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Aero-engine blade deformation control of milling process

机译:空气发动机叶片变形控制铣削过程

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The leaf blade manufacture precision's influencing factors are numerous, and they have coupling relationship each other. So it is difficult to peel out a single factor on the influencing regularity of the blade's machining accuracy. By researching the engine blades of helical milling state under the existing fixture, the leaf blade deformable model based on the instantaneous milling strength was established. Meanwhile, the off-line multi-level error compensation plan was proposed based on the processing surface static error forecasts and compensation. In order to revise the primitive NC tool path code and eliminate the processing distortion inaccuracy, the elastic deformity on each knife position spot is solved on the basis of iterative solution, using the finite element simulation and milling strength model. By using ANSYS finite element simulation, it receives the real-time error compensation of the tool path. And then the experiment has proven the accuracy and the usability of the compensation plan.
机译:叶片制造精度的影响因素无数,它们彼此耦合。因此,难以剥离一个因素对刀片加工精度的影响规律。通过在现有夹具下研究螺旋铣削状态的发动机叶片,建立了基于瞬时铣削强度的叶片可变形模型。同时,基于处理表面静态误差预测和补偿,提出了离线多级误差补偿计划。为了修改原始的NC工具路径代码并消除处理失真不准确,在每个刀具位置点的弹性畸形在使用有限元模拟和铣削强度模型的迭代解之基于迭代解。通过使用ANSYS有限元模拟,它接收刀具路径的实时误差补偿。然后实验证明了补偿计划的准确性和可用性。

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