Research Progress on Aerogel-based Integrated Thermal Protection Materials
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Affiliation:

Science and Technology on Advanced Ceramic Fibers and Composites Laboratory,College of Aerospace Science and Technology,National University of Defense Technology,Changsha 410073

Clc Number:

V45

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    Abstract:

    The rapid development of new high-speed aircraft has put forward higher requirements for thermal protection system. The integrated thermal protection materials based on aerogel is of great significance to improve the thermal insulation performance and structural efficiency of thermal protection system.In this paper, based on the difference of thermal protection materials, the research progress,structure and performance of aerogel-based integrated thermal protection materials are summarized, and the problems that need to be solved in the future are briefly described.

    Reference
    [1] 张纯学, 晗旭. 可负担的远程精确打击高超声速导弹[J]. 飞航导弹, 2006(12): 6-12.ZHANG C X,HAN X.Affordable long-range precision strike hypersonic missiles [J].Winged Missiles Journal,2006(12): 6-12.
    [2] 苏芳, 孟宪红. 三种典型热防护系统发展概况[J]. 飞航导弹, 2006(10): 57-60.SU F,MENG X H.Development of three typical thermal protection systems [J].Winged Missiles Journal,2006(10):57-60.
    [3] 曹舒蒙. 蜂窝夹芯热防护系统的热分析及结构优化设计[D]. 大连理工大学, 2016.CAO S M.Thermal analysis for honeycombed thermal protection systems and structural optimization[D].Dalian University of Technology. 2016
    [4] 胡良全, 薛忠民. 超长时热防护材料研究现状与发展[C]//中国空间科学学会空间材料专业委员会2009学术交流会论文集.湖南长沙:中国空间科学学会, 2009:165-172.HU L Q, XUE Z M. Research progress and development of ultra-long time thermal protection materials[C]//China Space Science Society Space Materials Committee 2009 Academic Exchange Conference, Changsha, Hunan: Chinese Society for Space Science, 2009:165-172.
    [5] JOEL W P, 西印. 航天飞机的防热毡[J].导弹与航天运载技术, 1992,(8): 80-84.JOEL W P, XI Y. Shuttle thermal blanket[J]. Missiles and Space Vehicles, 1992,(8): 80-84.
    [6] BANAS R,CREEDON J,CUNNINGTON G. Thermophysical and mechanical properties of the HTP family of rigid ceramic insulation materials[C]// 20th Thermophysics ConferenceWilliamsburg,VA, U.S.A.,1985,AIAA:85-1055.
    [7] 黄红岩, 苏力军, 雷朝帅, 等. 可重复使用热防护材料应用与研究进展[J]. 航空学报, 2020, 41(12): 6-40.HUANG H Y, SU L J, LEI C S, et al. Reusable thermal protective materials:application and research progress[J]. Acta Aeronautica ET Astronautica Sinica,2020,41(12):6-40.
    [8] 韩鸿硕. 国外航天运输系统防热系统、结构和材料的总体分析研究[J]. 宇航材料工艺,1997(4): 1-4.HAN H S.Analysis on thermal protection systems, structures and materials for space transportation systems abroad[J]. Aerospace Materials & Technology, 1997(4): 1-4.
    [9] 程海明, 洪长青, 张幸红. 低密度烧蚀材料研究进展[J]. 哈尔滨工业大学学报, 2018,50(5): 1-11.CHENG H M, HONG C Q, ZHANG X H. An overview on low-density ablators[J].Journal of Harbin Institute of Technology, 2018,50(5): 1-11.
    [10] 闫联生,李贺军,崔红,等.连续纤维补强增韧碳化硅基陶瓷复合材料研究进展[J].材料导报,2005(1): 60-63.YAN L S, LI H J, CUI H, et al. Advances of continuous fiber reinforced silicon carbide matrix ceramic composites[J]. Materials Reports, 2005(1): 60-63.
    [11] 谢巍杰, 陈明伟. SiC/SiC复合材料高温力学性能研究[J]. 人工晶体学报, 2016(6): 1534-1538.XIE W J, CHEN M W. Study on the high temperature properties of SiC/SiC composites[J]. Journal of Synthetic Crystals, 2016(6): 1534-1538.
    [12] KOURTIDES D A.Thermal performance of composite flexible blanket insulations for hypersonic aerospace vehicles[J]. Composites Engineering,1993,3(7/8):805-813.
