欢迎登录材料期刊网

材料期刊网

高级检索

连续纤维增强陶瓷基复合材料(CFRCMCs)因具有高比强、高比模、高可靠性、耐高温等优异性能,已成为航空航天、军事、能源等领域理想的高温结构材料.主要介绍了国外CFRCMCs在热防护系统、火箭发动机和超燃冲压发动机上应用的研究进展.

参考文献

[1] Anderson B L.X-38 program status/ overview[A].Arcachon,France,2001:26.
[2] Wulz H G;Trabandt U .Large integral hot CMC structures designed for future reusable launchers[AIAA,1997-2485][R].
[3] A.Muhlratzer;K.Handrick;H.Pfeiffer .Development of a new cost-effective ceramic composite for re-entry heat shield applications[J].Acta astronautica,1998(9):533-540.
[4] Ishikawa T;Ogasawara T .Overview of development activities of spaceplane components using NUSK-CMC (CMC with continuous Si-Ti-C-O fiber)[AIAA,2001-1879][R].
[5] Ogasawara T;Ishikawa T;Matsuzaki T .Thermal response and oxidation behaviorof Si-Ti-C-O fiber/Si-Ti-C-O ceramic matrix composites under atmospheric re-entry conditions[AIAA,2001-1779][R].
[6] 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[ADA,405477][R].
[7] Advanced Carbon Fiber Reinforced Silicon Carbide Technology For SM3 Divert and Attitude Control Systems[R].FMI
[8] 张建艺.陶瓷基复合材料在喷管上的应用[J].宇航材料工艺,2000(04):14-16.
[9] Mathieu A;Monteuuis B;Gounot V .Ceramic matrix composite materials for a low thrust bipropellant rocket engine[AIAA,90-2054][R].
[10] Papenburg U;Beyer S;Laube H.Advanced ceramic matrix composites (CMC's) for space propulsion systems[M].AIAA,1997
[11] Beyer S;Strobe F;Knabe H .Development and testing of C/SiC components for liquid rocket propulsion applications[AIAA,99-2896][R].
[12] Dirling Ray B Jr .Progress in materials and structures evaluation for the HyTech program[AIAA,98-1591][R].
[13] Paquette E;Warburton R;Eckel A .Cooled CMC scramjet combustor structure development[AIAA,2002-4132][R].
[14] Bouquet C;Fischer R;Larrier J M et al.Composite technologies development status for scramjet applications[AIAA,2003-6917][R].
[15] Uhrig G;Larrier J M .Towards an all composite SCRAMJET combustor[AIAA,2002-3883][R].
[16] Bouquet C;Luc-Bouhali A;Lawrence T et al.Ceramic matrix composites cooled panel development for advanced propulsion systems[AIAA,2004-1998][R].
[17] Bouquet C;Luc-Bouhali A et al.Validation of a leak-free C/SiC heat exchanger technology[AIAA,2003-6918][R].
上一张 下一张
上一张 下一张
计量
  • 下载量()
  • 访问量()
文章评分
  • 您的评分:
  • 1
    0%
  • 2
    0%
  • 3
    0%
  • 4
    0%
  • 5
    0%