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Experimental analysis and numerical simulation of a fuel tank filler in a crash environment

机译:碰撞环境中燃料箱填料的实验分析与数值模拟

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The work presented is part of a research on passive solutions that can limit fire risks in the case of aircraft crash events. Particularly, the development of metallic fillers, such as Explosafe~®, has recently awakened much interest because of the small weight and volume that they occupy in the fuel tank. In the previous phase of the work, impact tests on a helicopter fuel tank filled with water and the above mentioned filler have been carried out. A reduction of the fluid pressure and the overall stresses in the fuel tank have been observed. However, at that stage it was not possible to realize a well-correlated numerical model because the code used did not take into account inertial loads which are prevalent in impact scenarios. The commercial Abaqus software has been used in a consolidation analysis of porous media (*soils). A new model has been set up and an acceleration temporal history, obtained by experimental tests, has been imposed on all the elements, forcing the program to take into account the inertial loads as well. Results are encouraging and a good correlation has been achieved: the highest pressure value is reached. Some errors due to high Explosafe~® permeability and to validity limits of the porous media theory do persist. The stress distribution, transmitted by the fluid to the fuel tank, are coherent with the experimental data.
机译:所呈现的工作是关于无源解决方案的研究的一部分,可以在飞机碰撞事件的情况下限制火灾风险。特别是,由于它们在燃料箱中占据的小重量和体积,最近令人利益,如Explosafe〜®等金属填料的发育。在上一阶段的工作中,已经进行了充满水和上述填料的直升机燃料箱上的冲击试验。已经观察到减少流体压力和燃料箱中的整体应力。然而,在该阶段,不可能实现一个良好相关的数值模型,因为所用的代码没有考虑在影响方案中普遍存在的惯性负载。商业ABAQUS软件已用于多孔介质(*土壤)的合并分析。已经建立了一个新的模型,并通过实验测试获得的加速时间历史,并对所有要素施加,强迫该计划也考虑到惯性负载。结果令人鼓舞,实现了良好的相关性:达到最高压力值。由于高Explosafe〜®渗透率和多孔介质理论的有效性限制,一些误差确实存在。由流体向燃料箱传递的应力分布与实验数据相干。

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