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空间充气膨胀展开结构的可控刚化技术 被引量:6

RIGIDIZATION ON COMMAND OF SPACE INFLATABLE STRUCTURES
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摘要 刚化技术是空间充气膨胀展开结构的一项关键技术。Adherent Technologies有限公司的技术人员首次提出了"可控刚化"(Rigidization On Command-ROC)技术概念,利用此技术ILC Dover公司制造了空间充气膨胀展开结构的示范支撑管件。和传统的刚化技术相比可控刚化技术有许多优点,此技术可控、清洁,适用于空间的特殊环境。作者对空间充气膨胀展开结构刚化技术、可控刚化技术、可控刚化技术所用材料和紫外光(UV)固化复合材料进行了简单介绍。可控刚化技术可靠性高,固化后复合材料的机械性能好,为空间充气可膨胀展开结构提供一种急需的刚化技术,能满足充气膨胀展开结构多项任务的需要。 The rigidization technology is a key technology of space inflatable structures.The concept of Rigidization-On- Command (ROC) is proposed by the researchers of Adherent Technologies, Inc. for the first time and a cured demonstration tube is made at ILC Dover. This technology has many advantages compared to the approaches to rigidization in the past. It provided a controlled, clean rigidization technology to harden inflatable structure.The curing technologies of space inflatable structures, Rigidization-On-Command technology , the materials of ROC and the UV cured composite materials are introduced briefly in this paper. The ROC technology can provide a badly needed technology for the space inflatable structures. It can offer high reliability,good dynamic charateristics and can provide a much needed technology for the inflatable community.
出处 《真空与低温》 2009年第3期125-130,共6页 Vacuum and Cryogenics
基金 表面工程技术国家级重点实验室基金(9140C5404010804) 兰州交通大学"青蓝"人才工程基金(QL-08-02A)资助
关键词 空间充气膨胀展开结构 可控刚化 紫外光固化 阳离子光引发剂 inflatable space structures rigidization on eommand UV curing cationic photoinitiator
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  • 1FREELAND R E, BILYEU G D, VEAL G R, et al. Inflatable deployable space structures technology summary [A]. Proceedings of the49^th International Astmnautical Congress [C]. Melbourne : International Astronautical Federation, 1998. 1-10.
  • 2DAROOKA D K, JENSEN D W. Advanced space structure concepts and their development [A].Proceedings of the 42nd AIAA/ASME/ ASCE/AHS/ASC Structures , Structural Dynamics , and Materials Conference [C]. Seattle : American Institute of Aeronautics and Astronautics, 2001. 1-10.
  • 3DAVID P C, STEPHEN E S, FREDERIC D E. Rigidizable Materials for use in Gossamer Space Inflatable Structures[R].AIAA-2001 -1417.
  • 4刘宇艳,孟秋影,谭惠丰,杜星文.空间充气展开结构用刚化材料和刚化技术的研究现状[J].材料工程,2008,36(2):76-80. 被引量:6
  • 5孙凯,杨光,黄鹏程.用紫外光固化复合材料制备充气展开器件的研究[J].宇航材料工艺,2003,33(6):25-29. 被引量:7
  • 6RONALD A ,LARRY H, ANDREA H, et al, Inflatable Spacecraft using "Rigidization--on-Command Concept'American Institute of Aeronautics and Ast ronautics[R]. AIAA-2000-1637.
  • 7聂俊,何勇,孙梦洲.紫外阳离子光固化研究进展[J].涂料技术与文摘,2007,28(10):1-4. 被引量:10
  • 8吴宗南,刘红波.紫外光固化涂料的研究进展[J].广东化工,2009,36(2):52-55. 被引量:6
  • 9CRIVELLO, J V, YOUNG S. The Synthesis and Cationic Photopolymerization of Monomers. Based on Dicyclopentadience [J].J Polym Sei, Part A:Polym Chem, 1999 ,(37): 3427-3440.
  • 10CRIVELLO J V. The discovery and development of onium salt cationic photoinitiators [J]. J Polym Sci, Part A: Polym Chem 1999, 37(23): 4241-4254.

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