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Study on Mechanical Properties of Submunition’s Ribbon Straightening Section

机译:提交式色带矫直部分力学性能研究

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摘要

The humanitarian damage caused by the unexploded submunitions is one of the hot issues of concern to the international community at present. A portion of the submunition that did not explode was caused by a break at the connection between the ribbon riveting and the fuze. According to the physical structure of the submunition and the trajectory into which it was ejected, we analyzed the forces of the submunition in flight, deduced the related mathematical models, and clarify the key elements of the mechanics. In this paper, the commercial simulation software was used to calculate the mechanical properties of the ribbon. And the variation regularity between drop velocity and straightening force of ribbon are revealed. And the response characteristics of different material ribbon with different sizes of riveting holes and riveting joints under tensile action were simulated. The simulation results show that, in the trajectory environment with 30 m/s~55 m/s typical stream speed, the tensile force of the ribbon is less than 300 N, and the application concentration of the connecting parts of the riveting joint and the ribbon will not cause the failure of the kevlar ribbon, but it will cause the failure of the nylon ribbon. In order to verify the variation of the tension of kevlar ribbons in different trajectory environments, we designed the experimental scheme of tension test of the ribbon straightening section of submunition and conducted experiments. Experimental results and numerical simulation results revealed the same law. This paper provides effective technical support for solving the problem of unexploded submunitions.
机译:由未爆炸的中断造成的人道主义损害是目前国际社会关注的问题之一。未爆炸的一部分未爆炸的内置是由色带铆接和引信之间的连接处的断裂引起的。根据所提起的物理结构和喷射的轨迹,我们分析了飞行中提出的力量,推导了相关的数学模型,并阐明了力学的关键要素。本文使用了商业仿真软件来计算带的机械性能。揭示了带状速度和矫直力之间的变化规律。和不同尺寸的铆接孔和拉伸接头在拉伸作用下的不同材料带的响应特性进行了模拟。仿真结果表明,在具有30m / s〜55 m / s典型流速度的轨迹环境中,带的拉力小于300n,以及铆接接头的连接部分的施加浓度和铆接色带不会导致凯夫拉里带的失效,但它会导致尼龙带的失效。为了验证不同轨迹环境中Kevlar带的张力的变化,我们设计了提交的带状矫直部分的张力试验的实验方案和进行实验。实验结果和数值模拟结果显示了相同的法律。本文提供了用于解决未爆炸的中产问题的有效技术支持。

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