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高空长航时无人机热管理技术发展及挑战

胡沛 黄坤山 何世伟 余长贵 朱晓威

胡沛, 黄坤山, 何世伟, 等. 高空长航时无人机热管理技术发展及挑战[J]. 航空动力学报, 2025, 40(8):20230171 doi: 10.13224/j.cnki.jasp.20230171
引用本文: 胡沛, 黄坤山, 何世伟, 等. 高空长航时无人机热管理技术发展及挑战[J]. 航空动力学报, 2025, 40(8):20230171 doi: 10.13224/j.cnki.jasp.20230171
HU Pei, HUANG Kunshan, HE Shiwei, et al. Development of thermal management technologies for high-altitude long endurance unmanned aerial vehicles: challenges and perspectives[J]. Journal of Aerospace Power, 2025, 40(8):20230171 doi: 10.13224/j.cnki.jasp.20230171
Citation: HU Pei, HUANG Kunshan, HE Shiwei, et al. Development of thermal management technologies for high-altitude long endurance unmanned aerial vehicles: challenges and perspectives[J]. Journal of Aerospace Power, 2025, 40(8):20230171 doi: 10.13224/j.cnki.jasp.20230171

高空长航时无人机热管理技术发展及挑战

doi: 10.13224/j.cnki.jasp.20230171
详细信息
    作者简介:

    胡沛(1990-),男,工程师,硕士,主要从事无人机热管理系统方案设计

    通讯作者:

    朱晓威(1990-),男,教授,博士,主要从事飞行器热管理及高效热质传递技术研究。E-mail:xiaoweizhu@buaa.edu.cn

  • 中图分类号: V279

Development of thermal management technologies for high-altitude long endurance unmanned aerial vehicles: challenges and perspectives

  • 摘要:

    高空长航时无人机需在万米高空持续飞行数十小时,面对极端的低温和低气压环境,其热管理系统必须同时解决电子设备高效散热与关键部件保温防冻的双重难题。主要从高空大气环境、机载设备散热、机舱隔冷和冷凝水处理这几个角度分析论述目前高空长航时无人机热管理系统设计中所面临的技术挑战及相应的应对策略和方案,接着综述了目前可用于发展和改进无人机热管理系统的4个重要子技术方向,即综合热管理系统技术、高效热交换技术、先进数字化设计技术和高效热物性材料技术。研究表明:高空长航时无人机的热管理需实现全机能量动态分配与精确温控的协同优化,这对解决局部过热与过冷的矛盾问题至关重要。该综述的前沿技术进展与工程实践经验,可为推动我国无人机热管理技术的创新发展提供重要参考。

     

  • 图 1  大气温度、压力、密度及绝对湿度随海拔高度的变化曲线

    Figure 1.  Variation profiles of atmospheric temperature, pressure, density and humidity with the altitude

    图 2  RQ-4 无人机机舱增压方案

    Figure 2.  Compartment pressurization scheme of the RQ-4 UVA

    图 3  一种典型的发动机燃油冷却热管理系统构型[19]

    Figure 3.  Typical fuel cooled thermal management system architecture for turbine engine[19]

    图 4  几种航空航天领域常见的保温材料

    Figure 4.  Some commercial thermal insulation materials widely used in aerospace and aviation engineering

    图 5  一种无人机天线罩的结构设计方案[26]

    Figure 5.  Design concept of a sandwich structural radome for UVAs[26]

    图 6  典型的无人机热管理系统结构示意图[30]

    Figure 6.  Typical thermal management system for UVAs[30]

    图 7  一种提高能量利用率的无人机综合热能管理构型工作原理图[31]

    Figure 7.  Conceptual design of UVA’s thermal management system with improved energy efficiency[31]

    图 8  可机载的两相散热系统方案

    Figure 8.  Onboard two-phase heat dissipation systems

  • [1] 向锦武, 阚梓, 邵浩原, 等. 长航时无人机关键技术研究进展[J]. 哈尔滨工业大学学报, 2020, 52(6): 57-77. XIANG Jinwu, KAN Zi, SHAO Haoyuan, et al. A review of key technologies for long-endurance unmanned aerial vehicle[J]. Journal of Harbin Institute of Technology, 2020, 52(6): 57-77. (in Chinese doi: 10.11918/202004009

