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Study on an environmental simulation system of low/high temperature for great space

机译:巨大空间低/高温环境模拟系统研究

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An environmental simulation system of low/high temperature for great space that is for a function test on its unfolding structure of some aerials is designed based on air refrigeration principle. According to its practical run at chamber temperature of -70°C, its main parts such as driers, turbines, environmental chamber are investigated. The experiment results show that it is viable to adopting refrigeration way of air turbine for an environmental system of great space simulating low/high temperature. It is not only fulfilled with their temperature demand during those experiments, but also their humidity demand. The subsystem of driers works well and matches with its regeneration, which the wave of dew-point temperature reduces during its switch stage. Meanwhile, the energy is saved. The air turbine could adjust its cooling capacity by itself according to load changes. The pressure of environmental chamber keeps to be about 30~100Pa, so the whole system could run safely, stably and reliably.
机译:基于空气制冷原理设计了对其展开结构的巨大空间的低/高温的环境模拟系统。根据其在-70°C的室温下的实际运行,调查其主要部件,如干燥器,涡轮机,环境室。实验结果表明,采用空中涡轮机的制冷方式可行,用于模拟低/高温的巨大空间的环境系统。在这些实验期间,它不仅满足了它们的温度需求,而且还满足了它们的湿度需求。干燥器子系统良好,并与其再生匹配,露点温度波在其开关阶段期间脱落。同时,能量保存。空气涡轮机可以根据负载变化自身调节其冷却能力。环境室的压力保持在约30〜100pa,因此整个系统可以安全,稳定,可靠地运行。

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