• Title/Summary/Keyword: 드랍 케리지

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Development and Application of Drop Impact Tester for Aerospace Structures (항공우주구조물 낙하충격시험기 개발 및 응용)

  • Yesol Shin;Hyejin Kim;Juho Lee
    • Journal of Aerospace System Engineering
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    • v.18 no.3
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    • pp.56-64
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    • 2024
  • In this study, a drop impact tester was developed to comprehensively conduct basic testing and academic research on the drop impact characteristics of aerospace structures. A drop tester enables accurate assessment of the dynamic stresses and deformations that occur when an aircraft collides with the ground, thereby enabling the verification of important design factors, such as safety and mechanical strength. The drop tester consists of an electromagnet to attach and drop the test object, a crane to adjust the drop height of the test object, and a drop support structure for vertical drops. Numerical analysis of the drop test object for the test was performed, and basic tests were performed using the drop impact tester. Through the analysis and test results, the structural shape of the landing gear was analyzed, and the behavior of each part was evaluated.