    XIANG Jinwu, KAN Zi, SHAO Haoyuan, et al. A review of key technologies for long-endurance unmanned aerial vehicle[J]. Journal of Harbin Institute of Technology, 2020, 52(6): 57-77. (in Chinese) doi: 10.11918/202004009
    [2] BORCHARDT J K. Unmanned aerial vehicles spur composites use[J]. Reinforced Plastics, 2004, 48(4): 28-31. doi: 10.1016/S0034-3617(04)00194-8
    [3] ATREYA S, MATA M, JONES R, et al. Power system comparisons for a high altitude long endurance (HALE) remotely operated aircraft (ROA)[R]. AIAA-2005-7401, 2005.
    [4] Department of Defense. Global climatic data for developing military products (MIL-HDBK-310)[R]. Washington, DC, US: Government Printing Office, 1997.
    [5] PHILLIPS A L, WERT K L. Skin As radiator-passive thermal management for high altitude long endurance-UAVs: 1999-01-2501[R].Warrendale: 34th Intersociety Energy Conversion Engineering Conference, 1999.
    [6] FUEGLISTALER S, DESSLER A E, DUNKERTON T J, et al. Tropical tropopause layer[J]. Reviews of Geophysics, 2009, 47(1): 2008RG000267. doi: 10.1029/2008RG000267
    [7] 李德勇, 甘建, 甘学东, 等. 高空长航时无人机工作环境特性[J]. 装备环境工程, 2019, 16(12): 99-103. LI Deyong, GAN Jian, GAN Xuedong, et al. Work environmental characteristics of high altitude long endurance UAV[J]. Equipment Environmental Engineering, 2019, 16(12): 99-103. (in Chinese

    LI Deyong, GAN Jian, GAN Xuedong, et al. Work environmental characteristics of high altitude long endurance UAV[J]. Equipment Environmental Engineering, 2019, 16(12): 99-103. (in Chinese)
    [8] GILMORE M. MQ-9 Reaper armed unmanned aircraft system (UAS): FY-15[R]. Ohio, US: Air Force Wright Patterson Air Force Base United States, 2015.
    [9] BEHLER R F.MQ-9 reaper armed unmanned aircraft system (UAS): FY-17[R]. Ohio, US: Air Force Wright Patterson Air Force Base Unit-ed States, 2017.
    [10] KARAS, R S. USAF Block 5 reaper fleet still facing overheating problems[J]. Inside the Air Force, 2017, 28(39): 1-7.
    [11] 何立臣, 洪元, 杨立明, 等. 有源相控阵雷达天线冷却技术研究进展[J]. 航天器环境工程, 2022, 39(3): 316-325. HE Lichen, HONG Yuan, YANG Liming, et al. Advances in the cooling techniques for active electronically scanned antenna[J]. Spacecraft Environment Engineering, 2022, 39(3): 316-325. (in Chinese

    HE Lichen, HONG Yuan, YANG Liming, et al. Advances in the cooling techniques for active electronically scanned antenna[J]. Spacecraft Environment Engineering, 2022, 39(3): 316-325. (in Chinese)
    [12] 李延伟. 高空无人机载光学遥感器热控技术研究[D]. 长春: 中国科学院研究生院(长春光学精密机械与物理研究所), 2013. LI Yanwei. Research on thermal control technology of altitude optical sensor mounted on unmanned aerial vehicle[D]. Changchun: Changchun Institute of Optics, Fine Mechanics and Physics, Chinese Academy of Sciences, 2013. (in Chinese

    LI Yanwei. Research on thermal control technology of altitude optical sensor mounted on unmanned aerial vehicle[D]. Changchun: Changchun Institute of Optics, Fine Mechanics and Physics, Chinese Academy of Sciences, 2013. (in Chinese)
    [13] 寿荣中, 何慧姗. 飞行器环境控制[M]. 北京: 北京航空航天大学出版社, 2004. SHOU Rongzhong, HE Huishan. Spacecraft optimal control theory and method[M]. Beijing: Beijing University of Aeronautics & Astronautics Press, 2004. (in Chinese

