介绍了喷管炭/炭材料出口锥(CCEC)预制体结构的设计原则、3种预制体成型技术,并简要讨论了预制体结构对炭/炭出口锥材料性能的影响.预制体结构设计须依据喷管工作条件,满足性能稳定、结构稳定、工艺易实现性原则;三维结构和非织造结构比二维结构预制体纤维含量高、性能更优,适合喷管出口锥的预制成型;预制体的结构均匀性、纤维含量是影响CCEC烧蚀性能的关键参数;可通过建立CCCs宏观力学性能与预制体细观结构参数之间的模型预测其结构性能.
参考文献
[1] | Cook J;Carwford J A.Multidirectional substracts for advanced composites,paper presented at the 76th Ann[A].Chicago,1975:211. |
[2] | 扬国华.碳素材料[M].北京:中国物资出版社,1999 |
[3] | 陈华辉.现代复合材料[M].北京:中国物资出版社,1997 |
[4] | 贺福;王茂章.碳纤维及其复合材料[M].北京:科学出版社,1995 |
[5] | Erich Fitzer;Manocha L M.Carbon reiforcements and carbon/carbon composites[M].,1998:178. |
[6] | Lamere G C et al.MX first stage nozzle development[R].AD A103844 |
[7] | Russell A Ellis .Testing of Novoltex 3D Carbon-Carbon Interal throat and cones(ITECs)[R].AIAA-88-3361 |
[8] | Boury D;Filipuzzl L .Sepcarb Materials For Solid Rocket Booster Nozzle Components[R].AIAA 2001-3438,2001. |
[9] | Boury D;Munoz A Albert .Ariane5 SRM nozzle evolution[R].AIAA2002-4193 |
[10] | Donguy P;EllisR A .An advanced nozzle for space motor[R].AIAA1980-130 |
[11] | Donald L Schmidt .Unique applications of carbon-carbon composite materials[J].SAMPE Journal,1999,35(04):32. |
[12] | Montaudon M .Novoltex textures for thermostrctural material[R].AIAA1991-1848 |
[13] | 杨南生;叶定友;许定宇.固体火箭发动机设计与研究[M].北京:宇航出版社,1992 |
[14] | 宋桂明,周玉,王玉金,雷廷权.固体火箭发动机喉衬材料[J].固体火箭技术,1998(02):51. |
[15] | 许正辉;朱良杰;王俊山.3D炭/炭复合材料用碳纤维的选择[A].,1995:142. |
[16] | 刘建军,李铁虎,郝志彪.喉衬热环境与碳/碳复合材料的烧蚀[J].宇航材料工艺,2005(01):42-48. |
[17] | 蔡体敏;马丽滨.喷管喉衬温度场计算影响因素的数值分析[J].固体火箭技术,1988(04):46. |
[18] | Lachman W L et al.Multidirectional reinforced carbon-carbon composites[J].Metall Soc AIME,1978,4:213. |
[19] | Lugerm.Fabric composites[A].,1984:4:35. |
[20] | Fitzer E;Monacha L M.Carbon fibers[A].New York:Springer-verlag,1997:66. |
[21] | GB 2234-1989.GB 2234-1989.Munufacture of carbon fibre perform[S].,1980-09-01. |
[22] | Canfield A R .Braided Shaped Filamentary Structures and method of making[P].EP 0528336,1979-07-03. |
[23] | 苏君明 .俄罗斯和乌克兰固体火箭发动机炭/炭喉衬及延伸锥技术[R].出国考察技术报告,1993. |
[24] | Canfield A R .Braided carbon/carbon nozzle develiopment[R].AIAA 85-1096 |
[25] | Bussiere M;Prel M.Ariane v solid rocket booster nozzle development status[A]. |
[26] | Broquere B .Carbon/Carbon nozzle exit cones SEP's xperence and ne development[R].AIAA J,97-2674 |
[27] | Leith Steven D .Carbon fibrer-reinforced carbon composite materrial[P].US 5071700,1983-10-12. |
[28] | Aly-Hassan;Mohamed Hatta et al.Conparison of 2D and 3D carbon/carbon composites with respect to damage and fracture resistance[J].CARBON,2003,41(05):1069. |
[29] | Borie V;Brulard J .Carbon firber/phenolic exit cone to replace C/C in SCICBM composites and adhesivers[J].News Lett,1991,7(05):5. |
[30] | Windhorst T;Blount G .Carbon-carbon composites:a summary of recent developments and applications[J].Materials & Design,1997,18(01):11. |
[31] | 蔡顺才;刘侃.固体发动机用低成本低烧蚀喉衬材料[J].飞航导弹,1995(12):34. |
[32] | 刘建军;苏君明;陈长乐.[A].上海,1998:10. |
[33] | Aly-Hassan;Mohamed Hatta et al.Conparison of 2D and 3D carbon/carbon composites with respect to damage and fracture resistance[J].CARBON,2003,41(05):1069. |
[34] | 陶肖明;冼杏娟;高冠勋.纺织结构复合材料[M].北京:科学出版社,2001:291. |
[35] | Ko Frank K;Chritipher M P.Structure and properties of an integrated 3D-fabric for structural composites[A].,1985:428. |
[36] | Yang J M;Chou T M .Fiber inclination model of three dimensional textile structural composites[J].Journal of Composite Materials,1986,20(05):472. |
[37] | Wu D L .Three-cell model and 5D braided structural composites[J].Computer Science & Technology,1996,56(03):225. |
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:
-
10%
-
20%
-
30%
-
40%
-
50%