首页> 外文会议>International astronautical congress >EMPIRICAL EVALUATION OF THERMAL CONTACT RESISTANCE OF BOLTED JOINT CONFIGURATIONS FITTED WITH VARIOUS INTERFACE MATERIALS UNDER VACUUM CONDITIONS
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EMPIRICAL EVALUATION OF THERMAL CONTACT RESISTANCE OF BOLTED JOINT CONFIGURATIONS FITTED WITH VARIOUS INTERFACE MATERIALS UNDER VACUUM CONDITIONS

机译:真空条件下结合各种界面材料的螺栓连接构型的热接触电阻的实证评估

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This paper presents the results of the experiments conducted with two different test setups, representing the orthodox configurations of bolted joints and structural geometries in wide usage for space applications, to evaluate the thermal contact resistance across abovementioned joints when fitted with various polymeric gaskets and RTV silicone compounds and subjected to heat flux in vacuum conditions. The test subjects include a special bolt and washer configuration frequently employed in spacecraft designs and not studied comprehensively hitherto, in the form of two Al-6065 and Al-7071 specimen bolted together with interface materials between the two aluminum sheets and flat and spring washers inserted between the bolt heads and the upper plate and nuts and the bottom plate. The mentioned assembly is sandwiched between a copper and an aluminum slab, on the top of which the heater is installed. The whole configuration is covered with a MLI blanket and is attached to the base plate of a thermally conditioned vacuum chamber. The second test subject represents a more complex geometry comprising a hollow aluminum box with a hatch connected to the top of the box, and another aluminum plate to which the bottom of the box is jointed. The lower aluminum plate is in turn connected to an aluminum slab and thermal filler materials are inserted between the interface of the aluminum plate and the slab. An electrical heater is mounted on the top of the box and again, the whole setup is installed in the vacuum chamber. The effects of filler parameters like thickness on thermal contact resistance are studied and the results are discussed. These series of tests are designed to facilitate selection of the best performing-value for money- thermal fillers in these specific configurations for thermal control engineers in practical cases.
机译:本文介绍了使用两种不同测试设置进行的实验结果,这些测试设置代表了在空间应用中广泛使用的螺栓接头的正统配置和结构几何形状,以评估在安装了各种聚合物垫片和RTV硅酮时上述接头之间的热接触电阻化合物并在真空条件下经受热通量。测试对象包括特殊的螺栓和垫圈配置,该配置经常在航天器设计中使用,并且迄今尚未进行全面研究,以两个Al-6065和Al-7071标本的形式用螺栓固定在一起,两个铝板之间的接口材料以及插入的平垫和弹簧垫圈在螺栓头和上板之间以及螺母和底板之间。所述组件被夹在铜和铝板之间,在铜板和铝板的顶部安装了加热器。整个配置都覆盖有MLI橡皮布,并固定在经过热调节的真空室的底板上。第二个测试对象表示一个更复杂的几何形状,包括一个中空的铝制盒子,其上的阴影线连接到盒子的顶部,另一个铝板连接到盒子的底部。下铝板又连接到铝板,并且将热填充材料插入铝板和板的界面之间。电加热器安装在盒子的顶部,再次将整个装置安装在真空室中。研究了诸如厚度之类的填料参数对热接触电阻的影响,并讨论了结果。这些系列的测试旨在帮助在实际情况下为热控制工程师选择这些特定配置中的金钱热填充物最佳性能值。

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