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Mechanical Issues of FIREX Target under Cryogenic Environment

机译:低温环境下FIREX目标的机械问题

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A typical FIREX target is assembled with a 500 μm diameter PS shell, a glass fill tube and a gold cone guide. Each part is glued together by an epoxy resin. To date, several assembled targets have been cooled down to cryogenic environment. However, they could not survive a cool down process and appeared to rupture around the glued boundary between the PS shell and cone guide. To reveal a crucial factor of the target destruction, its thermal stress after cool down was calculated using the ANSYS code. A two dimensional axisymmetric calculation model is composed of the PS shell and cone guide glued by an epoxy resin which is covered on by an epoxy fillet. A cool down process from 293 K to 10 K was simulated. The calculation showed that the rupture of the shell would start from the PS shell and gold cone guide boundary and the target validity depended on how the epoxy fillet could reinforce the PS shell.
机译:典型的FIREX靶标配有直径为500μm的PS外壳,玻璃填充管和金锥导向器。每个部分都用环氧树脂粘合在一起。迄今为止,已经将几个组装好的靶冷却到低温环境。但是,它们无法在冷却过程中幸存下来,并且似乎在PS外壳和圆锥导向器之间的粘合边界周围破裂。为了揭示目标破坏的关键因素,使用ANSYS代码计算了冷却后的目标热应力。二维轴对称计算模型由PS壳体和由环氧树脂胶粘的圆锥形导板组成,并用环氧树脂圆角覆盖。模拟了从293 K到10 K的冷却过程。计算表明,壳体的破裂将从PS壳体和金锥导向边界开始,目标有效性取决于环氧圆角如何增强PS壳体。

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