Technical Papers
Sep 8, 2023

Development of Miniature Tensile-Test System of Intermediate Strain Rate Based on Electromagnetic Launch

Publication: Journal of Engineering Mechanics
Volume 149, Issue 11

Abstract

To study the dynamic properties of intermediate strain rates for filiform or filmy materials, a miniature tensile-test system with an intermediate strain rate based on magnetic resistance actuation is designed herein. The loading part of the system is formed by inertial movement and an electromagnetic launcher, and the testing part is formed by high-speed optical noncontact measurements using a microforce sensor. Constant tension and intermediate speed are realized by designing the inertial motion of a large-mass combined accelerator. Friction and vibration are offset using magnetic attraction. The electromagnetic acceleration force was eliminated by adjusting the length differences, construction, and relative motion of the structures. The stress–strain curves are obtained by synchronizing the strain signal measured using the optical extensometer method and the stress signal measured using the microforce sensor. The system is verified to be miniature, stable, easy to control, accurate for strain rate, economic, and used for small samples. The stability and reliability of the system are verified using speed testing and motion-state photography. Therefore, the designed system is miniature, easy to control, highly cost-effective, and can be used for filiform or filmy samples.

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Data Availability Statement

All data, models, and code generated or used during the study appear in the published article.

Acknowledgments

This work is financially supported by the National Natural Science Foundation of China (11972084) and the National Science and Technology Major Project (2017-VI-0003-0073).

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Information

Published In

Go to Journal of Engineering Mechanics
Journal of Engineering Mechanics
Volume 149Issue 11November 2023

History

Received: Jan 15, 2023
Accepted: Jul 12, 2023
Published online: Sep 8, 2023
Published in print: Nov 1, 2023
Discussion open until: Feb 8, 2024

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Su Cai
School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, China.
Chitao Zhang
School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, China.
Zhanwei Liu [email protected]
Professor, School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, China (corresponding author). Email: [email protected]
Xiaoming Wang
School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, China.

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