An Experimental Study of Installing-Holes Parameter Optimization for Metallic Inserts Bonded into CFRP Laminates

DOI

10.2991/icmse-15.2015.274How to use a DOI?

Keywords

installing-holes; metallic inserts; bonded; CFRP laminates

Abstract

CFRP laminates are used for various aircraft structural components because of their good mechanical and physical properties. Metallic inserts are one kind of aerospace fasteners, which are usually installed in the metallic components by an interference fit. However, when metallic inserts are installed in the CFRP laminates by the traditional installing way, delamination and low efficiencies are troublesome. Therefore, excellent quality and cost effective installing metallic inserts into the CFRP laminates remains a challenge. In this paper, a series of experiments were carried out to study the installing-holes parameter optimization for metallic inserts bonded into the CFRP laminates. The experimental results show that the push-out values and breakaway torque values of metallic inserts bonded in the CFRP laminates are not reduced obviously for 4 different type installing-holes.

Copyright

© 2015, the Authors. Published by Atlantis Press.

Open Access

This is an open access article distributed under the CC BY-NC license (http://creativecommons.org/licenses/by-nc/4.0/).

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TY  - CONF
AU  - Jing Liu
AU  - Xuemei Chen
AU  - Hui Zhang
AU  - Jing Xu
AU  - Fengtao He
AU  - Kun Hou
AU  - Zhenbo Yin
PY  - 2015/12
DA  - 2015/12
TI  - An Experimental Study of Installing-Holes Parameter Optimization for Metallic Inserts Bonded into CFRP Laminates
BT  - Proceedings of the 2015 6th International Conference on Manufacturing Science and Engineering
PB  - Atlantis Press
SP  - 1522
EP  - 1527
SN  - 2352-5401
UR  - https://doi.org/10.2991/icmse-15.2015.274
DO  - 10.2991/icmse-15.2015.274
ID  - Liu2015/12
ER  -