材料工程与机械制造

飞机橡皮囊成形零件毛坯精确预示方法研究

  • 朱明华 ,
  • 王文斌 ,
  • 鲍益东 ,
  • 黄翔
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  • 1. 南京航空航天大学 机电学院, 江苏 南京 210016;
    2. 上海飞机制造有限公司, 上海 200436
朱明华 女, 博士研究生, 研究员。主要研究方向: 飞机钣金零件成形工艺。 Tel: 021-61385691 E-mail: zhuminghua@comac.cc;王文斌 男, 研究员, 博士生导师。主要研究方向: 大型飞机制造。 Tel: 021-61385691 E-mail: wangwenbin@comac.cc;鲍益东 男, 博士, 副教授。主要研究方向: 板料成形与控制。 Tel: 025-84892570 E-mail: baoyd@nuaa.edu.cn;黄翔 男, 博士, 教授, 博士生导师。主要研究方向: 数字化设计、 制造与检测。 Tel: 025-84892910 E-mail: xhuang@nuaa.edu.cn

收稿日期: 2012-04-23

  修回日期: 2012-10-18

  网络出版日期: 2013-03-29

基金资助

国家自然科学基金(51075206);2011年度上海市高新技术产业化重点项目(11-42);上海飞机制造有限公司2012年度创新基金

Research on Precise Blank Prediction Method of Aircraft Part by Rubber Bladder Forming

  • ZHU Minghua ,
  • WANG Wenbin ,
  • BAO Yidong ,
  • HUANG Xiang
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  • 1. College of Mechanical and Electrical Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China;
    2. Shanghai Aircraft Manufacturing Co., Ltd, Shanghai 200436, China

Received date: 2012-04-23

  Revised date: 2012-10-18

  Online published: 2013-03-29

Supported by

National Natural Science Foundation of China (51075206); 2011 Advanced Technology Key Project of Shanghai Municipal Commission of Economy and Informatization (11-42); 2012 Innovation Funds of Shanghai Aircraft Manufacturing Co., Ltd.

摘要

橡皮囊成形是飞机钣金零件成形的主要方法之一,其初始毛坯形状的预示是橡皮囊成形中的一个难点问题。针对橡皮囊成形的工艺特点,提出了一种基于一步逆成形有限元法的飞机橡皮囊成形钣金零件毛坯快速精确预示方法。首先将设计好的飞机钣金零件作为最终构形,然后采用一步逆成形有限元法进行初始毛坯的快速反向模拟,最后将通过该方法获得的毛坯外形应用到实际飞机钣金橡皮囊成形中,实验结果表明该方法可以快速精确地预示出飞机橡皮囊成形钣金零件的初始毛坯形状。

本文引用格式

朱明华 , 王文斌 , 鲍益东 , 黄翔 . 飞机橡皮囊成形零件毛坯精确预示方法研究[J]. 航空学报, 2013 , 34(3) : 670 -676 . DOI: 10.7527/S1000-6893.2013.0105

Abstract

Rubber bladder forming is one of the main forming methods for aircraft sheet metal parts in which the prediction of initial blank shape is difficult. In accordance with the technology characteristics of rubber bladder forming, a fast prediction method is proposed for the initial blank shape of a rubber bladder formed part based on one-step inverse forming finite element method. Firstly, the designed aircraft sheet metal part is treated as the final configuration; then a quick reverse simulation is carried out to obtain the initial blank by the one-step inverse finite element method. Finally, the blank outline from the above method is applied to real rubber bladder forming manufacture. The experimental results demonstrate that this method can predict the precise initial blank shape for a rubber bladder forming part.

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