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A geometry reconstruction approach based on cross-section curve blending for adaptive repair of blades

机译:基于截面曲线融合的几何重构方法自适应修复叶片

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Due to the inevitable distortion and defects of a worn part, the nominal CAD model from the design stage is no longer suitable for the use in the repair process. This causes the main problem of precisely repairing complex blades. In this paper, an approach to geometry reconstruction based on cross-section curve blending with wavelet decomposition for blade adaptive repair is proposed. It is useful to satisfy the demand of smooth transition machining and improve the precision for the repairing of blades. Firstly, the cross-section curve of the repair blade is decomposed with wavelet which can describe the curve geometry property in detail. Also, blending between curves with constraint is implemented while key geometric features can be preserved such as aerofoil chordal lengths and leading edge radii ratio. Secondly, by using the cross-section curve blending and deformation error compensation methods, adaptive model for shape distortion and defects is reconstructed to solve the part-to-part variation machining problem and to realize precision repair for geometrically complex blades. Finally, tool paths used for the last NC machining process can then be generated to implement the repairing process work adaptively. Examples show that the geometry reconstruction approach is feasible for adaptive repair of blades and the results carry high precision and efficiency.
机译:由于不可避免地会出现变形和磨损零件的缺陷,因此从设计阶段开始的名义CAD模型就不再适合在维修过程中使用。这引起精确修复复杂叶片的主要问题。本文提出了一种基于截面曲线融合与小波分解的叶片重构自适应几何修复方法。满足平滑过渡加工的需求并且提高叶片修复的精度是有用的。首先,用小波分解修复叶片的横截面曲线,可以详细描述曲线的几何特性。同样,在具有约束的曲线之间进行融合,同时可以保留关键的几何特征,例如机翼弦长和前缘半径比。其次,采用截面曲线融合和变形误差补偿的方法,重建了形状畸变和缺陷的自适应模型,解决了零件间零件加工问题,实现了复杂叶片的精密修复。最后,然后可以生成用于最后的NC加工过程的刀具路径,以自适应地执行修复过程。实例表明,几何重构方法对于叶片的自适应修复是可行的,其结果具有较高的精度和效率。

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