准一维传热下冷面绝热边界材料对隔热试验结果的影响
作者:
作者单位:

1.北京航天长征飞行器研究所,北京 100076;2.航天材料及工艺研究所,北京 100076

中图分类号:

V416.5


Effect of Cold Surface Adiabatic Boundary Material on Thermal Insulation Test Under Quasi-one-dimensional Heat Transfer
Author:
Affiliation:

1.Beijing Institute of Space Long March Vehicle,Beijing 100076;2.Aerospace Research Institute of Materials & Processing Technology,Beijing 100076

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    摘要:

    为评估冷面绝热边界对试验结果的影响,在充分验证测控系统可控性和试验方法稳定性的基础上,分别以柔性隔热毡、刚性隔热瓦和纳米隔热材料为冷面绝热边界,对陶瓷纤维刚性隔热材料进行500 ℃、3 000 s的石英灯热辐射考核试验,并利用迭代绝热边界当量热导率的方法对试验结果进行了模拟计算和分析。结果表明,以柔性隔热毡为冷面绝热边界时隔热材料的冷面温度最高,刚性隔热瓦和纳米隔热材料为冷面绝热边界时则冷面温度较低且相近,3者间最大相对偏差高达19.0%。模拟计算证实由冷面绝热边界材料引起的接触热阻对试验结果起到了决定性作用,而不简单地取决于绝热边界材料的隔热性能。

    Abstract:

    In order to evaluate the influence of cold surface adiabatic boundary, after fully verifying the controllability and the stability of the heat radiation testing system, flexible insulation mat, rigid insulation tile and nano insulation material were used as cold surface insulation boundary respectively. The thermal radiation test of quartz lamp at 500℃ and 3 000 s was carried out, and the test results were simulated and analyzed by using iterative equivalent method. The results show that the cold surface temperature of ceramic fiber rigid insulation material is the highest when flexible insulation mat is used , while the cold surface temperature is lower and similar when rigid insulation tile and nano insulation material are used as the boundary, with maximum relative deviation of 19.0 % between the highest and lowest. Simulation results show that the contact thermal resistance caused by the cold surface insulating boundary material plays a decisive role in tests, rather than simply depending on the insulation performance of the insulating material.

    参考文献
    [1] 王长青.空天飞行技术创新与发展展望[J].宇航学报,2021, 42(7): 807-819.WANG Changqing.technological innovation and development prospect of aerospace vehicle[J]. Journal of Astronautics,2021, 42(7): 807-819.
    [2] 夏吝时,齐斌,张昕,等. 防隔热试验用平板型石英灯加热器热环境分析[J]. 红外技术,2016, 38(7): 617-621.XIA Linshi, QI Bin, ZHANG Xin. The thermal-environment analysis of flat quartz lamp heater system for thermal protection &insulation test[J]. Infrared Technology, 2016, 38(7): 617-621.
    [3] 王晓婷,张宏波,杨海龙等.耐高温隔热材料组合结构模拟研究与试验验证[J].宇航材料工艺,2014,44(1):92-96.WANG Xiaoting,ZHANG Hongbo, YANG Hailong.High temperature resistant heat insulating material simulation and experimental verification[J].Aerospace material & Technology, 2014,44(1):92-96.
    [4] 时圣波,王韧之,严立等.运载火箭尾段防热/承载一体化热防护系统设计及性能分析[J].上海航天,2020,37(4):64-73.SHI Shengbo,WANG Renzhi,YAN Li,et al.Design and property analysis of integrated thermalprotection system for tail cabin of launch vehicle[J].Aerospace Shanghai,2020,37(4): 64-73.
    [5] 吴大方,商兰,高镇同等.1700℃高温、有氧及时变环境下隔热性能试验研究[J].宇航学报,2015,36(9):1083-1092.WU Dafang, SHANG Lan, GAO Zhentong. Experimental research on thermal-insulation performance under high-temperature/oxidation and time-varying environment up to 1700℃[J]. Journal of Astronautics, 2015, 36(9): 1083-1092.
    [6] 吴大方,王峰,任浩源等. 航天器热防护材料不同边界条件下的隔热性能试验研究[J]. 航天器环境工程,2018, 35(4): 315-322.WU Dafang, WANG Feng, REN Haoyuan. Experimental research of thermal insulation performance of thermal protection materials for spacecraft under different boundary conditions [J]. Spacecraft Environment Engineering,2018, 35(4): 315-322.
    [7] 杨景兴,何凤梅,于帆.气凝胶热参数测试及评价[J].宇航材料工艺2013,43(2):92-94.YANG Jingxing, HE Fengmei, YU Fan.Measurement and estimate of thermophysical parameters of aerogel[J]. Aerospace material & Technology, 2013,43(2):92-94.
    [8] Mitsubishi Chemical Corporation. Polycrystalline alumina fiber MAFTEC[EB/OL]. https://www.m-chemical.co.jp/en/products/departments/mcc/maf-metal/product/1201261_7532.html2022-2-10.
    [9] 孙晶晶,胡子君,吴文军,等.氧化铝气凝胶复合高温隔热瓦的制备及性能[J].宇航材料工艺,2017,47(3):33-36,41.SUN Jingjing, HU Zijun, WU Wenjun. Fabrication and properties of aerogels impregrated high-temperature insulating tiles[J].Aerospace material & Technology,2017,47(3):33-36,41.
    [10] 李俊宁,胡子君,吴文军.纳米孔隔热材料制备与导热系数计算[J].工程热物理学报2018,39(12):2784-2788.LI Junning, HU Zijun, WU Wenjun. nanoporous thermal insulator: preparation and thermal conductivity calculation[J]. Journal of Engineering Thermophysics,2018,39(12):2784-2788.
    [11] 杨景兴,何凤梅,陈聪慧.高温长时使用隔热材料热导率评价[J].复合材料学报,2013,30(12):279-282.YANG Jingxing, HE Fengmei, CHEN Conghui.Evaluation of thermal conductivity of insulation materials at high - temperature for longtime[J]. Acta Materiae Compositae Sinica,2013,30(12):279-282.
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夏吝时,杨海龙,钱丽,孙波,张春伟.准一维传热下冷面绝热边界材料对隔热试验结果的影响[J].宇航材料工艺,2023,53(6):82-86.

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  • 收稿日期:2022-04-14
  • 最后修改日期:2022-06-29
  • 录用日期:2022-06-30
  • 在线发布日期: 2023-12-15
  • 出版日期: 2023-12-30
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