碳/碳化硅复合材料接触热阻计算方法

doi:10.12382/bgxb.2021.0590

摘要/Abstract

摘要： 在高速飞行器结构与防隔热系统设计及评估中，需要准确判断接触热阻对结构热响应的影响。针对当前高速飞行器采用性能优异的碳/碳化硅复合材料，建立了该材料接触热阻理论计算方法，并完成了典型工况地面风洞验证试验研究，进一步利用该方法开展碳/碳化硅复合材料之间接触热阻的变化规律研究。研究结果表明，建立的高温接触热阻计算方法与地面风洞试验结果对比具有较好的精度，典型工况下碳/碳化硅复合材料接触热阻的热响应预示结果与地面试验结果误差仅约4%，有关结果可以为高速飞行器结构与热防护系统的设计及安全评估提供参考。

关键词: 碳/碳化硅, 接触热阻, 理论方法, 地面试验

Abstract: Thermal contact resistance must be accurately evaluated to ensure proper design and safety of hypersonic vehicles. In terms of the C/SiC composite material for hypersonic vehicle structures, an approach for assessing the thermal contact resistance of this material is proposed and wind tunnel experiments are performed. The change law of the thermal contact resistance for the C/SiC composite material is also investigated. The results show that the thermal contact resistance and contact resistance proposed in this paper have good accuracy compared with the wind tunnel results, with a difference of only 4%. The proposed approach and test results serve as a reference for designing and evaluating the structure and thermal protection performance of hypersonic vehicles.

Key words: C/SiCcompositematerial, thermalcontactresistance, engineeringmethod, experimentalinvestigation

中图分类号:

V215

曹占伟，陈鑫，付斌，徐晓亮，袁野，毛伟，王培枭，姚军，梅杰. 碳/碳化硅复合材料接触热阻计算方法[J]. 兵工学报, 2022, 43(11): 2897-2904.

CAO Zhanwei, CHEN Xin, FU Bin, XU Xiaoliang, YUAN Ye, MAO Wei, WANG Peixiao, YAO Jun, MEI Jie. Engineering Investigations of Thermal Contact Resistance of C/SiC Composite Materials[J]. Acta Armamentarii, 2022, 43(11): 2897-2904.