    SHOU Rongzhong, HE Huishan. Spacecraft optimal control theory and method[M]. Beijing: Beijing University of Aeronautics & Astronautics Press, 2004. (in Chinese)
    [14] TALASILA H M. Modular frequency multiplier and filters for the NASA global hawk snow radar[D]. Lawrence: University of Kansas, 2017.
    [15] 杨建忠, 欧阳晶鹏, 陈希远, 等. 多电飞机电动环境控制系统设计研究综述[J]. 航空工程进展, 2022, 13(4): 11-24. YANG Jianzhong, OUYANG Jingpeng, CHEN Xiyuan, et al. Review on design of electric environment control system for more electric aircraft[J]. Advances in Aeronautical Science and Engineering, 2022, 13(4): 11-24. (in Chinese

    YANG Jianzhong, OUYANG Jingpeng, CHEN Xiyuan, et al. Review on design of electric environment control system for more electric aircraft[J]. Advances in Aeronautical Science and Engineering, 2022, 13(4): 11-24. (in Chinese)
    [16] JIANG Hongsheng, DONG Sujun, ZHANG Helin. Energy efficiency analysis of electric and conventional environmental control system on commercial aircraft[C]//2016 IEEE International Conference on Aircraft Utility Systems. Piscataway, US: IEEE, 2016: 973-978.
    [17] LUI C, ARCE E C, BANKS C, et al. Potential technology to unclog hot day operational limit[C]//SAE Technical Paper Series. SAE International, 2010-01-1788.
    [18] LI Dong, HANG Jie, LI Yunhua, et al. Fuel flowrate control for aeroengine and fuel thermal management for airborne system of aircraft: an overview[J]. Applied Sciences, 2022, 12(1): 279.
    [19] SRINATH A N, LÓPEZ Á P, MIRAN FASHANDI S A, et al. Thermal management system architecture for hydrogen-powered propulsion technologies: practices, thematic clusters, system architectures, future challenges, and opportunities[J]. Energies, 2022, 15(1): 304. doi: 10.3390/en15010304
    [20] DOOLEY M, LUI N, NEWMAN R, et al. Aircraft thermal management-heat sink challenge: 2014-01-2193[R].Warrendale:SAE 2014 Aerospace Systems and Technology Conference, 2014.
    [21] HAIR J, BROWELL E, MCGEE T, et al. Development of the global ozone lidar demonstrator (GOLD) instrument for deployment on the NASA global hawk: NF1676L-10529[R]. St. Petersburg: 25th International Laser Radar Conference, 2010.
    [22] KELLERMANN H, HABERMANN A L, HORNUNG M. Assessment of aircraft surface heat exchanger potential[J]. Aerospace, 2020, 7(1): 1.
    [23] 段国晨, 赵景丽, 赵伟超. 先进复合材料在无人机结构的应用[J]. 纤维复合材料, 2022, 39(2): 105-114. DUAN Guochen, ZHAO Jingli, ZHAO Weichao. Application of advanced composite materials in UAV at home and abroad[J]. Fiber Composites, 2022, 39(2): 105-114. (in Chinese doi: 10.3969/j.issn.1003-6423.2022.02.020

    DUAN Guochen, ZHAO Jingli, ZHAO Weichao. Application of advanced composite materials in UAV at home and abroad[J]. Fiber Composites, 2022, 39(2): 105-114. (in Chinese) doi: 10.3969/j.issn.1003-6423.2022.02.020
    [24] ORTEGA C B. Thermal management of electrical systems in a solar-electric stratospheric HALE[R]. AIAA-2022-3271, 2022.
    [25] LAMPERT A, ALTSTÄDTER B, BÄRFUSS K, et al. Unmanned aerial systems for investigating the polar atmospheric boundary layer: technical challenges and examples of applications[J]. Atmosphere, 2020, 11(4): 416. doi: 10.3390/atmos11040416
    [26] CALOMFIRESCU M, NEUMAIER R, KORWIEN T, et al. R&T activities on composite structures for existing and future military A/C platforms at Airbus DS[R]. STO-MP-AVT-267-11, 2018.
    [27] WESTHOFF A, WAGNER C. Experimental study of moist air flow in the gap between the aircraft’s fuselage and its cabin wall[J]. CEAS Aeronautical Journal, 2020, 11(3): 591-607. doi: 10.1007/s13272-020-00440-3
    [28] ZHANG Tengfei, LI Guohui, LIN C H, et al. Measured moisture accumulation in aircraft walls during simulated commercial flights[J]. Science and Technology for the Built Environment, 2018, 24(8): 820-829. doi: 10.1080/23744731.2018.1430973
    [29] 于广民, 王奉明, 卢娟. 高空长航时无人机用发动机推力需求及技术特点分析[J]. 燃气涡轮试验与研究, 2021, 34(6): 41-46, 55. YU Guangmin, WANG Fengming, LU Juan. Analysis of engine requirements and technical characteristics for high altitude long endurance UAV[J]. Gas Turbine Experiment and Research, 2021, 34(6): 41-46, 55. (in Chinese doi: 10.3969/j.issn.1672-2620.2021.06.009

