航天推进技术研究院主办
[1]刘志泉,马武军.C/SiC复合材料推力室应用研究[J].火箭推进,2011,37(02):19-24.
LIU Zhi-quan,MA Wu-jun.Applied research of rocket engine thrusters made of ceramic matrix composite[J].Journal of Rocket Propulsion,2011,37(02):19-24.
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LIU Zhi-quan,MA Wu-jun.Applied research of rocket engine thrusters made of ceramic matrix composite[J].Journal of Rocket Propulsion,2011,37(02):19-24.
C/SiC复合材料推力室应用研究
《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V]
卷:
37
期数:
2011年02期
页码:
19-24
栏目:
研究与设计
出版日期:
2011-04-15
- Title:
- Applied research of rocket engine thrusters made of ceramic matrix composite
- 文章编号:
- 1672-9374(2011)02-0025-05
- 关键词:
- C/SiC复合材料推力室; 液体火箭发动机; 焊接连接
- Keywords:
- carbon fiber reinforced silicon carbide (C/SiC) composite thruster; liquid-propellant rocket engine; welding joint
- 分类号:
- V434-34
- 文献标志码:
- A
- 摘要:
- C/SiC复合材料密度低、耐高温、抗氧化、抗烧蚀，并且具有非常好的高温力学性能，是制备高性能液体火箭发动机推力室的理想材料。本文从C/SiC复合材料燃烧室结构计算、无损探伤及C/SiC与金属连接等方面，论述了上海空间研究所在C/SiC复合材料应用于液体火箭发动机推力室方面的基础研究及应用进展。
- Abstract:
- Carbon fiber reinforced silicon carbide (C/SiC) composite has low density, high oxidation and erosion resistance, as well as high mechanical performance at high temperature. Therefore, it is the most perfect material to fabricate thrust chamber which is used in liquid propellant rocket engine. The development and application of rocket engine thrusters made of the ceramic matrix composite in Shanghai Institute of Space Propulsion (SISP) are described in the aspects of nondestructive inspection, structural computation, and welding joint of C/SiC ceramic matrix composites and metal materials.
参考文献/References:
[1]邹武, 张康助, 张立同. 陶瓷基复合材料在液体火箭发动机上的应用[J]. 固体火箭技术, 2000, (2):63-67.
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[3]STEFFIER W S, SHINAVSKI R J, RUSNAK C F, et al. Improved performance and durability of liquid propulsion rocket thrusters fabricated from triaxially braided C-SiC intraply hybrid-fiber/SiC matrix composites, ADA405477 [R]. USA: ADA, 2005.
[4]MARTIN Minthorn. Advanced carbon fiber reinforced silicon carbide technology for SM3 divert and attitude control systems, N96-284[R]. [S. l.]: Fiber Material Inc., 2002.
[5]SCHMIDT S, BEYER S, KNABE H, et al. Advanced ceramic matrix composites materials for current and future propulsion technology applications[J]. Acta Astronautica, 2004, 55 (3-9): 409-420.
[6]杨海涛. 压力容器的安全与强度计算[M]. 天津: 天津科学技术出版社, 1985.
[7]陈烈民, 杨宝宁. 复合材料的力学分析[M]. 北京: 中国科学技术出版社, 2006.
[8]任家烈, 吴爱萍. 先进材料的连接[M]． 北京: 机械工业出版社, 2000.
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备注/Memo
收稿日期：2010-10-15；修回日期：2010-12-15
作者简介： 刘志泉（1978—），男，工程师，研究领域为高室压、快响应复合材料液体轨控发动
更新日期/Last Update:
1900-01-01