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大型飞机整体壁板喷丸成形延展变形分析
引用本文:彭艳敏,陈金平,杨亮,王永军.大型飞机整体壁板喷丸成形延展变形分析[J].航空制造技术,2017(9).
作者姓名:彭艳敏  陈金平  杨亮  王永军
作者单位:1. 中航飞机股份有限公司西安飞机分公司,西安,710089;2. 西北工业大学机电学院,西安,710072
摘    要:针对基于喷丸成形的大型飞机机翼整体壁板延展变形问题,从影响整体壁板喷丸延展变形的因素出发,通过对整体壁板喷丸成形展向应变的理论计算和实测延展数据对比,得出整体壁板喷丸成形加工环节的延展变形规律。

关 键 词:整体壁板  喷丸成形  延展变形  残余应力

Study on Elongation After Shot Peen Forming for Integral Panel of Large Aircraft
PENG Yanmin,CHEN Jinping,YANG Liang,WANG Yongjun.Study on Elongation After Shot Peen Forming for Integral Panel of Large Aircraft[J].Aeronautical Manufacturing Technology,2017(9).
Authors:PENG Yanmin  CHEN Jinping  YANG Liang  WANG Yongjun
Abstract:Aiming at the elongation problem of the integral panel of large aircraft based on shot peen forming,this article from the factors influencing the integral panel elongation deformation in shot peen forming,through the comparison of theoretical calculation of wingspan shot peen forming strain and experimental data of elongation deformation,elongation law of integral panel in shot peen forming is concluded.
Keywords:Integral panel  Shot peen forming  Extension deformation  Residual stress
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