    YU Guangmin, WANG Fengming, LU Juan. Analysis of engine requirements and technical characteristics for high altitude long endurance UAV[J]. Gas Turbine Experiment and Research, 2021, 34(6): 41-46, 55. (in Chinese) doi: 10.3969/j.issn.1672-2620.2021.06.009
    [30] MEHTA J, CHARNESKI J, WELLS P. Unmanned aerial systems (UAS) thermal management needs, current status, and future innovations[R]. AIAA-2012-4051, 2012.
    [31] 马慧才, 刘毅玲, 党晓民. 高空长航时无人机综合热能管理的构型分析[J]. 化工学报, 2020, 71(增刊1): 417-424. MA Huicai, LIU Yiling, DANG Xiaomin. Configuration analysis of integrated thermal management about high altitude long-endurance unmanned aerial vehicle[J]. CIESC Journal, 2020, 71(Suppl. 1): 417-424. (in Chinese

    MA Huicai, LIU Yiling, DANG Xiaomin. Configuration analysis of integrated thermal management about high altitude long-endurance unmanned aerial vehicle[J]. CIESC Journal, 2020, 71(Suppl. 1): 417-424. (in Chinese)
    [32] SHARAR D, JANKOWSKI N R, MORGAN B. Review of two-phase electronics cooling for army vehicle applications: ARL-TR-5323 [R]. Maryland, US: Army Research Laboratory, 2010.
    [33] PARK C, VALLURY A, PEREZ J. Advanced hybrid cooling loop technology for high performance thermal management[R]. AIAA-2006-4059, 2006.
    [34] NORTHCUTT B, MUDAWAR I. Enhanced design of cross-flow microchannel heat exchanger module for high-performance aircraft gas turbine engines[J]. Journal of Heat Transfer, 2012, 134(6): 061801. doi: 10.1115/1.4006037
    [35] STRUMPF H, MIRZA Z. Development of a microchannel heat exchanger for aerospace applications[C]// Proceedings of the ASME 10th international conference on nanochannels, microchannels and minichannels. New York: American Society of Mechanical Engineers, 2013: 459-467.
    [36] SALTZMAN D, BICHNEVICIUS M, LYNCH S, et al. Design and evaluation of an additively manufactured aircraft heat exchanger[J]. Applied Thermal Engineering, 2018, 138: 254-263. doi: 10.1016/j.applthermaleng.2018.04.032
    [37] WROBEL R, SCHOLES B, HUSSEIN A, et al. A metal additively manufactured (MAM) heat exchanger for electric motor thermal control on a high-altitude solar aircraft-experimental characterisation[J]. Thermal Science and Engineering Progress, 2020, 19: 100629. doi: 10.1016/j.tsep.2020.100629
    [38] KAUR I, SINGH P. State-of-the-art in heat exchanger additive manufacturing[J]. International Journal of Heat and Mass Transfer, 2021, 178: 121600. doi: 10.1016/j.ijheatmasstransfer.2021.121600
    [39] PHILLIPS A L, GERNERT N J. Passive aircraft anti icing system using waste heat[C]// International Conference On Environmental Systems. Warrendale: SAE International, 1998: 981542.
    [40] PAGNONI F, AYEL V, BERTIN Y, et al. Loop heat pipe for thermal management of aircraft engine equipment[J]. Journal of Thermophysics and Heat Transfer, 2021, 35(2): 323-334. doi: 10.2514/1.T6049
    [41] 刘晓红, 崔二光. 某无人机SAR天线系统的热设计[J]. 电子机械工程, 2014, 30(3): 12-15. LIU Xiaohong, CUI Erguang. Thermal design of the SAR antenna of an unmanned aerial vehicle[J]. Electro-Mechanical Engineering, 2014, 30(3): 12-15. (in Chinese doi: 10.3969/j.issn.1008-5300.2014.03.005

