Loop heat pipe(LHP) is the most advanced heat-transfer device in the spacecraft thermal-control field
and dual compensation chamber LHP(DCC-LHP) has become hot spot in the aero and ground applications since it can work without the limit of the orientation between the evaporator and compensation chamber.In this paper
the state-of-the-art investigation on ground-experiments of LHPand DCC-LHPhad been analyzed;the visualized experiments' results had been summarized;due to the investigative deficiencies in some aspects of the heat-transfer mechanism and circulating behaviors in LHP
more visualized experiments should be carried out for the steady-state
transient performance and active thermal-control characteristics
and the visualized validation should be made to previous theories and assumptions.
Adverse effect of non-condensable gas on the operating performance of loop heat pipe
Theoretical analysis of steady-state operating characteristics of a cryogenic loop heat pipe
考虑多源不确定性的复合材料风扇叶片高周疲劳失效概率评估
基于三维接触摩擦单元的套齿连接解析建模研究
与发动机匹配的旁路式双喉道气动矢量喷管数值模拟研究
Related Author
HE Jiang
LIN Gui-ping
BAI Li-zhan
MIAO Jian-yin
ZHANG Hong-xing
BAI Li-zhan
LIN Gui-ping
Related Institution
Laboratory of Fundamental Science on Ergonomics and Environment Control, School of Aeronautic Science and Engineering, Beijing University of Aeronautics and Astronautics
Beijing Key Laboratory of Space Thermal Control Technology, Beijing Institute of Spacecraft System Engineering, China Academy of Space Technology
School of Aeronautic Science and Engineering, Beijing University of Aeronautics and Astronautics