参考文献

［1］王安良，赵剑锋. 接触热阻预测的研究综述[J]. 中国科学：技术科学，2011,41(5): 545-556.
WANG A L, ZHAO J F. Review of prediction for thermal contact resistance[J]. Science China Technology Science, 2011, 41(5): 545-556. (in Chinese)
[2] 朱广生.世界高超声速机动飞行器技术发展纵览[M]. 北京:科学出版社，2018.
ZHU G S. Overview of world hypersonic maneuvering vehicle technology development [M]. Beijing: Science Press, 2018. (in Chinese)
[3] LANDER C H. Communications on a review of recent progress in heat transfer[J]. Proceedings of the Institution of Mechanical Engineers, 1943, 149: 126-130.
[4] 陆敏恂，南国腾，周爱国. 基于 ANSYS 的接触热阻的有限元分析[J].流体传动与控制, 2013(6): 34-37.
LU M X, NAN G T,ZHOU A G. Finite element analysis of thermal contact resistance based on ANSYS[J]. Fluid Power Transmission and Control, 2013(6): 34-37. (in Chinese)
[5] 张楠，王丽华，何雨松，等. 分形粗糙表面的计算模拟[J]. 新技术新工艺,2013(6):82-84.
ZHANG N, WANG L H, HE Y S, et al. Computer simulation of fractal rough surfaces[J]. New Technology & New Process, 2013(6):82-84. (in Chinese)
[6] 孙柯,赵美英,万小朋, 等. 接触热导率数值预测研究[J]. 机械科学与技术, 2013, 32(7): 973-976.
SUN K, ZHAO M Y, WAN X P, et al. Numerically predicting thermal contact conductance[J]. Mechanical Science and Technology for Aerospace Engineering, 2013, 32(7): 973-976. (in Chinese)
[7] FLETCHER L S. Recent developments in contact conductance heat transfer［J］． Journal of Heat Transfer, 1988, 110(4): 1059- 1070．
[8] SRIDHAR M R，YOVANOVICH M M. Review of elastic and plastic contact conductance models: comparison with experiment［J］． Journal of Thermophysics and Heat Transfer，1994，8(4): 633-640．
[9] LAMBERT M A，FLETCHER L S. Review of models for thermal contact conductance of metals［J］． Journal of Thermophysics and Heat Transfer，1997，11(2) : 129-140．
[10] YOVANOVICH M M. Conduction and thermal contact resistances (conductances)[M]. ROHSENOW W M, HARTNETT J P, CHO Y I, eds. Handbook of Heat Transfer. Chapter 3. New York，NY，US: McGraw Hill, 1998.
[11] YOVANOVICH M M, ANTONETTI V W. Application of thermal contact resistancetheory to electronic packages[M]. BAR-COHEN A, KRAUS A D, eds. Advances in Thermal Modeling of Electronic Components and Systems. New York，NY，US: Hemisphere Publishing, 1988.
[12] MADHUSUDANA C V. Thermal contact conductance[M]. New York，NY，US: Springer-Verlag, 1996.
[13] MADHUSUDANA C V, FLETCHER L S. Contact heat transfer-The last decade[J]. AIAA J, 1986, 24(3): 510-523 .
[14] LIU D H，LUO Y，SHANG X C. Experimental investigation of high temperature thermal contact resistance between high thermal conductivity C/C material and inconel 600［J］． International Journal of Heat and Mass Transfer，2015，80: 407-410．
[15] LIU D H，LIU Y H. Heat transfer capability simulation of high temperature heat pipe in supersonic vehicle leading edge applications[J]. Advances in Mechanical Engineering，2016，8(4): 1-10 ．
[16] 刘冬欢，郑小平，黄拳章，等. C/C复合材料与高温合金GH600之间高温接触热阻的试验研究[J].航空学报, 2010,31(11):2189-2194.
LIU D H, ZHENG X P, HUANG Q Z, et al. Experimental investigation of high-temperature thermal contact resistance between C/C conposite material and superalloy GH600[J]. Acta Aeronautica et Astronautica Sinica, 2010, 31(11): 2189-2194.（in Chinese）
[17] 顾慰兰. 接触热阻的试验研究[J].南京航空航天大学学报, 1992, 24(1): 46-52 .
GU W L. Experiment on thermal contact resistance[J]. Journal of Nanjing University of Aeronautics & Astronautics, 1992, 24(1): 46-52. (in Chinese)
[18] 顾慰兰. 一种随机表面间接触热阻的计算方法[J].航空动力学报, 1995, 10(3): 232-236.
GU W L. A method for calculation of contact heat resistance between two contacting surfaces[J]. Journal of Aerospace Power, 1995, 10(3): 232-236. (in Chinese)
[19] 顾慰兰, 杨燕生. 温度对接触热阻的影响[J].南京航空航天大学学报, 1994, 26(3): 342-349 .
GU W L, YANG Y S. The influence of temperature on contact resistance of metallic surfaces temperature[J]. Journal of Nanjing University of Aeronautics & Astronautics, 1994, 26(3): 342-349. (in Chinese)
[20] 宣益民,李强,张平. 高温条件下的固-固界面接触热阻测试方法与系统[J]. 中国科学：技术科学, 2019, 49(5): 491-500.
XUAN Y M, LI Q, ZHANG P. Measurement method and instrument of thermal contact resistance at high temperature[J]. Scientia Sinica Technologica, 2019, 49(5):491-500. (in Chinese)
[21] 张仡，成竹，秦强，等．接触热阻对超声速飞行器结构响应分析的影响[J]．科学技术与工程，2020，20(12): 4985-4991.
ZHANG Y，CHENG Z，QIN Q，et al． Effects of thermal contact resistance on structural responses of supersonic aircraft in numerical simulation［J］． Science Technology and Engineering，2020，20(12): 4985-4991. (in Chinese)
[22] MILANEZ F H，YOVANOVICH M M，MANTELLI M B. Thermal contact conductance at low contact pressures［J］． Journal of Thermophysics and Heat Transfer，2004，18(1): 37-44．
[23] MIKIAC＇U2 B B. Thermal contact conductance: theoretical considerations［J］. International Journal of Heat and Mass Transfer, 1974, 17（2）: 205-214 .
[24] TABOR D. A simplfied account of surface topography and the contact between solids［J］. Wear, 1975，32(2): 269-271.
[25] ANTONETTI V W. Statistical variability of thermal interface conductance[C]∥NSF/DITAC workshop. Melbourne, Australia, 1992： 37-45.
[26] SONG S，YOVANOVICH M.M. Relative contact pressure: dependence on surface roughness and Vickers microhardness[J]. Journal of Thermophysics and Heat Transfer, 1988,2(1): 43-47.
[27] 杨世铭，陶文诠.传热学[M].第2版.北京：高等教育出版社,2010.
YANG S M, TAO W Q. Heat transfer[M]. 2nd edit. Beijing: Higher Education Press, 2010. (in Chinese)

[1]	李婷，刘林，彭云程，崔超雄，薛非. 面向战备完好的飞机群组预防性维护优化和备件预测方法[J]. 兵工学报, 2022, 43(7): 1695-1705.
[2]	陶小创, 郭霖瀚, 肖波平, 刘瑞. 基于备件保障概率分配的备件需求量预测模型[J]. 兵工学报, 2012, 33(8): 975-979.
[3]	王乃超，康锐，程海龙. 基于马尔可夫过程的备件库存动态特性分析[J]. 兵工学报, 2009, 30(7): 984-988.
[4]	王乃超，康锐. 多约束条件下备件库存优化模型及分解算法[J]. 兵工学报, 2009, 30(2): 247-251.
[5]	郭霖瀚，章文晋，康锐. 导弹武器系统维修保障建模与仿真[J]. 兵工学报, 2006, 27(5): 851-856.
[6]	李占国，张宏，石岩,徐春鹰. 齿轮激光热处理工艺研究[J]. 兵工学报, 2003, 24(2): 226-229.
[7]	1:张宏;2:余承业;3:吴鸿兴,郭大浩. 小孔激光冲击表面强化技术研究[J]. 兵工学报, 2001, 22(3): 330-333.