• CN:11-2187/TH
  • ISSN:0577-6686

机械工程学报 ›› 2020, Vol. 56 ›› Issue (10): 102-109.doi: 10.3901/JME.2020.10.102

• 材料科学与工程 • 上一篇    下一篇

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航空扩口导管轴向收缩量快速预测方法

鲍益东1, 钱文清1, 陈晓豫1, 寸文渊1,2, 舒阳2   

  1. 1. 南京航空航天大学机电学院 南京 210016;
    2. 成都飞机工业(集团)有限责任公司产品研制部 成都 610092
  • 收稿日期:2019-05-28 修回日期:2019-10-31 出版日期:2020-05-20 发布日期:2020-06-11
  • 通讯作者: 鲍益东(通信作者),男,1976年出生,博士,副教授,硕士研究生导师。主要研究方向为板料成形与控制。E-mail:baoyd@nuaa.edu.cn
  • 作者简介:钱文清,女,1994年出生。主要研究方向为板料成形与控制、数字化设计与制造。E-mail:qwqcmcc@nuaa.edu.cn;陈晓豫,女,1995年出生。主要研究方向为板料成形与控制、管路系统分析。E-mail:yannypotter@nuaa.edu.cn
  • 基金资助:
    国家自然科学基金(51875283)和航空科学基金(20161852018)资助项目。

Fast Prediction Method of the Axial Contraction of Aviation Flared Tube

BAO Yidong1, QIAN Wenqing1, CHEN Xiaoyu1, CUN Wenyuan1,2, SHU Yang2   

  1. 1. College of Mechanical Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016;
    2. Product Development Department, Chengdu Aircraft Industrial(Group) Co., Ltd., Chengdu 610092
  • Received:2019-05-28 Revised:2019-10-31 Online:2020-05-20 Published:2020-06-11

摘要: 航空扩口导管的轴向收缩量是影响管路装配质量的重要因素,对于扩口段轴向长度不合格的管件,只能凭工人经验现场调整。常用的有限元法需多次模拟才可求得轴向收缩量,效率较低。自主开发扩口管一步逆成形程序,提出径向投影法获得初始解,并采用网格光顺算法提高初始解精度,经全量理论的塑性迭代获取初始管坯尺寸,从而在几秒内快速预测出精确的轴向收缩量,为设计阶段管坯尺寸的确定提供依据。将扩口管一步逆成形程序的轴向收缩量预测过程与商用有限元软件LS-DYNA、Abaqus对比,一步逆成形程序极大地简化了前处理操作,提高了计算效率。选取多个不同规格的典型航空用导管进行冲压扩口成形试验,一步逆成形程序模拟量相对于试验值的误差在6.33%以内。扩口管一步逆成形程序计算速度快,求解精度高,可准确预测扩口管轴向收缩量,具有工程应用意义。

关键词: 扩口导管, 轴向收缩量, 一步逆成形, 径向投影, 网格光顺

Abstract: The axial contraction of the aviation flared tube is an important factor affecting the pipeline assembly. Currently the flared tube whose axial length is not qualified for the flared section is only adjusted on site by the workers' experience. Commonly used finite element methods require multiple simulations to obtain the axial contraction amount, and the computation efficiency is low. An one-step inverse analysis program of flared tube is developed. A radial projection method is proposed to obtain an initial guess, and the mesh smoothing algorithm is used to improve the precision of the initial guess. The size of the initial tube is obtained through the plastic iteration based on the full-scale theory, and the exact axial contraction is predicted within several seconds. The predicted axial contraction can provide basis for the determination of tube blank size in the design stage. Compared with the commercial finite element software LS-DYNA and Abaqus, the one-step inverse analysis program obviously simplifies the pre-processing operation and improves the calculation efficiency. Typical aviation flared tubes in different specifications are chosen for the stamping and flaring experiments. The error of results of one-step inverse analysis program is within 6.33% compared with experimental values. Generally speaking, the one-step inverse analysis program of flared tube has a fast calculation speed and high solution precision, can accurately predict the axial contraction of the flared tube and has a high practical application value.

Key words: flared tube, axial contraction, one-step inverse analysis, radial projection, mesh smoothing

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