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[1]冯 雪,沈 俊,田 桂,等.复合材料压力容器在航天领域的应用研究[J].火箭推进,2014,40(04):35-42.
　FENG Xue,SHEN Jun,TIAN Gui,et al.Research of composite over-wrapped pressure vessels for space application[J].Journal of Rocket Propulsion,2014,40(04):35-42.
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复合材料压力容器在航天领域的应用研究

《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V] 卷: 40 期数: 2014年04期 页码: 35-42 栏目: 研究与设计 出版日期: 2014-08-28
Title:
Research of composite over-wrapped pressure vessels for space application
作者:
冯 雪; 沈 俊; 田 桂; 晏 飞
上海空间推进研究所，上海201112
Author(s):
FENG Xue;  SHEN Jun;  TIAN Gui;  YAN Fei
Shanghai Institute of Space Propulsion, Shanghai 201112, China
关键词:
复合材料压力容器; 应用研究;  树脂基体选择;  无损检测
Keywords:
composite pressure vessel;  application research;  resin matrix selection;  nondestructive inspection
分类号:
V432-34
文献标志码:
A
摘要:
综述了复合材料压力容器在航天领域的最新应用进展，列举了国外空间系统应用的几个典型实例，从金属内衬、纤维材料及树脂基体方面给出了比较重要的技术信息。论述了低温复合材料压力容器的研发与应用趋势，金属内衬和缠绕纤维在低温环境下的性能表现优异及低温环境下树脂基体的选择。探讨了复合材料压力容器无损检测方法的研究现状及展望。未来复合材料压力容器无损检测技术将向着高效实时、精确定位、定量分析及由局部缺陷检测向整体缺陷检测的方向发展。
Abstract:
The latest development of composite over-wrapped pressure vessels (COPVs) for space applications are summarized based on a study of published literatures and some typical samples on applications of overseas spacecrafts are introduced in this paper. Besides, some valuable information about the metal liner, fiber and resin matrix of COPVs is presented respectively. R&D and application trends of cryogenic composite pressure vessel are described. The properties of the metal liner and fiber behave very well in cryogenic temperature environment. The selection principles of resin matrix in cryogenic temperature environment are pointed out emphatically. The research status and prospect of nondestructive detection for COPVs are discussed. It is pointed out that COPV NDE technologies will advance to high efficiency, real time, precise positioning, quantitative analysis and overall defect detection.

参考文献/References:

[1]MCLAUGHLAN P B, FORTH S C, GRIMES-LEDESMA L. Composite overwrapped pressure vessels, NASA SP-2011-573[R]. USA: NASA, 2011.
[2]张天平. 空间应用复合材料压力容器研究技术[J]. 上海航天, 2002 (1): 54-58.
[3]CHANG J B. Development of COPV-related standards, AIAA2007-2146[R]. USA: AIAA, 2007.
[4]侯继东. 国外复合材料压力容器的发展及应用[J]. 载人航天信息, 1995 (4): 34-37.
[5]王荣国, 矫维成, 刘文博, 等. 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.
[6]SCHNEIDER J, DYESS M, HASTINGS C, et al. Light- weight cryogenic composite over-wrapped pressure vessels (COPVS) for launch vehicle applications, AIAA 2007-2148[R]. USA: AIAA, 2007.
[7]MALLICK K, CRONIN J, RYAN K, et al. An integrated systematic approach to linerless composite tank development, AIAA 2005-2089[R]. USA: AIAA, 2005.
[8]PATTERSON J, DELAY T. Material evaluation for filament wound pressure vessels[C]//Proceedings of 46th International SAMPE Symposium and Exhibition on a Materials and Processes Odyssey. California, USA: [s.n.], 2001:1307-1315.
[9]郑传祥. 复合材料压力容器[M]. 北京: 化学工业出版社, 2006.
[10]杜善义. 先进复合材料与航空航天[J]. 复合材料学报, 2007, 24(1): 1-12.
[11]HARRIS J, GRANDE R, HIGGINS M. Ultralight propellant tank for NASA space technology, AIAA 2003- 4608[R]. USA: AIAA, 2003.
[12]OLSON M A. Super robust and ultra-light pressure vessels using new technology[C]// Proceedings of 49th International SAMPE Symposium and Exhibition on Ma- terials and Processing Technology. California, USA: [s.n.], 2004: 111-120.
[13]RAY D M, GREENE N J, REVILOCK D, et al. High pressure composite overwrapped pressure vessel (COPV) development tests at cryogenic temperatures, AIAA 2008-1912[R]. USA: AIAA, 2008.
[14]PATTERSON J, DELAY T, SCHNEIDER J, et al. High pressure COPVS for cryogenic storage applications, AIAA 2006-4718 [R]. USA: AIAA, 2006.
[15]DELAY T, PATTERSON J, SCHNEIDER J, et al. Development of composite overwrapped pressure vessels for high pressure cryogenic storage applications [C]//Proceedings of 51st International SAMPE Symposium and Exhibition on Creating New Opportunities for the World Economy. California, USA:[s.n.], 2006: 11-18.
[16]SAULSBERRY R, GREENE N, CAMERON K, et al. Nondestructive methods and special test instrumentation supporting NASA composite overwrapped pressure vessel assessments, AIAA 2007-2324[R]. USA: AIAA, 2007.
[17]赫晓东, 赵俊青, 王荣国, 等. 复合材料压力容器无损检测研究现状[J]. 哈尔滨工业大学学报, 2009, 41(12): 78-82.

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备注/Memo

收稿日期：2014-01-22；修回日期：2014-03-26 作者简介：冯雪（1980—），女，硕士，研究领域为空间压力容器

更新日期/Last Update: 1900-01-01