C/SiC复合材料在超燃冲压发动机中的应用研究进展

doi:10.3724/SP.J.1077.2013.12466

无机材料学报 ›› 2013, Vol. 28 ›› Issue (3): 247-255.DOI: 10.3724/SP.J.1077.2013.12466

C/SiC复合材料在超燃冲压发动机中的应用研究进展

马青松¹, 刘海韬^1,2, 潘余², 刘卫东², 陈朝辉¹

(国防科技大学 1. 新型陶瓷纤维及其复合材料重点实验室; 2. 高超声速冲压发动机技术重点实验室, 长沙 410073)

收稿日期:2012-08-07 修回日期:2012-10-10 出版日期:2013-03-20 网络出版日期:2013-02-20
基金资助:
国家自然科学基金重大研究计划(90916002, 91116001); 湖南省高校科技创新团队支持计划

Research Progress on the Application of C/SiC Composites in Scramjet

MA Qing-Song¹, LIU Hai-Tao^1,2, PAN Yu², LIU Wei-Dong², CHEN Zhao-Hui¹

(1. Science and Technology on Advanced Ceramic Fibers &Composites Laboratory, National University of Defense Technology, Changsha 410073, China; 2. Science and Technology on Scramjet Laboratory, National University of Defense Technology, Changsha 410073, China)

Received:2012-08-07 Revised:2012-10-10 Published:2013-03-20 Online:2013-02-20
Supported by:
Grand Research Project of National Natural Science Foundation of China (90916002, 91116001); Aid program for Science and Technology Innovative Research Team in Higher Educational Institutions of Hunan Province

摘要/Abstract

摘要： 超燃冲压发动机是发展高超声速技术的核心, 以其为动力装置的各类高超声速飞行器对于国防安全和航天运输都有重要意义。本文分析了超燃冲压发动机对热防护材料的要求, 综述了C/SiC复合材料在超燃冲压发动机中的应用研究现状, 提出了发展建议, 指出了需要关注的关键问题。

关键词: C/SiC复合材料, 热防护, 主动冷却, 超燃冲压发动机, 综述

Abstract: Scramjet is crucial to develop hypersonic technology. The hypersonic vehicles with scramjet as power device are of much significance for national defense security and space transportation. In this paper, the requirements for thermal protection materials of scramjet were analyzed and current status of the application of C/SiC composites in scramjet was reviewed. At last, the development proposals and key problems needed to be solved for C/SiC composites were offered in order to meet the demands of scramjet.

Key words: C/SiC composites, thermal protection, active cooling, scramjet, review

中图分类号:

TB323

马青松, 刘海韬, 潘余, 刘卫东, 陈朝辉. C/SiC复合材料在超燃冲压发动机中的应用研究进展[J]. 无机材料学报, 2013, 28(3): 247-255.

MA Qing-Song, LIU Hai-Tao, PAN Yu, LIU Wei-Dong, CHEN Zhao-Hui. Research Progress on the Application of C/SiC Composites in Scramjet[J]. Journal of Inorganic Materials, 2013, 28(3): 247-255.

参考文献

[1] LIU Xiao-Yong. Scramjet technology. Journal of Propulsion Technology, 2003(2): 38–42.

[2] Voland R T, Huebner L D, McClinton C R. X-43A hypersonic vehicle technology development. Acta Astronautica, 2006, 59(1-5): 181–191.

[3] WANG Zhen-Guo, LIANG Jian-Han, DING Meng, et al. A review on hypersonic airbreathing propulsion system. Advances in Mechanics, 2009, 39(6): 716–739.

[4] MA Jie, LIANG Jun-Long. Development trends and directions of liquid ramjet/scramjet technology. Journal of Rocket Propulsion, 2011, 37(4): 12–17.

[5] REN Jia-Wan, TAN Yong-Hua. Thermal protection techniques of ramjet combustor. Journal of Rocket Propulsion, 2006, 32(4): 38–42.

[6] Wie D M, Drewry D G, King D E, et al. The hypersonic environment: required operating conditions and design challenges. Journal of Materials Science, 2004, 39(19): 5915–5924.

[7] Jackson T A, Eklund D R, Fink A J. High speed propulsion: performance advantage of advanced materials. Journal of Materials Science, 2004, 39(19): 5905–5913.

[8] ZHANG Quan-Ming. Research on CMC for aerospace applications. Aerospace Materials &Technology, 2011(6): 1–3.

[9] LIU Zhi-Quan, MA Wu-Jun. Applied research of rocket engine thrusters made of ceramic matrix composite. Journal of Rocket Propulsion, 2011, 37(2): 19–24.

