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
Abstract
Jianfeng Wang, Liang Ding, Baoyu Song, Yiqun Liu, Pei Zhong Zhao, Yajing Xie, Haibo Gao
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.
OpenAlex reports 3 citations for this work. Citation counts describe recorded attention and do not establish research quality.
A contribution statement is not available in the OpenAlex record.
Method details are not available in the OpenAlex metadata.
Findings are not separately available in the OpenAlex metadata.
Limitations are not available in the OpenAlex metadata.
Application details are not available in the OpenAlex metadata.
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