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问题的提出随着空间技术的发展,为保持飞行器的尺寸和重量,在飞船和长寿命的通信卫星的设计中,通常是使能流密度愈来愈大。对于这样高的能量输出,在电子设备中将产生大量的废热。此时,欲使飞行器内部的温度仍能维持在一定的范围之内,就必须排出这些热量,为此须在蒙皮与热源之间建立适当的导热通路。这样一来,就要求仔细地研究相接触表面
PROBLEM PROBLEMS With the development of space technology, in order to maintain the size and weight of aircraft, the design of spacecraft and long-lived communication satellites is usually enabled to increase the density of the flow. For such a high energy output, a large amount of waste heat will be generated in the electronic equipment. At this time, to maintain the temperature inside the aircraft within a certain range, it is necessary to discharge the heat, for which an appropriate thermal conduction path must be established between the skin and the heat source. As a result, careful study of the contact surfaces is required