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Machining distortion prediction of aerospace monolithic components
Authors:Yun-bo Bi  Qun-lin Cheng  Hui-yue Dong  Ying-lin Ke
Institution:(1) State Key Lab of Fluid Power Transmission and Control, Zhejiang University, Hangzhou, 310027, China;(2) Shanghai Spaceflight Precision Machinery Research Institute, Shanghai, 201600, China
Abstract:To predict the distortion of aerospace monolithic components.a model is established to simulate the numerical control (NC)milling process using 3D finite element method(FEM).In this model,the cutting layer is simplified firstly.Then,the models of cutting force and cutting temperature are established to gain the cutting loads,which are applied to the mesh model of the part.Finally,a prototype of machining simulation environment is developed to simulate the milling process of a spar.Key factors influencing the distortion,such as initial residual stress,cutting loads,fixture layout,cutting sequence,and tool path are considered all together.The total distortion of the spar is predicted and an experiment is conducted to validate the numerical results.It is found that the maximum discrepancy between the simulation results and experiment values is 19.0%
Keywords:Monolithic component  Machining distortion  Finite element simulation
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