空间遥感器用环路热管瞬态数值模拟与在轨验证

doi:10.13700/j.bh.1001-5965.2019.0584

北京航空航天大学学报 ›› 2020, Vol. 46 ›› Issue (11): 2045-2055.doi: 10.13700/j.bh.1001-5965.2019.0584

空间遥感器用环路热管瞬态数值模拟与在轨验证

孟庆亮^1,2, 杨涛^1,2, 于志^1,2, 赵振明^1,2, 赵宇^1,2, 于峰^1,2

1. 北京空间机电研究所, 北京 100094;
2. 先进光学遥感技术北京市重点实验室, 北京 100094

收稿日期:2019-11-14 发布日期:2020-12-01
通讯作者: 孟庆亮 E-mail:qlmeng@mail.ustc.edu.cn
作者简介:孟庆亮,男,博士,高级工程师。主要研究方向:微重力下两相流动与传热。
基金资助:
国家自然科学基金（51806010）

Transient numerical simulation and on-orbit verification of loop heat pipe used for space remote sensor

MENG Qingliang^1,2, YANG Tao^1,2, YU Zhi^1,2, ZHAO Zhenming^1,2, ZHAO Yu^1,2, YU Feng^1,2

1. Beijing Institute of Space Mechanics and Electricity, Beijing 100094, China;
2. Beijing Key Laboratory of Advanced Optical Remote Sensing Technology, Beijing 100094, China

Received:2019-11-14 Published:2020-12-01

摘要/Abstract

摘要： 为满足空间遥感器环路热管（LHP）在轨应用需求，建立了高分九号卫星电荷耦合器件（CCD）用LHP瞬态数值模型。模型采用了节点-网络法和流动与传热关系式耦合的方法，考虑了蒸发器与储液器之间的传热传质过程。通过仿真与在轨数据的对比，发现LHP内部组件温度偏差为0.2~0.4℃，冷凝器测点温度偏差为0.5~2.0℃；预热器通过干度的变化调节了冷凝器外热流和热源工作模式的影响；热源的工作模式对蒸发器向储液器漏热、回路流阻及两相段长度均有影响。所提模型可用于不同轨道外热流及热源工作模式下，研究LHP内部各参数的变化规律，预测LHP系统的瞬态工作特性，并指导后续产品的设计与研发。

关键词: 环路热管(LHP), 空间遥感器, 精密控温, 传热传质, 数值模拟

Abstract: For the purpose of meeting the requirement of application on-orbit for Loop Heat Pipe (LHP), a transient numerical model of LHP, which is used for the thermal control of Charge-Coupled Device (CCD) of GF-9 satellite, is developed by using the node-network method and flow and heat transfer relation formula. The processes of heat and mass transfer between evaporator and accumulator are considered. By comparison between simulation and on-orbit results, it is found that the temperature differences are 0.2-0.4℃ and 0.5-2.0℃, for the interior components and condensers, respectively. The influence of orbital external heat flux and working mode of heat source can be adjusted by the degree of dryness in the pre-heater. The heat leak from evaporator to accumulator, flow resistance of loop, and the length of two-phase loop can be affected by the working mode of heat sources. The model can be used to study the variation of LHP interior parameters under different orbital external heat flux and heat source working modes, and predict the transient behavior of LHP system, which can also be used to guide the design and development of subsequent products.

Key words: Loop Heat Pipe (LHP), space remote sensor, precise thermal control, heat and mass transfer, numerical simulation

中图分类号:

V416
TK124

孟庆亮, 杨涛, 于志, 赵振明, 赵宇, 于峰. 空间遥感器用环路热管瞬态数值模拟与在轨验证[J]. 北京航空航天大学学报, 2020, 46(11): 2045-2055.

MENG Qingliang, YANG Tao, YU Zhi, ZHAO Zhenming, ZHAO Yu, YU Feng. Transient numerical simulation and on-orbit verification of loop heat pipe used for space remote sensor[J]. Journal of Beijing University of Aeronautics and Astronautics, 2020, 46(11): 2045-2055.

