欢迎登录材料期刊网

材料期刊网

高级检索

通过对环氧树脂、NOL环力学性能、金属内衬表面性能、复合材料真空质损和复合材料气瓶性能等进行研究和分析,研制出一种用于卫星推进系统的复合材料气瓶.结果表明:该复合材料气瓶经150次疲劳试验后爆破压强为86 MPa,容器特征系数达57.7 km,且满足真空使用环境要求.

参考文献

[1] Haddock R C;Darms F J .Space system applicantions of advanced composite fiber/Metal pressure vessels[J].American Institute of Aeronautics and Astronautics,1990,2227:128.
[2] Edgar E .Advances in Composite Fiber/Metal Pressure Vessels Technology[J].American Institute of Aeronautics and Astronautics,1989,2643:1210.
[3] Morris E E;Segimoto M;Lynn V .Lighter weight fiber/ metal pressure vessels using carbon overwrap[J].American Institute of Aeronautics and Astronautics,1986,1504:129.
[4] Braun C A .Advanced composite fiber/Metal pressure vessels for space system applications[J].American Institute of Aeronautics and Astronautics,1991,1976:1211.
[5] Chen H C;Chiu S T;Chang J B .Impact damage effects on composite over wrapped pressure vessels[J].American Institute of Aeronautics and Astronautics,1999,1321:1065.
[6] 张天平.空间应用压力容器研制技术[J].上海航天,2002(01):55-58.
[7] 林再文,李涛,孙浩伟,王明寅.几种纤维复合材料压力容器的性能对比研究[J].纤维复合材料,2005(01):21-22.
[8] 王荣国,矫维成,刘文博,杨帆,赫晓东.轻量化复合材料压力容器研究进展[J].航空制造技术,2009(15):86-89.
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%