[10] Glass D E. Ceramic Matrix Composite (CMC) Thermal Protection Systems (TPS) and Hot Structures for Hypersonic Vehicles. AIAA 2008–2682.

[11] Beyer S, Strobe F, Knabe H. Development and Testing of C/SiC Components for Liquid Rocket Propulsion Applications. AIAA 99–2896.

[12] Wang Y G, Liu W, Cheng L F, et al. Preparation and properties of 2D C/ZrB2-SiC ultra high temperature ceramic composites. Materials Science &Engineering A, 2009, 524(1/2): 129–133.

[13] ZHANG Li-Tong, CHENG Lai-Fei, XU Yong-Dong. Progress in research work of new CMC-SiC. Aeronautic Manufacturing Technology, 2003(1): 24–32.

[14] Bouquet C, Fischer R, Thebault J, et al. Composite Technologies Development Status for Scramjet. AIAA 2005–3431.

[15] Dirling R B. Progress in Materials and Structures Evaluation for the HyTech program. AIAA 98–1591.

[16] Chen F F, Tam W F, Shimp N R, et al. An Innovative Thermal Management System for a Mach 4 to Mach 8 Hypersonic Scramjet engine. AIAA 98–3734

[17] Sillence M A. Hydrocarbon Scramjet Engine Technology Flowpath Component Development. AIAA 2002–5158.

[18] Haug T, Ehrmann U, Knabe H. Air Intake Ramp Made from C/Sic via the Polymer Route for Hypersonic Propulsion Systems. AIAA 93–5036.

[19] Paquette E. Cooled CMC Structures for Scramjet Engine Flowpath Components. AIAA 2005–3432.

[20] Bouquet C, Lacombe A, Hauber B, et al. Ceramic Matrix Composites Cooled Panel Development for Advanced Propulsion Systems. AIAA 2004–1998.

[21] Bouquet C, Fischer R, Bouhali A L, et al. Fully Ceramic Composite Heat Exchanger Qualification for Advanced Combustion Chambers. AIAA 2005–3433.

[22] Steel S. Ceramic materials for reusable liquid fueled rocket engine combustion devices. The AMPTIAC Quarterly, 2004, 8(1): 39–43.

[23] Jaskowiak M H. Cooled ceramic composite panel tested successfully in rocket combustion facility. http://www.grc.nasa.gov/ WWW/RT2002/5000/5130jaskowiak.html.

[24] Bouchez M, Beyer S. PTAH-SOCAR Fuel-cooled Composite Materials Structure: 2009 status. AIAA 2009–7353.

[25] Bouchez M, Beyer S. PTAH-SOCAR Fuel-cooled Composite Materials Structure for Dual-mode Ramjet and Liquid Rocket Engines-2005 status. AIAA 2005–3434.

[26] Ortelt M, Hald H, Fischer I, et al. Empirical Verification of Effusion Cooled CMC Rocket thrust Chambers. AIAA 2005–3569.

[27] Mehta J M, Shouse D, Cox B, et al. Innovative SiC-SiC Ceramic Liner for the Trapped Vortex Combustor (TVC) Concept. AIAA 2004–689.

[28] Ohlhorst C W, Glass D E, Bruce W E, et al. Development of X-43A Mach10 Leading edges. IAC-05-D2.5.06, 2005.

[29] Li Q G, Zhou H J, Dong S M, et al. Fabrication and comparison of 3D Cf/ZrC-SiC composites using ZrC particles/polycarbosilane and ZrC precursor/polycarbosilane. Ceramics International, 2012, 38(6): 5271–5275.

[30] Padmavathi N, Kumari S, Prasad V V B, et al. Processing of carbon- fiber reinforced (SiC+ZrC) mini-composites by soft-solution approach and their characterization. Ceramics International, 2009, 35(8): 3447–3454.

[31] Va?en R, Jarligo M O, Steinke T, et al. Overview on advanced thermal barrier coatings. Surface & Coatings Technology, 2010, 205(4): 938–942.

[32] Blum Y D, Marschall J, Hui D, et al. Thick protective UHTC coatings for SiC-based structures: process establishment. Journal of the American Ceramic Society, 2008, 91(5): 1453–1460.

[33] Liu Q, Zhang L T, Liu J, et al. The oxidation behavior of SiC-ZrC-SiC-coated C/SiC minicomposites at ultrahigh temperatures. Journal of the American Ceramic Society, 2010, 93(12): 3990–3992.

[34] Xiang Y, Li W, Wang S, et al. Ablative property of ZrC-SiC multilayer coating for PIP-C/SiC composites under oxy-acetylene torch. Ceramics International, 2012, 38(4): 2893–2897.