    [13] 夏刚, 程文科, 秦子增. 充气式再入飞行器柔性热防护系统的发展状况[J]. 宇航材料工艺, 2003, 33(6): 1-6.XIA G, CHENG W K, QIN Z Z. Development of flexible thermal protection for system inflatable re-entry vehicles[J]. Aerospace Materials & Technology, 2003, 33(6): 1-6.
    [14] 关春龙,李壵,赫晓东.可重复使用热防护系统防热结构及材料的研究现状[J].宇航材料工艺,2003,33(6):9-13,44.GUAN C L,LI Y,HAO X D.Research status of structuresand materialsforreusable TPS[J].Aerospace Materials & Technology,2003,33(6): 9-13+44.
    [15] 周志勇,马彬,张萃,等.X-37B轨道试验飞行器可重复使用热防护系统综述[J].航天器工程,2016,25(4): 95-101.ZHOU Z Y, MA B, ZHANG C, et al. Reusable thermal protection system for orbital test vehicle X-37B[J]. Spacecraft Engineering, 2016, 25(4): 95-101.
    [16] BOHON H L,SHIDELER J L,RUMMER D R. Radiative metallic thermal protection systems: A status report[J]. Journal of Spacecraft & Rockets, 1977, 14(10): 626-631.
    [17] GRALLERT H,KELLER K.Metallic thermal protection system design for aerospace structures[J]. Thin-Walled Structures, 1991, 11(1/2): 105-127.
    [18] 孟松鹤, 杜善义, 韩杰才. 热防护系统及材料的研究进展[C]//第十四届全国复合材料学术会议论文集(上).湖北宜昌:中国宇航出版社, 2006: 11-17.MENG S H, DU S Y, HAN J C. Research progress of thermal protection systems and materials[C]//Proceedings of the 14th National Conference on Composite Materials. Yichang, Hubei: China Astronautic Publishing House, 2006:11-17.
    [19] 周德山. 宇宙往返机用超合金蜂窝热防护材料[J]. 国外导弹与航天运载器, 1989(10): 81-82.ZHOU D S.Superalloy honeycomb thermal protection material for space shuttle[J].Missiles and Space Vehicles,1989(10):81-82.
    [20] POTEET C C, ABU-KHAJEEL H, HSU S Y. Preliminary thermal-mechanical sizing of a metallic thermal protection system[J]. Journal of Spacecraft & Rockets, 2012, 41(2): 173-182.
    [21] 薛华飞,姚秀荣,程海明,等.热防护用轻质烧蚀材料现状与发展[J].哈尔滨理工大学学报,2017,22(1): 123-128.XUE H F, YAO X R, CHENG H M, et al. Current situation development of lightweight ablation materials for thermal protection[J]. Journal of Harbin University of Science and Technology, 2017, 22(1): 123-128.
    [22] MILOS F S. Thermostructural analysis of SIRCA tile for X-34 wing leading edge TPS[C]// Aiaa Aerospace Sciences Meeting & Exhibit. 2013.
    [23] MILOS F S, Gasch M J, Prabhu D K. Conformal phenolic impregnated carbon ablator arcjet testing, ablation, and thermal response[J]. Journal of Spacecraft and Rockets, 2015, 52(3): 804-812.
    [24] 彭志航, 曹峰, 陈莉, 等. 一种轻质微烧蚀型复合材料及其制备方法[P]. CN109957208A2019-07-02.PENG Z H, CAO F, CHEN L, et al. The invention discloses a light and micro-ablative composite material and a preparation method thereof[P]. CN109957208A2019.07.02.
    [25] 孟馨玥,何昕,秦岩,等.石英纤维增强可瓷化硼酚醛耐烧蚀复合材料研究[J].热固性树脂,2020,35(3): 10-14.MENG X Y, HE X, QIN Y, et al. Study on the quartz fiber reinforced ceramizable boron phenolic ablation resistant composite[J].Thermosetting Resin,2020,35(3):10-14.
    [26] 徐博,丁杰,王兵,等.AlB2 对高硅氧纤维增强可瓷化酚醛树脂基复合材料及其裂解产物力学性能的影响[J]. 复合材料学报, 2021, 38: 129-136.XU B, DING J, WANG B, et al. Effects of AlB2 on mechanical properties of high silica fiber/ceramicizable phenolic resin composites and their pyrolysis products[J]. Acta Materiae Compositae Sinica, 2021, 38: 129-136.
