An Experimental Study of Installing-Holes Parameter Optimization for Metallic Inserts Bonded into CFRP Laminates
- 10.2991/icmse-15.2015.274How to use a DOI?
- installing-holes; metallic inserts; bonded; CFRP laminates
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.
- © 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/).
Cite this article
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 -