A progressive approach to predict shot peening process parameters for forming integral panel of Al7050-T7451  

作　　者：Chuang LIU Zhiyong ZHAO Xianjie ZHANG Junbiao WANG 

机构地区：[1]School of Mechanical Engineering,Northwestern Poly technical University,Xi'an 710072,China

出　　处：《Chinese Journal of Aeronautics》2021年第5期617-627,共11页中国航空学报（英文版）

基　　金：supported by the National Level Project of China。

摘　　要：In this paper,a progressive approach to predict the multiple shot peening process parameters for complex integral panel is proposed.Firstly,the invariable parameters in the forming process including shot size,mass flow,peening distance and peening angle are determined according to the empirical and machine type.Then,the optimal value of air pressure for the whole shot peening is selected by the experimental data.Finally,the feeding speed for every shot peening path is predicted by regression equation.The integral panel part with thickness from 2 mm to 5 mm and curvature radius from 3200 mm to 16000 mm is taken as a research object,and four experiments are conducted.In order to design specimens for acquiring the forming data,one experiment is conducted to compare the curvature radius of the plate and stringer-structural specimens,which were peened along the middle of the two stringers.The most striking finding of this experiment is that the outer shape error range is below 3.9%,so the plate specimens can be used in predicting feeding speed of the integral panel.The second experiment is performed and results show that when the coverage reaches the limit of 80%,the minimum feeding speed is 50 mm/s.By this feeding speed,the forming curvature radius of the specimens with different thickness from the third experiment is measured and compared with the research object,and the optimal air pressure is 0.15 MPa.Then,the plate specimens with thickness from 2 mm to 5 mm are peened in the fourth experiment,and the measured curvature radius data are used to calculate the feeding speed of different shot peening path by regressive analysis method.The algorithm is validated by forming a test part and the average deviation is 0.496 mm.It is shown that the approach can realize the forming of the integral panel precisely.

关 键 词：Curvature radius measure Integral panel Process parameters prediction Regressive analysis method Shot peening process 

分 类 号：TG668[金属学及工艺—金属切削加工及机床] V261[航空宇航科学与技术—航空宇航制造工程]