2015•Journal of Reinforced Plastics and CompositesRequires access

Effect of size and shape of joining insert on the strength of sandwich-structured laminate panels for wheeled vehicle’s body

Jianfeng Wang, Liang Ding, Baoyu Song, Yiqun Liu, Pei Zhong Zhao, Yajing Xie, Haibo Gao

Open publisher page 3 citations

Abstract

For automobile applications, sandwich-structured materials are used for thin components that are subjected to relatively small loadings. Other components are usually assembled onto the sandwich panels. In order to ensure adequate connection strength, joining inserts are added to the structures. The joining insert and honeycomb core are connected by adhesives and are used to connect the sandwich structure with the other components. In this work, tensile tests were performed on four different types of inserts for sandwich panels. The ultimate loads of inserts with different shapes and sizes are measured to determine the effect of the insert design on panel strength. The experimental results show that the regular hexagonal shaped has the most influence on the ultimate load.

About this research paper

What this paper is about

For automobile applications, sandwich-structured materials are used for thin components that are subjected to relatively small loadings. Other components are usually assembled onto the sandwich panels. In order to ensure adequate connection strength, joining inserts are added to the structures. The joining insert and honeycomb core are connected by adhesives and are used to connect the sandwich structure with the other components. In this work, tensile tests were performed on four different types of inserts for sandwich panels. The ultimate loads of inserts with different shapes and sizes are measured to determine the effect of the insert design on panel strength. The experimental results show that the regular hexagonal shaped has the most influence on the ultimate load.

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Available abstract

For automobile applications, sandwich-structured materials are used for thin components that are subjected to relatively small loadings. Other components are usually assembled onto the sandwich panels. In order to ensure adequate connection strength, joining inserts are added to the structures. The joining insert and honeycomb core are connected by adhesives and are used to connect the sandwich structure with the other components. In this work, tensile tests were performed on four different types of inserts for sandwich panels. The ultimate loads of inserts with different shapes and sizes are measured to determine the effect of the insert design on panel strength. The experimental results show that the regular hexagonal shaped has the most influence on the ultimate load.

Key concepts: Insert (composites), Sandwich-structured composite, Materials science, Composite material, Ultimate tensile strength, Honeycomb structure, Core (optical fiber), Honeycomb

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