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Study of a coupling mechanism between an UHTC Wing Leading Edge and a metallic structure at high temperature values

机译:UHTC机翼前缘与金属结构在高温条件下的耦合机理研究

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In the frame of thermal structures design activities, particular interest covers the choice of the coupling mechanism (bolt material, preload, etc) between bodies characterized by high temperature values. In fact, those high values cause significant thermal expansion of the elements connecting the hot bodies. In particular, when two bodies made of different materials have to be joined, a difference in the thermal expansion will be encountered leading to a loosening of the coupling mechanism. The resulted bolt preload will decrease significantly.The present work illustrates a particular coupling mechanism that is able to maintain a sufficient preload even at very high temperature values. A local model has been considered for the structural analyses. The boundary conditions applied have been retrieved from the global structural analyses results. Structural non-linear analyses by means of Finite Element code ANSYS have been performed.
机译:在热结构设计活动的框架中,特别关注的是选择以高温值为特征的物体之间的耦合机制(螺栓材料,预紧力等)。实际上,这些高值导致连接热体的元件发生明显的热膨胀。特别地,当必须连接由不同材料制成的两个主体时,将会遇到热膨胀的差异,从而导致联接机构的松动。所产生的螺栓预紧力将大大降低。 本工作说明了一种特殊的耦合机制,即使在非常高的温度值下也能保持足够的预紧力。已经考虑了局部模型进行结构分析。应用的边界条件已从全局结构分析结果中检索到。已经通过有限元代码ANSYS进行了结构非线性分析。

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