NUMERICAL STUDY ON THE FORCEMATE BUSHING COLD EXPANSION OF COMPOSITE HOLES USING A NOVEL ASSISTING SLEEVE

被引:0
|
作者
Yan, Wuzhu [1 ]
Li, Zhen [2 ]
Liang, Shujing [3 ]
Guo, Yuchang [1 ]
Chen, Xifeng [2 ]
Wang, Xing [4 ]
Liu, Jun [1 ]
Geng, Xiaoliang [1 ]
Long, Xu [1 ]
机构
[1] Northwestern Polytech Univ, Sch Mech Civil Engn & Architecture, Dept Engn Mech, Xian 710129, Peoples R China
[2] AVIC First Aircraft Inst, Dept Struct Design, Xian 710087, Peoples R China
[3] Aecc Aero Sci & Technol Co LTD, Aero Engine Technol Blade Branch, Chengdu 610041, Peoples R China
[4] Shenyang Aircraft Ind Grp Co LTD, Innovat Res Inst, Shenyang 110031, Peoples R China
基金
中国国家自然科学基金;
关键词
fiber reinforced composite; cold expansion; bushing; composite holes; residual stress; finite element simulation; OPTIMIZATION;
D O I
10.2140/jomms.2024.19.747
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
Cold expansion technology has been one of the most common anti-fatigue strengthening technologies for fastening holes. In this paper, a newly developed assisting sleeve is employed to install the ForceMate bushing, and the resulting deformation, rebound, drawing force, contact pressure, residual stress and damage are compared to those resulting from traditional ForceMate bushing process. The 3D Hashin failure criterion was implemented into finite element simulation via a specially written user subroutine to simulate the deformation and failure of cold expanded composite holes. The results show that a more uniform distribution of residual contact pressure and residual circumferential stress is achieved by introducing the assisting sleeve, and less damage around the composite hole is induced under the same interference level. In comparison with the traditional ForceMate bushing process, a better anti-fatigue performance of cold expanded composite holes can be expected by using the assisting sleeve.
引用
收藏
页码:747 / 762
页数:17
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