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刘冬欢等:内置高导C/C材料的疏导式热防护结构防热效果 249· 参考文献 Proceeding of Chinese Society of Engineering Thermophysics.Xi Silverstein CC.A Feasibility Study of Heat Pipe Cooled Leading An,2011 Edges for Hypersonic Cruise Aircraft [R/OL].NASA Contractor (肖光明,任建勋,桂业伟,等.基于热网络分析法的疏导式 Report NASA CR-1857 [2014-12-19].http://ntrs.nasa.gov/ 热防护用高温热管启动特性研究/中国工程热物理学会学 archive/nasa/casi.ntrs.nasa.gov/19720005300.pdf 术会议.西安,2011) Camarda C J,Masek R V.Design,analysis and tests of a shuttle- [13]Lu Q,Jiang GQ,Yu J J.Research on the thermal response of type heat-pipe-cooled leading edge.J Spacecr Rockets,1981,18: the start-up of high temperature heat pipe /Proceeding of the 11 13th Heat Pipe Meeting.Shanghai,2012:1 B]Colwell C T,Jang J,Camarda C J.Modeling of startup from the (鲁芹,姜贵庆,俞继军.高温热管启动热响应方法研究1 frozen state /Proceedings of the Sixth International Heat Pipe 第十三届全国热管年会.上海,2012:1) Conference.Grenoble,1987:165 04] Chen LZ.Ou D B.Liu D Y.Elementary experiment study on 4]Jang J.An Analysis of Startup from the Frozen State and Transient the application of high temperature heat-pipe to the thermal pro- Performance of Heat Pipes [Dissertation].Georgia Institute of tection.Front Sci,2009,3(10):41 Technology,1988 (陈连忠,欧东斌,刘德英.高温热管在热防护中应用初探 [5]Wojcik CC,Clark LT.Design,analysis,and testing of refracto- 前沿科学,2009,3(10):41) ry metal heat pipe using lithium as the working fluid /Proceed- [15]Li T Q.Hu Z J.Carbon materials with high directional thermal ings of the 26th Thermophysics Conference.Honolulu,1991:1 conductivity and their structure design of thermal management [6]Juhasz A J.Rovang R D.Carbon-Carbon Heat Pipe Testing and system.Aerosp Mater Technol,2007(1):16 Eraluation [R/OL].NASA Technical Memorandum 106630 (李同起,胡子君.定向高导热碳材料及其热管理结构设计 AIAA-94-4065 014-12-19].http://ntrs.nasa.gov/archive/ 字航材料工艺,2007(1):16) nasa/casi.ntrs.nasa.gov/19940032810.pdf [16]Jiang GQ,Ai B C,Yu J J.The property expression and conduc- 7]Glass D E,Camarda C J,Merrigan M A,et al Fabrication and tion analysis of solid medium for Shu-ao thermal protection.Ac- testing of Mo-Re heat pipes embedded in carbon/carbon.J ta Aerodyn Sin,2008,26(Suppl 1):44 Spacecr Rockets,1999,36:79 (姜贵庆,艾邦成,俞继军.疏导热防护的固体传导的性能 8]Jiang GQ.Ai BC.Yu JJ.The cooling mechanism of mitigate 表征与传导特性分析.空气动力学报,2008,26(增刊1): thermal protection.Acta Aerodyn Sin,2009,27 (Suppl 1):46 44) (姜贵庆,艾邦成,俞继军.疏导热防护的冷却机制.空气动 [17]Sun J,Liu W Q.Analysis of sharp leading-edge thermal protec- 力学学报,2009,27(增刊1):46) tion of high thermal conductivity materials.Acta Aeronaut Astro- Liu D H,Zheng X P,Wang F,et al.Mechanism of thermome- naut Sin,2011,32(9):1622 chanical coupling of high temperature heat pipe cooled C/C com- (孙健,刘伟强.尖化前缘高导热材料防热分析.航空学报, posite material thermal protection structure.Acta Mater Compos 2011,32(9):1622) Sim,2010,27(3):43 [18]Sun J Liu W Q.Analysis of thermal protection mechanism of (刘冬欢,郑小平,王飞,等.