参考文献

[1] HOLST G C.CCD arrays,cameras,and displays[M].Bellingham:SPIE,1996.
[2] 鲁盼,赵振明,颜吟雪.高分辨率遥感相机CCD器件精密热控制[J].航天返回与遥感,2014,35(4):59-66.LU P,ZHAO Z M,YAN Y X.Precise thermal control of CCD in high resolution remote sensing[J].Spacecraft Recovery & Remote Sensing,2014,35(4):59-66(in Chinese).
[3] 童叶龙,李国强,余雷,等.CCD组件的热分析和热实验[J].航天返回与遥感,2014,35(5):46-53.TONG Y L,LI G Q,YU L,et al.Heat dissipation and precise temperature control for high-power CCD assembly[J].Spacecraft Recovery & Remote Sensing,2014,35(5):46-53(in Chinese).
[4] 李春林.空间光学遥感器热控技术研究[J].宇航学报,2014,35(8):863-870.LI C L.Research on space optical remote sensor thermal control technique[J].Journal of Astronautics,2014,35(8):863-870(in Chinese).
[5] 苗建印,张红星,吕巍,等.航天器热传输技术研究进展[J].航天器工程,2010,19(2):106-112.MIAO J Y,ZHANG H X,LV W,et al.Development of heat transfer technologies for spacecraft[J].Spacecraft Engineering,2010,19(2):106-112(in Chinese).
[6] 张畅,谢荣建,张添,等.液氮温区平板蒸发器环路热管实验研究[J].北京航空航天大学学报,2019,45(6):1211-1217.ZHANG C,XIE R J,ZHANG T,et al.Experimental study on a liquid nitrogen temperature region loop heat pipe with flat evaporator[J].Journal of Beijing University of Aeronautics and Astronautics,2019,45(6):1211-1217(in Chinese).
[7] 赵振明,孟庆亮,张焕冬,等.CCD器件用机械泵驱动两相流体回路仿真与实验[J].北京航空航天大学学报,2019,45(5):893-901.ZHAO Z M,MENG Q L,ZHANG H D,et al.Simulation and experimental study of mechanically pumped two-phase loop for CCD[J].Journal of Beijing University of Aeronautics and Astronautics,2019,45(5):893-901(in Chinese).
[8] GAO T,YANG T,ZHAO S L,et al.The design and application of temperature control loop heat pipe for space CCD camera[C]//46th International Symposium of Space Optical Instrument and Application,2017:15-20.
[9] CHUANG P.An improved steady-state model of loop heat pipes based on experimental and theoretical analyses[D].State College:Pennsylvania State University,2003.
[10] KAYA T,PÉREZ R,GREGORI C,et al.Numerical simulation of transient operation of loop heat pipes[J].Applied Thermal Engineering,2008,28(8-9):967-974.
[11] ADONI A,AMBIRAJAN A,JASVANTH V,et al.Thermohydraulic modeling of capillary pumped loop and loop heat pipe[J].Journal of Thermophysics and Heat Transfer,2007,21(2):410-421.
[12] BAI L,LIN G P,ZHANG H X,et al.Mathematical modeling of steady-state operation of a loop heat pipe[J].Applied Thermal Engineering,2009,29(13):2643-2654.
[13] RIVIÉRE N,SARTRE V,BONJOUR J.Fluid mass distribution in a loop heat pipe with flat evaporator[C]//15th International Heat Pipe Conference,2010:hal-00541426.
[14] WRENN K R,ALLEN R D,HOANG T T,et al.Verification of a transient loop heat pipe model:1999-01-2010[R].Warrendale:SAE Technical Paper,1999.
[15] HOANG T,KU J.Transient modeling of loop heat pipes:AIAA-2003-6082[R].Reston:AIAA,2003.
[16] POUZET E,JOLY J L,PLATEL V,et al.Dynamic response of a capillary pumped loop subjected to various heat load transients[J].International Journal of Heat and Mass Transfer,2004,47(10-11):2293-2316.
[17] CULLIMORE B,BAUMANN J.Steady state and transient loop heat pipe modeling:2000-01-2316[R].Warrendale:SAE Technical Paper,2000.
[18] ZINNA S,MARENGO M,MOLINA M.Numerical model of the LHP for the thermal control of the cryomagnet avionic box (CAB) mounted on the AMS-02 experiment[C]//VII Minsk International Seminar "Heat pipes,Heat pumps,Refrigerators,Power Sources",2008:351-359.
[19] XIN G,CHENG Y,LUAN T,et al.Simulation of a LHP-based thermal control system under orbital environment[J].Applied Thermal Engineering,2009,29(13):2726-2730.
[20] 何发龙,杜王芳,赵建福,等.深冷环路热管瞬态数值仿真研究[J].载人航天,2018,24(4):515-519.HE F L,DU W F,ZHAO J F,et al.Study on transient numerical simulation of cryogenic loop heat pipe[J].Manned Spaceflight,2018,24(4):515-519(in Chinese).
[21] KU J T.Operating characteristics of loop heat pipe[C]//29th International Conference on Environmental System,1999:1991-01-2007.
[22] 弗兰克P·英克鲁佩勒,大卫P·德维特,狄奥多尔L·伯格曼,等.传热和传质基本原理[M].葛新石,叶宏,译.北京:化学工业出版社,2011:297-332.INCROPERA F P,DEWITT D P,BERGMAN T L,et al.Fundamentals of heat and mass transfer[M].GE X S,YE H,translated.Beijing:Chemical Industry Press,2011:297-332(in Chinese).
[23] SHAH M M.Prediction of heat transfer during boiling of cryogenics fluids flowing in tubes[J].Cryogenics,1984,24(5):231-236.
[24] CHURCHILL S W.Friction factor equation spans all fluid-flow regimes[J].Chemical Engineering Journal,1977,84(24):91-92.
[25] FRIEDEL L.Improved friction pressure drop correlation for horizontal and vertical two-phase pipe flow[C]//European Two-Phase Flow Group Meeting,1979:485-492.

空间遥感器用环路热管瞬态数值模拟与在轨验证

Transient numerical simulation and on-orbit verification of loop heat pipe used for space remote sensor

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