航空合金钢30CrMnSiA深孔钻削预测模型研究
Prediction Model of Deep Hole Drilling of 30CrMnSiA Alloy Steel
-
摘要: 通过正交实验设计方法,开展了航空合金钢30CrMnSiA ϕ2.7 mm深孔钻削实验,研究主轴转速、进给速度和孔深3个钻削参数对30CrMnSiA深孔钻削中孔径偏差的影响规律。通过极差分析发现孔深是影响30CrMnSiA ϕ2.7 mm深孔钻削孔径偏差的主要因素。采用偏最小二乘分析算法,建立了航空合金30CrMnSiA ϕ2.7 mm深孔钻削孔径偏差预测模型。通过对比实验值和预测模型的预测值,得到该预测模型的平均相对误差仅为7.45%,验证了该预测模型的合理性和有效性。Abstract: Experimental study on deep hole drilling of 30CrMnSiA alloy steel was conducted by orthogonal design method. The influences of drilling parameters such as spindle speed, feed rate, and hole depth on the aperture deviation in 30CrMnSiA deep hole drilling were studied. Range analysis is applied to evaluate the influence of various drilling parameters on hole diameter deviation and it can be seen that the hole depth is the main influence factor of hole diameter deviation. Meanwhile, the prediction model of the holediameter deviation is carried out by using partial least squares method. Comparison between predictive value and experimental value reflects that the mean absolute error is small, verifying the reasonableness and validity of prediction model.