内置高温热管C/C复合材料热 leading structure embedded high directional thermal conductivity 防护结构热力耦合机制.复合材料学报,2010,27(3):43) layer.Acta Phys Sin,2012,61(12):124401 [10]Liu D H,Zheng X P,Wang F,et al.Heat conduction and heat (孙健,刘伟强.内嵌定向高导热层疏导式结构热防护机理 proof mechanism of the heat pipe cooled thermal protection sys- 分析.物理学报,2012,61(12):124401) tem.J Tsinghua Univ Sci Technol,2010,50(7):1094 [19]Sun J.Liu WQ.Application of leading structure on thermal pro- (刘冬欢,郑小平,王飞,等.内置高温热管热防护结构的传 tection of nosetip.Acta Phys Sin,2012,61(17):174401 热防热机理.清华大学学报:自然科学版,2010,50(7): (孙健,刘伟强.疏导式结构在头锥热防护中的应用.物理 1094) 学报,2012,61(17):174401) [11]Liu D H,Shang X C.Effect of thermal contact resistance on the 20]Liu D H,Zheng X P,Huang QZ,et al.Experimental investiga- performance of heat-pipe-cooled thermal protection structures. tion of high-emperature thermal contact resistance between C/C Acta Aeronaut Astronaut Sin,2012,33(10):1834 composite material and superalloy GH600.Acta Aeronaut Astro- (刘冬欢,尚新春.接触热阻对疏导式热防护结构防热效果 naut Sin,2010,31(11):2189 的影响.航空学报,2012,33(10):1834) (刘冬欢,郑小平,黄拳章,等。CC复合材料与高温合金 [12]Xiao G M,Ren J X,Gui Y W,et al.Research on the start-up GH600之间高温接触热阻的试验研究.航空学报,2010,31 of high tempearture heat pipe with thermal network analysis / (11):2189)刘冬欢等: 内置高导 C/C 材料的疏导式热防护结构防热效果 参 考 文 献 [1] Silverstein C C. A Feasibility Study of Heat Pipe Cooled Leading Edges for Hypersonic Cruise Aircraft [R /OL]. NASA Contractor Report NASA CR--1857 [2014--12--19]. http: / / ntrs. nasa. gov / archive / nasa /casi. ntrs. nasa. gov /19720005300. pdf [2] Camarda C J,Masek R V. Design,analysis and tests of a shuttle￾type heat-pipe-cooled leading edge. J Spacecr Rockets,1981,18: 71 [3] Colwell G T,Jang J,Camarda C J. Modeling of startup from the frozen state / / Proceedings of the Sixth International Heat Pipe Conference. Grenoble,1987: 165 [4] Jang J. An Analysis of Startup from the Frozen State and Transient Performance of Heat Pipes [Dissertation]. Georgia Institute of Technology,1988 [5] Wojcik C C,Clark L T. Design,analysis,and testing of refracto￾ry metal heat pipe using lithium as the working fluid / / Proceed￾ings of the 26th Thermophysics Conference. Honolulu,1991: 1 [6] Juhasz A J,Rovang R D. Carbon-Carbon Heat Pipe Testing and Evaluation [R /OL]. NASA Technical Memorandum 106630 AIAA--94--4065 [2014--12--19]. http: / / ntrs. nasa. gov /archive / nasa /casi. ntrs. nasa. gov /19940032810. pdf [7] Glass D E,Camarda C J,Merrigan M A,et al Fabrication and testing of Mo-- Re heat pipes embedded in carbon /carbon. J Spacecr Rockets,1999,36: 79 [8] Jiang G Q,Ai B C,Yu J J. The cooling mechanism of mitigate thermal protection. Acta Aerodyn Sin,2009,27( Suppl 1) : 46 ( 姜贵庆,艾邦成,俞继军. 疏导热防护的冷却机制. 