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首页> 外文期刊>Journal of Sound and Vibration >Analytical calculation of in-plane response of plates with concentrated masses to impact and application to pyroshock simulation
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Analytical calculation of in-plane response of plates with concentrated masses to impact and application to pyroshock simulation

机译:集中质量的板对冲击的平面响应分析计算及其在热震模拟中的应用

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摘要

In aerospace missions pyroshocks occur due to controlled explosions of ordnance devices enabling the functionality of space modules. These shocks result from deployment mechanisms or opening solar sails and can cause failures of electronic devices and structures. Thus, essential components for assuring the reliability of modules are pyroshock tests for the completion of which strict requirements by the aerospace administrations have to be met. One of them is the definition of a specific acceleration signal and, based on this, the Shock Response Spectrum (SRS) for each part. So far, there is rather empirical than analytical knowledge about producing desired SRS with mechanical impacts and its characteristics due to the variation of input parameters. In this paper a widespread testing procedure for far-field pyroshocks is discussed which is realized by the in-plane impact of a hammer pendulum on a plate including the test specimen. The mechanical model consists of the contact between a rigid sphere and a free deformable rectangular plate with attached masses including subsequent propagation and reflection of longitudinal waves. In order to allow for a prediction of the acceleration field and the corresponding SRS due to the impact the problem is solved semi-analytically by using Hertzian contact theory, the Galerkin-procedure and numerical integration in time domain. The in-plane problem has, to the best of the authors knowledge, not yet been treated in the literature in the way presented. The results calculated are compared with experimental data showing very good coincidence and allowing for a fast prediction of far-field pyroshock tests due to the impact excitation by a hammer pendulum. Hence, the framework of this paper is an enrichment for the current state of the art considering analytical pyroshock simulation. By better understanding the effect of pyroshocks to one and two dimensional structures a reduction of costs as well as durations for testing procedures seems promising.
机译:在航空航天任务中,由于军械装置的爆炸性爆炸而产生了电击,使空间模块能够正常工作。这些冲击是由展开机制或打开的太阳帆引起的,并可能导致电子设备和结构发生故障。因此,为确保模块的可靠性,必不可少的组件是热震试验,为完成这些试验,必须满足航空航天管理部门的严格要求。其中之一是特定加速度信号的定义,并基于此定义每个零件的冲击响应谱(SRS)。到目前为止,由于输入参数的变化,对于产生具有机械冲击及其特性的所需SRS而言,还没有经验或分析知识。在本文中,讨论了一种广泛的远场电击测试程序,该程序通过锤子摆在包括测试样品的板上的面内冲击来实现。力学模型包括刚性球体和自由变形的矩形板之间的接触,并带有附加质量,包括随后传播和反射的纵波。为了预测由于碰撞而引起的加速度场和相应的SRS,使用赫兹接触理论,Galerkin过程和时域数值积分对问题进行了半解析求解。就作者所知,面内问题尚未在文献中以提出的方式进行处理。将计算结果与实验数据进行比较,实验数据显示出非常好的一致性,并且由于锤子的冲击激发,可以快速预测远场热震试验。因此,本文的框架充实了考虑分析热震模拟的当前技术水平。通过更好地了解热震对一维和二维结构的影响,降低成本以及测试过程的持续时间似乎是有希望的。

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