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A Rapid Method to Achieve Aero-Engine Blade Form Detection

机译:一种实现航空发动机叶片形状检测的快速方法

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摘要

This paper proposes a rapid method to detect aero-engine blade form, according to the characteristics of an aero-engine blade surface. This method first deduces an inclination error model in free-form surface measurements based on the non-contact laser triangulation principle. Then a four-coordinate measuring system was independently developed, a special fixture was designed according to the blade shape features, and a fast measurement of the blade features path was planned. Finally, by using the inclination error model for correction of acquired data, the measurement error that was caused by tilt form is compensated. As a result the measurement accuracy of the Laser Displacement Sensor was less than 10 μm. After the experimental verification, this method makes full use of optical non-contact measurement fast speed, high precision and wide measuring range of features. Using a standard gauge block as a measurement reference, the coordinate system conversion data is simple and practical. It not only improves the measurement accuracy of the blade surface, but also its measurement efficiency. Therefore, this method increases the value of the measurement of complex surfaces.
机译:根据航空发动机叶片表面特征,提出了一种快速检测航空发动机叶片形状的方法。该方法首先基于非接触式激光三角测量原理推导了自由曲面测量中的倾斜误差模型。然后独立开发了四坐标测量系统,根据叶片形状特征设计了专用夹具,并计划了对叶片特征路径的快速测量。最后,通过使用倾斜误差模型对获取的数据进行校正,可以补偿由倾斜形式引起的测量误差。结果,激光位移传感器的测量精度小于10μm。经实验验证,该方法充分利用了光学非接触式测量的快速,高精度和测量范围广的特点。使用标准量块作为测量参考,坐标系转换数据既简单又实用。它不仅提高了叶片表面的测量精度,而且提高了测量效率。因此,该方法增加了复杂表面的测量值。

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