    [27] 吴晓栋,宋梓豪,王伟,等.气凝胶材料的研究进展[J].南京工业大学学报(自然科学版),2020,42(4):405-451.WU X D, SONG Z H, WANG W, et al. Advances of aerogels materials[J]. Journal of Nanjing Tech University(Natural Science Edition), 2020,42(4):405-451.
    [28] 刘婷, 刘源, 王晓栋, 等. 聚酰亚胺气凝胶材料的制备及其应用[J]. 工程科学学报, 2020, 42(1): 39-47.LIU T, LIU Y, WANG X D, et al. Preparation and application of polyimide aerogel materials[J].Chinese Journal of Engineering, 2020, 42(1): 39-47.
    [29] 黄兴, 冯坚, 张思钊, 等. 纤维素基气凝胶功能材料的研究进展[J]. 材料导报, 2016, 30(7): 9-14.HUANG X, FENG J, ZHANG S Z, et al.Development of cellulose-based aerogel functional materials[J].Materials Review, 2016,30(7):9-14.
    [30] 冯军宗.炭气凝胶及其隔热复合材料的制备与性能研究[D]. 长沙: 国防科学技术大学, 2012.FENG J Z. Preparation and characterization of carbon aerogel and composite for thermal insulation[D]. Changsha: National University of Defense Technology, 2012.
    [31] 岳晨午, 冯坚, 姜勇刚, 等. N杂化石墨烯气凝胶的组成和热导率[J]. 南京工业大学学报(自然科学版), 2016,38(2):1-6.YUE C W,FENG J,JIANG Y G, et al.Composition and thermal conductivity of N-doped graphene aerogel[J].Journal of Nanjing Tech University(Natural Science Edition),2016,38(2):1-6.
    [32] 孔勇,唐金琼,沈晓冬,等.块状碳化钛,氮化钛或碳氮化钛气凝胶的制备方法[P]. CN111892420A2020.11.06.KONG Y, TANG J Q, SHEN X D, et al. Method for preparing bulk titanium carbide, titanium nitride or titanium carbonitride aerogel[P]. CN111892420A2020.11.06.
    [33] 陈珂,包志豪,朱秀榕,等.碳化硅气凝胶的模板限制反应法制备与特性[J].原子能科学技术,2012,46(7):855-860.CHEN K, BAO Z H, ZHU X R, et al.Synthesis and characterization of silicon carbide aerogels via template-confined magnesiothermic reaction[J].Atomic Energy and Technology, 2012,46(7):855-860.
    [34] 锁浩,陆宇操,徐良旭,等.一种块状碳化硼气凝胶的制备方法[P]. CN108439409A2018.08.24.SUO H, LU Y C, XU L X, et al. The invention discloses a preparation method of massive boron carbide aeroge[P]. CN108439409A2018.08.24.
    [35] 杨杰,隋学叶,刘瑞祥,等.航天飞机及高超飞行器用刚性隔热材料研究进展[J].现代技术陶瓷,2015,36(3): 25-29.YANG J,SUI X Y,LIU R X,et al.The research development of rigid insulation materials for the space shuttle and hypersonic aircraft[J].Advanced Ceramics,2015,36(3):25-29.
    [36] HONG C Q,HAN J C,ZHANG X H,et al.Novel nanoporous silica aerogel impregnated highly porous ceramics with low thermal conductivity and enhanced mechanical properties[J]. Scripta Materialia, 2013, 68(8): 599-602.
    [37] 刘瑞祥. 氧化硅-氧化铝复合高温隔热瓦的制备与性能研究[D]. 哈尔滨:哈尔滨工业大学, 2016.LIU R X. Preparation and property of silica-alumina composite for high temperature insulation tile[D].Harbin:Harbin Institute of Technology, 2016.
    [38] 吴文军,肖鹏,曾凡,等.隔热瓦/SiO2气凝胶复合材料的制备与性能[J].宇航材料工艺,2019,49(5):35-38.WU W J,XIAO P,ZENG F,et al.Fabrication and properties of insulating tiles/SiO2 aerogels composite[J]. Aerospace Materials & Technology,2019,49(5):35-38.
