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Validity check of an analytical dimensioning approach for potted insert load introductions in honeycomb sandwich panels

机译:蜂窝夹芯板中引入的盆栽嵌件载荷的分析尺寸确定方法的有效性检查

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An easy to handle mechanical-analytical dimensioning approach for insert load introductions on sandwich panels with honeycomb cores is of great value, since remarkable weight reductions can be achieved if the diameters of all inserts in a structure are reduced to their inevitable minimum. This is of special interest for mass critical structures of e.g. satellites, airplanes or race cars. For these structures, a combination of core connected (i.e. potted), through-the-thickness inserts in sandwich panels with fiber reinforced face sheets and aluminum honeycomb core material is frequently in use, since it offers an outstand lightweight performance. Unfortunately, a straight forward, mechanical-analytical dimensioning approach, especially for this particular insert-sandwich combination, is still missing.An analytical-mechanical model, basing on the higher order sandwich theory, was developed by Ericksen in 1953 for inserts without a connection to the core (i.e. clamped between the face sheets). In 1981, Hertel modified Ericksen’s model in order to achieve more convenient to use solution equations. However, Hertel used his modified model also for strength predictions of core connected inserts, although the core shear stress progression, decisive for the strength of an insert, differs highly from clamped inserts. However, since Hertel did not validate his extension of the modified Ericksen model onto core-connected inserts in any way, the authors suspect a misunderstanding. Unfortunately, the model was used frequently for core connected inserts afterwards and is even cited in a standard reference published by ESA and ECSS.To address this uncertainty, the authors carried out a comparison of experimental results to the predictions of the modified Ericksen model for core connected inserts within this work. Therefore, initially a cumulated overview of the Ericksen model and Hertel’s modifications is provided, since this is not available in literature. Included are current approaches for the homogenization of the anisotropic FRP- and honeycomb material properties in order to receive moat precise results.The comparison of experimental and analytical results offers mostly a poor correspondence in terms of the strength of an core connected insert. This, on one hand, reveals that the modified Ericksen formulation is not applicable on core connected inserts without significant restrictions in contrast to Hertel’s assumption. Moreover, it also becomes apparent that the various state-of-the-art test data interpretations deliver widely diverging results for the strength of an insert load introduction. Consequently, the analytical dimensioning of core connected inserts remains unreliable. Yet, this investigation derives useful improvement measures on both, theoretical and practical side.
机译:一种易于操作的机械分析尺寸确定方法,可将具有蜂窝芯的夹心板引入嵌件负载,具有巨大的价值,因为如果将结构中所有嵌件的直径减小到不可避免的最小值,则可以显着减轻重量。这对于例如硅藻土的质量关键结构特别有意义。卫星,飞机或赛车。对于这些结构,由于夹芯板具有出色的轻便性能,因此经常使用夹芯板连接的芯(即,盆状),厚板插入式夹芯板和纤维增强面板以及铝蜂窝芯材料的组合。不幸的是,仍然缺少一种简单的机械-分析尺寸标注方法,尤其是对于这种特殊的刀片-三明治组合而言.1953年,Ericksen针对高连接性的刀片建立了基于高阶三明治理论的解析-机械模型。到核心(即夹在面板之间)。 1981年,Hertel修改了Ericksen的模型,以便更方便地使用解方程。但是,Hertel也使用他的改进模型对核心连接刀片的强度进行了预测,尽管决定刀片强度的核心剪切应力变化与夹紧刀片有很大不同。但是,由于Hertel并未以任何方式验证他对修改后的Ericksen模型在核心连接刀片上的扩展,因此作者怀疑存在误解。不幸的是,此模型后来被频繁用于芯连接插入件,甚至在ESA和ECSS发布的标准参考文献中被引用。为解决这种不确定性,作者对实验结果与改进的Ericksen芯模型进行了比较这项工作中的连接插件。因此,最初提供了Ericksen模型和Hertel的修改的累积概述,因为这在文献中是不可用的。为了获得护城河精确的结果,目前包括使FRP和蜂窝材料各向异性的材料均质化的现有方法。实验和分析结果的比较在核心连接插入物的强度方面几乎没有很好的对应关系。一方面,这表明,与Hertel的假设相比,修改后的Ericksen公式在没有明显限制的情况下不适用于核心连接刀片。此外,显而易见的是,各种最新的测试数据解释为插入载荷引入的强度提供了截然不同的结果。因此,芯连接插件的分析尺寸仍然不可靠。然而,这项研究从理论和实践两方面都得出了有用的改进措施。

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