跳到主要导航 跳到搜索 跳到主要内容

Tensile properties of a composite–metal single-lap hybrid bonded/bolted joint

  • Xiaoqi LI
  • , Xiaoquan CHENG*
  • , Yujia CHENG
  • , Zhiyong WANG
  • , Wenjun HUANG
  • *此作品的通讯作者
  • Beihang University
  • Ltd.
  • China Helicopter Research and Development Institute

科研成果: 期刊稿件文章同行评审

摘要

Hybrid bonded/bolted (HBB) joint has been widely used in engineering practice because it can overcome the potential weakness of pure bonded and pure bolted joints. However, studies on HBB joint are still at the initial stage. In this paper, tensile properties of a composite–metal single-lap HBB joint was investigated experimentally. And a detailed finite element model (FEM) was established to simulate the tensile behavior of the joint. The model was verified by the experimental results. Then the damage propagation and load transfer mechanism were explored based on the FEM. The results show that the HBB joint can provide multi-load transmission paths and resist damage propagation in the adhesive. The HBB joint has higher strength and energy absorption capacity than the pure bonded joint. And the HBB joint has greater initial damage load and tensile stiffness than pure bolted joint. Adhesive fillets can obviously improve the tensile performances of the HBB joint. Lateral stiffness of the joint boundary and testing machine show obvious effects on tensile performances of single-lap hybrid joints.

源语言英语
页(从-至)629-640
页数12
期刊Chinese Journal of Aeronautics
34
2
DOI
出版状态已出版 - 2月 2021

指纹

探究 'Tensile properties of a composite–metal single-lap hybrid bonded/bolted joint' 的科研主题。它们共同构成独一无二的指纹。

引用此