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DESIGN OF AN ANTI-IMPACT STRUCTURE IN A CERTAIN FUZE

机译:一定引信中的抗冲击结构设计

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The fuze installed in the missile withstands all kinds of impact loading during the throw, cutting the shell, explosive separation, etc. The design of an anti-impact structure has been drawing much attention in the fuze field. The fuze under high impact-3000g and frequency-8000Hz is studied in this paper. Under such strong impact loading, the fuse often breaks down and loses its original function. At first, one protective structure is designed. Secondly, the finite element simulation model is established. Based on this model, the modal analysis is carried out to simulate the natural frequency value. The stresses of the fuze are analyzed under impact loading. The analysis results show that the max stress of the structure is less than the ultimate tensile strength of the material. Thirdly, impact response spectrum experiments are executed and verify that the fuze structure meets the test conditions of environmental impact.
机译:在导弹中安装的引信可承受各种冲击载荷,在抛出,切割壳,爆炸性分离等。抗冲击结构的设计在引信领域的关注很大。本文研究了高影响力-3000G和频率-8000Hz的引信。在这种强烈的冲击载荷下,保险丝经常分解并失去其原始功能。首先,设计了一种保护结构。其次,建立了有限元仿真模型。基于该模型,执行模态分析以模拟自然频率值。在冲击载荷下分析引信的应力。分析结果表明,该结构的最大应力小于材料的极限拉伸强度。第三,执行影响响应谱实验,并验证引信结构是否符合环境影响的测试条件。

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