空气动 力学学报,2009,27( 增刊 1) : 46) [9] Liu D H,Zheng X P,Wang F,et al. Mechanism of thermome￾chanical coupling of high temperature heat pipe cooled C /C com￾posite material thermal protection structure. Acta Mater Compos Sin,2010,27( 3) : 43 ( 刘冬欢,郑小平,王飞,等. 内置高温热管 C /C 复合材料热 防护结构热力耦合机制. 复合材料学报,2010,27( 3) : 43) [10] Liu D H,Zheng X P,Wang F,et al. Heat conduction and heat proof mechanism of the heat pipe cooled thermal protection sys￾tem. J Tsinghua Univ Sci Technol,2010,50( 7) : 1094 ( 刘冬欢,郑小平,王飞,等. 内置高温热管热防护结构的传 热防热机理. 清华大学学报: 自然科学版,2010,50 ( 7 ) : 1094) [11] Liu D H,Shang X C. Effect of thermal contact resistance on the performance of heat-pipe-cooled thermal protection structures. Acta Aeronaut Astronaut Sin,2012,33( 10) : 1834 ( 刘冬欢,尚新春. 接触热阻对疏导式热防护结构防热效果 的影响. 航空学报,2012,33( 10) : 1834) [12] Xiao G M,Ren J X,Gui Y W,et al. Research on the start-up of high tempearture heat pipe with thermal network analysis / / Proceeding of Chinese Society of Engineering Thermophysics. Xi’ An,2011 ( 肖光明,任建勋,桂业伟,等. 基于热网络分析法的疏导式 热防护用高温热管启动特性研究 / / 中国工程热物理学会学 术会议. 西安,2011) [13] Lu Q,Jiang G Q,Yu J J. Research on the thermal response of the start-up of high temperature heat pipe / / Proceeding of the 13th Heat Pipe Meeting. Shanghai,2012: 1 ( 鲁芹,姜贵庆,俞继军. 高温热管启动热响应方法研究 / / 第十三届全国热管年会. 上海,2012: 1) [14] Chen L Z,Ou D B,Liu D Y. Elementary experiment study on the application of high temperature heat-pipe to the thermal pro￾tection. Front Sci,2009,3( 10) : 41 ( 陈连忠,欧东斌,刘德英. 高温热管在热防护中应用初探. 前沿科学,2009,3( 10) : 41) [15] Li T Q,Hu Z J. Carbon materials with high directional thermal conductivity and their structure design of thermal management system. Aerosp Mater Technol,2007( 1) : 16 ( 李同起,胡子君. 定向高导热碳材料及其热管理结构设计. 宇航材料工艺,2007( 1) : 16) [16] Jiang G Q,Ai B C,Yu J J. The property expression and conduc￾tion analysis of solid medium for Shu-Dao thermal protection. Ac￾ta Aerodyn Sin,2008,26( Suppl 1) : 44 ( 姜贵庆,艾邦成,俞继军. 疏导热防护的固体传导的性能 表征与传导特性分析. 空气动力学报,2008,26 ( 增刊 1) : 44) [17] Sun J,Liu W Q. Analysis of sharp leading-edge thermal protec￾tion of high thermal conductivity materials. Acta Aeronaut Astro￾naut Sin,2011,32( 9) : 1622 ( 孙健,刘伟强. 尖化前缘高导热材料防热分析. 航空学报, 2011,32( 9) : 1622) [18] Sun J Liu W Q. Analysis of thermal protection mechanism of leading structure embedded high directional thermal conductivity layer. Acta Phys Sin,2012,61( 12) : 124401 ( 孙健,刘伟强. 内嵌定向高导热层疏导式结构热防护机理 分析. 物理学报,2012,61( 12) : 124401) [19] Sun J,Liu W Q. Application of leading structure on thermal pro￾tection of nosetip. Acta Phys Sin,2012,61( 17) : 174401 ( 孙健,刘伟强. 疏导式结构在头锥热防护中的应用. 物理 学报,2012,61( 17) : 174401) [20] Liu D H,Zheng X P,Huang Q Z,et al. Experimental investiga￾tion of high-temperature thermal contact resistance between C /C composite material and superalloy GH600. Acta Aeronaut Astro￾naut Sin,2010,31( 11) : 2189 ( 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. 航空学报,2010,31 ( 11) : 2189) · 942 ·
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