摘要
双储液器环路热管的独特设计可以解决常规单储液器环路热管地面重力场中运行姿态受限的问题,拓展常规环路热管的应用领域。对双储液器环路热管在3种特定姿态下的稳态运行特性进行了实验研究,验证了双储液器环路热管即使在最为苛刻的姿态下仍可正常运行的能力。通过对实验结果的分析可得:双储液器环路热管在重力辅助姿态下的工作温度偏低是由系统外回路压降变化引起的;可变热导区内工作温度随热载荷的变化是由控温储液器的能量平衡所决定。此外,实验发现双储液器环路热管在热载荷递增和递减过程会出现温度迟滞现象。
A dual compensation chamber loop heat pipe is developed to solve the problem of relative orientation limit of the conventional loop heat pipes operating in ground environment and extend the application domain of conventional loop heat pipes.The steady-state operating characteristics at three typical orientations are investigated,and the operating ability of the dual compensation chamber loop heat pipe at the most severe orientation is demonstrated by experiments.Analysis of the experimental results shows that the operating temperature is lower at gravity-assisted orientation than other orientations and this phenomenon is caused by the pressure drop change of the external loop.The operating temperature variation with different heat load is determined by the energy conservation of the compensation chambers.In addition,the temperature hysteresis phenomena are found in the heat load step increase and decrease process in the experiments.
出处
《航空学报》
EI
CAS
CSCD
北大核心
2010年第8期1558-1564,共7页
Acta Aeronautica et Astronautica Sinica
基金
国家自然科学基金(50676006)
北京航空航天大学博士研究生创新基金
关键词
环路热管
双储液器
运行特性
温度控制
loop heat pipes
dual compensation chambers
operating characteristics
temperature control