[35] Liedtke V, Olivares I H, Langer M, et al. Manufacturing and performance testing of Sol/Gel based oxidation protection systems for re-usable space vehicles. Journal of the European Ceramic Society, 2007, 27(2/3): 1493–1502.

[36] GUO Chao-Bang, NIU Wen, LIU Wen-Jie. Research progress in TPS and thermal structure technology of HTV-2 vehicle. Winged Missiles Journal, 2012(1): 92–98.

[37] Wulz H G, Stark H, Trabandt U. Joining and Load Transfer Technology for Hot CMC Structures. AIAA 2000–2435.

[38] Paquette E L, Palko J. Hypersonic Airframe and Propulsion Seal preload Device Development for 2300F service. AIAA 2004–3888.

[39] Peng L N, He G Q, Liu P J. Experimental and Numerical Investigation of Active Cooling Ceramic Matrix Composite for Ramjet Propulsion System. AIAA 2009–5462.

C/SiC复合材料在超燃冲压发动机中的应用研究进展

Research Progress on the Application of C/SiC Composites in Scramjet

RichHTML

PDF (PC)

可视化

被引次数

摘要/Abstract

引用本文

使用本文

参考文献

相关文章 15

编辑推荐

Metrics

本文评价

[1]	丁玲, 蒋瑞, 唐子龙, 杨运琼. MXene材料的纳米工程及其作为超级电容器电极材料的研究进展[J]. 无机材料学报, 2023, 38(6): 619-633.
[2]	杨卓, 卢勇, 赵庆, 陈军. X射线衍射Rietveld精修及其在锂离子电池正极材料中的应用[J]. 无机材料学报, 2023, 38(6): 589-605.
[3]	陈强, 白书欣, 叶益聪. 热管理用高导热碳化硅陶瓷基复合材料研究进展[J]. 无机材料学报, 2023, 38(6): 634-646.
[4]	林俊良, 王占杰. 铁电超晶格的研究进展[J]. 无机材料学报, 2023, 38(6): 606-618.
[5]	牛嘉雪, 孙思, 柳鹏飞, 张晓东, 穆晓宇. 铜基纳米酶的特性及其生物医学应用[J]. 无机材料学报, 2023, 38(5): 489-502.
[6]	苑景坤, 熊书锋, 陈张伟. 聚合物前驱体转化陶瓷增材制造技术研究趋势与挑战[J]. 无机材料学报, 2023, 38(5): 477-488.
[7]	游钧淇, 李策, 杨栋梁, 孙林锋. 氧化物双介质层忆阻器的设计及应用[J]. 无机材料学报, 2023, 38(4): 387-398.
[8]	杜剑宇, 葛琛. 光电人工突触研究进展[J]. 无机材料学报, 2023, 38(4): 378-386.
[9]	杨洋, 崔航源, 祝影, 万昌锦, 万青. 柔性神经形态晶体管研究进展[J]. 无机材料学报, 2023, 38(4): 367-377.
[10]	齐占国, 刘磊, 王守志, 王国栋, 俞娇仙, 王忠新, 段秀兰, 徐现刚, 张雷. GaN单晶的HVPE生长与掺杂进展[J]. 无机材料学报, 2023, 38(3): 243-255.
[11]	林思琪, 李艾燃, 付晨光, 李荣斌, 金敏. Zintl相Mg₃X₂(X=Sb, Bi)基晶体生长及热电性能研究进展[J]. 无机材料学报, 2023, 38(3): 270-279.
[12]	张超逸, 唐慧丽, 李宪珂, 王庆国, 罗平, 吴锋, 张晨波, 薛艳艳, 徐军, 韩建峰, 逯占文. 新型GaN与ZnO衬底ScAlMgO₄晶体的研究进展[J]. 无机材料学报, 2023, 38(3): 228-242.
[13]	陈昆峰, 胡乾宇, 刘锋, 薛冬峰. 多尺度晶体材料的原位表征技术与计算模拟研究进展[J]. 无机材料学报, 2023, 38(3): 256-269.
[14]	刘岩, 张珂颖, 李天宇, 周菠, 刘学建, 黄政仁. 陶瓷材料电场辅助连接技术研究现状及发展趋势[J]. 无机材料学报, 2023, 38(2): 113-124.
[15]	谢兵, 蔡金峡, 王铜铜, 刘智勇, 姜胜林, 张海波. 高储能密度聚合物基多层复合电介质的研究进展[J]. 无机材料学报, 2023, 38(2): 137-147.