结果验证了该参数提取方法的准确性和鲁棒性。

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