    LIU Xiaohong, CUI Erguang. Thermal design of the SAR antenna of an unmanned aerial vehicle[J]. Electro-Mechanical Engineering, 2014, 30(3): 12-15. (in Chinese) doi: 10.3969/j.issn.1008-5300.2014.03.005
    [42] SU Qian, CHANG Shinan, ZHAO Yuanyuan, et al. A review of loop heat pipes for aircraft anti-icing applications[J]. Applied Thermal Engineering, 2018, 130: 528-540. doi: 10.1016/j.applthermaleng.2017.11.030
    [43] 陈刘忠. 无人机综合热管理系统建模与仿真[D]. 南京: 南京航空航天大学, 2016. CHEN Liuzhong. The modeling and simulation of UAV integrated thermal management system [D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2016. (in Chinese

    CHEN Liuzhong. The modeling and simulation of UAV integrated thermal management system [D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2016. (in Chinese)
    [44] 汪思齐. 无人机燃油-环控系统热管理研究[D]. 南京: 南京航空航天大学, 2019. WANG Siqi. Research on thermal management of UAV fuel and environmental control system[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2019. (in Chinese

    WANG Siqi. Research on thermal management of UAV fuel and environmental control system[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2019. (in Chinese)
    [45] 高峰, 朱德润. 太阳能无人机热管理系统设计及优化[J]. 制冷与空调, 2016, 16(11): 32-37. GAO Feng, ZHU Derun. Design and optimization of thermal management system for solar unmanned aerial vehicle[J]. Refrigeration and Air-Conditioning, 2016, 16(11): 32-37. (in Chinese doi: 10.3969/j.issn.1009-8402.2016.11.008

    GAO Feng, ZHU Derun. Design and optimization of thermal management system for solar unmanned aerial vehicle[J]. Refrigeration and Air-Conditioning, 2016, 16(11): 32-37. (in Chinese) doi: 10.3969/j.issn.1009-8402.2016.11.008
    [46] 周旭, 姜春英, 李胜宇, 等. 机载综合热管理系统控制特性分析[J]. 航空动力学报, 2022, 37(3): 511-522. ZHOU Xu, JIANG Chunying, LI Shengyu, et al. Analysis of control characteristics of airborne integrated thermal management system[J]. Journal of Aerospace Power, 2022, 37(3): 511-522. (in Chinese

    ZHOU Xu, JIANG Chunying, LI Shengyu, et al. Analysis of control characteristics of airborne integrated thermal management system[J]. Journal of Aerospace Power, 2022, 37(3): 511-522. (in Chinese)
    [47] HERBER D R, ALLISON J T, BUETTNER R, et al. Architecture generation and performance evaluation of aircraft thermal management systems through graph-based techniques[R]. AIAA-2020-0159, 2020.
    [48] VEYDT A. System level thermal hydraulic performance of water-based and PAO-based alumina nanofluids[D]. Dayton: University of Dayton, 2010.
    [49] MATHEW J, KRISHNAN S. A review on transient thermal management of electronic devices[J]. Journal of Electronic Packaging, 2021, 144(1): 010801.
    [50] PAL D, JOSHI Y K. Thermal management of an avionics module using solid-liquid phase-change materials[J]. Journal of Thermophysics and Heat Transfer, 1998, 12(2): 256-262. doi: 10.2514/2.6329
    [51] LI Yongtong, GONG Liang, XU Minghai, et al. A review of thermo-hydraulic performance of metal foam and its application as heat sinks for electronics cooling[J]. Journal of Electronic Packaging, 2021, 143(3): 030801. doi: 10.1115/1.4048861
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  • 收稿日期:  2023-03-22
  • 网络出版日期:  2025-05-29

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