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飞机薄壁构件铆接干涉配合的数值模拟

符文科 马贵春 王迎

兵工自动化2017,Vol.36Issue(1):64-67,87,5.
兵工自动化2017,Vol.36Issue(1):64-67,87,5.DOI:10.7690/bgzdh.2017.01.016

飞机薄壁构件铆接干涉配合的数值模拟

Numerical Simulation of Riveting Interference Fit of Aircraft Thin-walled Structures

符文科 1马贵春 1王迎1

作者信息

  • 1. 中北大学机电工程学院,太原 030051
  • 折叠

摘要

Abstract

In order to improve the predictability of aircraft riveting process test, build numerical simulation model of aircraft thin-walled structures riveting interference fit. The model uses finite element software ANSYS LS-DYNA, carry out the numerical simulation of a single rivet interference fit dynamic riveting process. Analyze the relationship between process parameters at different overhang and the amount of interference formed by caulking and the corresponding fatigue life. Simulation results show that when meeting the same size and appearance requirements under heading with extended amount of caulking between 1.1D to 1.2D, the riveting interference value distribution is uniform with the highest quality and maximum fatigue life.

关键词

铆接/数值模拟/干涉配合/有限元分析

Key words

riveting/numerical simulation/interference fit/finite element analysis

分类

信息技术与安全科学

引用本文复制引用

符文科,马贵春,王迎..飞机薄壁构件铆接干涉配合的数值模拟[J].兵工自动化,2017,36(1):64-67,87,5.

基金项目

山西省科技攻关项目(20140321008-03) (20140321008-03)

兵工自动化

OACSTPCD

1006-1576

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