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空间发电系统热管式吸热器热性能分析
引用本文:崔海亭,徐伟强,袁修干,朱玉峰. 空间发电系统热管式吸热器热性能分析[J]. 航空动力学报, 2004, 19(3): 351-355
作者姓名:崔海亭  徐伟强  袁修干  朱玉峰
作者单位:河北科技大学,机械与电子工程学院,河北,石家庄,050018;北京航空航天大学,航空科学与工程学院,北京,100083;北京航空航天大学,航空科学与工程学院,北京,100083;河北科技大学,机械与电子工程学院,河北,石家庄,050018
基金项目:国家自然科学基金资助项目(50276001),河北科技大学校立基金资助项目(XL2003055)
摘    要:为了提高吸热器的热性能、降低吸热器的质量,将热管用于空间太阳能热动力发电系统的吸热蓄热器,建立了相应的物理和数学模型,给出了数值求解方法,计算了蓄热容器最高温度、热管最高壁温、工质出口温度、相变材料(PCM)熔化率等参数,并与基本形吸热器进行了对比,验证了PCM的储热能力,减小了工质气体出口温度的波动。计算结果可用于吸热器的设计。 

关 键 词:航空、航天推进系统  太阳能发电  吸热器  热管  热性能
文章编号:1000-8055(2004)03-0351-05
收稿时间:2003-07-02
修稿时间:2003-07-02

Thermal Performance Analysis of Heat Pipe Receiver for Solar Dynamic Space System
CUI Hang-ting,XU Wei-qiang,YUAN Xiu-gan and ZHU Yu-feng. Thermal Performance Analysis of Heat Pipe Receiver for Solar Dynamic Space System[J]. Journal of Aerospace Power, 2004, 19(3): 351-355
Authors:CUI Hang-ting  XU Wei-qiang  YUAN Xiu-gan  ZHU Yu-feng
Affiliation:1.Hebei University of Science and Technology,Shijiazhuang050018,China2.Beijing University of Aeronautics and Astronautics,Beijing100083,China
Abstract:In order to reduce the mass and improve the thermal performance of the heat receiver,heat pipe receiver is used for the space solar dynamic power system.A corresponding mathematical and physical model is built,and a method for numerical solution is given by which the temperature of the containment canister outer wall,heat pipe wall temperature,working fluid exit temperature,liquid Phase Change Material (PCM) fraction of the total heat transfer tube are calculated and compared with those obtained from the baseline heat receiver.The results show it is possible to promote receiver performance,to reduce the fluctuation of working fluid temperature and the weight of heat receiver.All results of the calculations can be used to guide the heat receiver design.
Keywords:aerospace propulsion system  solar dynamic power  heat receiver  heat pipe  thermal performance
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