    [39] 李勇,隋学叶,刘瑞祥,等.可加工氧化硅气凝胶复合刚性隔热瓦及其制备方法[P].CN104494225B2015.04.08.LI Y, SUI X Y, LIU R X, et al. Processable silica aerogel composite rigid heat insulation tile and its preparation method[P].CN104494225B.2015-04-08.
    [40] REN H Y,WU D F,WU W J,et al. Experimental and numerical research on high-temperature thermal insulation performance of lightweight porous ceramic/nanomaterial composite structure[J].Materialwissenschaft und Werkstofftechnik, 2019,50(12): 1525-1536.
    [41] 吕双祺,李想,左渝钰,等.气凝胶隔热复合材料在空天飞行器热防护技术中的应用[J].飞航导弹,2020,425(5):19-25.LYU S Q,LI X,ZUO Y Y,et al. Application of aerogel thermal insulation composite material in thermal protection technology of space vehicle[J].Aerodynamic Missile Journal, 2020,425(5):19-25.
    [42] 姚鸿俊,王飞,朱召贤,等.柔性有机硅气凝胶复合材料的制备及性能研究[J].宇航材料工艺,2019,49(6): 26-32.YAO H J,WANG F,ZHU Z X,et al.Preparation and properties of flexible silicone aerogel composites[J].Aerospace Materials & Technology,2019,49(6):26-32.
    [43] 沈晓冬,邵高峰,陆宇操,等.一种轻质柔性可重复使用防隔热一体化材料及其制备方法[P]. CN107142715A2019.09.08.SHEN X D, SHAO G F, LU Y C, et al.The invention and a preparation method thereof relates to a lightweight, flexible and reusable anti-heat insulation integrated material[P]. CN107142715A. 2019-09-08.
    [44] 高岩. SiOC气凝胶/柔性陶瓷纤维复合材料的制备及其性能研究[D]. 哈尔滨: 哈尔滨工业大学, 2017.GAO Y. Preparation and characterization of silicon oxycarbide aerogel/flexibel ceramic fiber composite[D]. Harbin: Harbin Institute of Technology, 2017.
    [45] 孙现凯, 张世超, 吴蔚, 等. 氧化铝纤维/氧化硅气凝胶/石墨纸多层缝合柔性隔热材料制备及隔热性能研究[J]. 陶瓷学报, 2018, 39(1): 59-63.SUN X K, ZHANG S C, WU W, et al. Preparation and thermal insulation effect of stitched alumina fiber/ silica aerogel/ graphite paper multi-layer flexible composites[J].Journal of Ceramics,2018,39(1):59-63.
    [46] BUFFENOIR F,ZEPPA C,PICHON T,et al. Development and flight qualification of the C-SiC thermal protection systems for the IXV[J].Acta Astronautica,2016,124: 85-89
    [47] BUFFENOIR F, ESCAFRE D, BRAULT T, et al. Dynamical and thermal qualification of the C-SiC nose for the IXV[J]. Acta Astronautica,2016,124: 79-84.
    [48] 李广德,张长瑞,胡海峰,等.盖板式陶瓷热防护系统的传热性能优化[J].国防科技大学学报,2014,36(5): 143-148.LI G D, ZHANG C R, HU H F, et al. Optimization study of heat transfer properties for generic shingle ceramic thermal protection system[J]. Journal of National University of Defense Technology,2014, 36(5): 143-148.
    [49] 姚栋嘉, 吴恒, 刘喜宗, 等. 一种热防护板[P]. CN110626011A. 2019-12-13.YAO D J, WU H, LIU X Z, et al. The utility model relates to a thermal protective plate[P]. CN110626011A. 2019-12-13.
    [50] LI Y,ZHANG L,HE R,et al.Integrated thermal protection system based on C/SiC composite corrugated core sandwich plane structure[J].Aerospace Science & Technology, 2019,91: 607-616.
    [51] 汤素芳, 杨鸷, 胡成龙, 等. 一种防隔热、承载一体化炭气凝胶/陶瓷层状复合材料及其制备方法和应用[P]. CN107473761A. 2017-12-15.TANG S F, YANG Z, HU C L, et al. The invention relates to an integrated carbon aerogel/ceramic lamellar composite material with heat insulation and bearing capacity and a preparation method and application thereof[P]. CN107473761A. 2017-12-15.
    [52] 曹峰,冯坚,姜勇刚,等.一种耐高温隔热三明治结构陶瓷复合材料及其制备方法[P].CN102642350A.2012-08-22.CAO F,FENG J,JIANG Y G,et al.The invention discloses a ceramic composite material with high temperature resistance and heat insulation sandwich structure and a preparation method thereof[P]. CN102642350A. 2012-08-22.
    [53] 向阳,曹峰,彭志航,等.一种低成本耐高温陶瓷复合材料及其快速制备方法[P].CN109824372A. 2019-05-13.XIANG Y,CAO F,PENG Z H, et al. The invention relates to a low-cost high temperature resistant ceramic composite material and a rapid preparation method thereof[P].CN109824372A. 2019-05-13.
    [54] 李健,张凡,张丽娟,等.一种耐高温多层热防护组件结构设计与性能研究[J].北京理工大学学报,2019,39(10):1051-1056.LI J,ZHANG F,ZHANG L J,et al.Structure design and performance study of a multi-layer thermal protection component with high temperature endurance[J].Transactions of Beijing Institute of Technology,2019,39(10): 1051-1056.
    [55] 姚草根,吕宏军,贾新潮,等.金属热防护系统材料与结构研究进展[J].宇航材料工艺,2005,35(2): 10-13.YAO C G,LYU H J,JIA X C,et al.Development of metallic thermal protection system[J].Aerospace Materials & Technology,2005,35(2): 10-13.
    [56] 夏德顺. 重复运载器金属热防护系统的述评[J]. 导弹与航天运载技术, 2002(2): 23-28.XIA D S. Review of metallic thermal protection system for the reusable launch vehicle[J]. Missiles and Space Vehicles, 2002(2): 23-28.
    [57] GUO Q, WANG S A, HUI W Z, et al. Thermo-mechanical optimization of metallic thermal protection system under aerodynamic heating[J]. Structural and Multidisciplinary Optimization, 2020, 61(2): 819-836.
    [58] CAO C Y,WANG R X,XING X D,et al. Performance improvement of integrated thermal protection system using shaped-stabilized composite phase change material[J]. Applied Thermal Engineering, 2019, 164: 114529.
    [59] 刘文祎, 曲海涛, 苏亚东, 等. 一种钛基复合材料热防护蒙皮结构的制备方法[P]. CN110527933A. 2019-12-03.LIU W Y,QU H T, SU Y D,et al.The invention discloses a preparation method for thermal protective skin structure of titanium matrix composite material[P].CN110527933A. 2019-12-03.
    [60] 刘海涌, 刘朝阳, 刘存良. 气凝胶夹芯金属热防护结构换热特性的实验研究[J]. 固体火箭技术, 2016(2): 253-258.LIU H Y, LIU C Y, LIU C L. Experimental investigation on heat transfer characteristics of the metallic thermal protection system with aerogel insulation[J]. Journal of Solid Rocket Technology, 2016(2): 253-258.
    [61] 朱召贤,董金鑫,贾献峰,等.酚醛气凝胶/炭纤维复合材料的结构与烧蚀性能[J].新型炭材料,2018,33(4): 370-376.ZHU Z X, DONG J X, JIA X F, et al. The microstructure and ablation behavior of carbon fiber/phenolic aerogel composites[J]. New Carbon Materials, 2018,33(4): 370-376.
    [62] WANG C H, CHENG H M, HONG C Q, et al. Lightweight chopped carbon fibre reinforced silica-phenolic resin aerogel nanocomposite: Facile preparation, properties and application to thermal protection[J].Composites Part A: Applied Science and Manufacturing,2018,112: 81-90.
    [63] 王瑞杰, 苏力军, 李文静, 等. 一种碳基增强耐烧蚀酚醛气凝胶材料及其制备方法[P]. CN110981524A. 2020-04-10.WANG R J, SU L J, LI W J, et al. The invention relates to a carbon base enhanced ablative resistant phenolic aerogel material and a preparation method thereof[P]. CN110981524A. 2020-04-10.
    [64] 苏力军, 刘斌, 张凡, 等. 一种微烧蚀隔热材料及其制备方法[P]. CN103449825A. 2013-12-18.SU L J, LIU B, ZHANG F, et al. The invention relates to a micro-ablative heat insulation material and a preparation method thereof[P]. CN103449825A. 2013-12-18.
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History
  • Received:September 15,2021
  • Revised:July 03,2022
  • Adopted:December 21,2021
  • Online: September 02,2022
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