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热真空环境对常用胶接材料性能的影响 被引量:1

Effect of Thermal Vacuum Environment on Performance of Adhesive Bonding Materials
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摘要 空间的热真空环境是造成光电子器件胶接材料性能退化和放气污染的重要因素。为此,考察了几类典型胶接材料的热真空老化和热真空挥发特性,分析了热真空老化后的力学性能变化及真空挥发产物的主要来源,并对热真空挥发预处理方法进行了验证。结果表明软质的硅橡胶与硬质的环氧树脂胶和丙烯酸树脂胶相比有着更大的质量损失,且含有端羟基的缩聚型硅橡胶和环氧树脂胶真空老化后的模量变化较大。通过真空预处理可以作为降低固化胶真空挥发产物来源的一种有效手段。可为宇航用光电子器件胶接材料的设计选型提供参考依据。 The thermal vacuum of space condition is an important factor to cause properties degradation and out-gassing contamination of adhesive bonding materials used in optic-electrical components. The thermal vacuum aging and volatile characteristic of several typical adhesive bonding materials were investigated. The change of mechanical properties and the source of volatile after thermal vacuum test were analyzed and discussed, and the pretreatment method under thermal vacuum condition were validated and analyzed. The results indicate that the soft silicone rubber adhesive display greater mass loss than that of harder epoxy resin and acrylic resin adhesives, and the condensation type silicone rubber and epoxy resin adhesives appear greater changes of modulus because of end hydroxyl group exist in their molecular structures. The pretreatment method under thermal vacuum condition could be used as an effective measure to reduce the outgassing contamination of adhesive bonding materials. The results are important for the design and screening of nonmetallic materials used in optic-electrical components.
出处 《宇航材料工艺》 CAS CSCD 北大核心 2012年第6期92-96,共5页 Aerospace Materials & Technology
关键词 光电子器件 胶接 热真空老化 真空挥发产物 预处理方法 Optic-electrical components, Adhesive bonding materials,Thermal vacuum aging, Outgassing ingre-dients, Pretreatment method
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参考文献14

  • 1徐坚,杨斌,杨猛,蔡震波.空间紫外辐照对高分子材料破坏机理研究综述[J].航天器环境工程,2011,28(1):25-30. 被引量:27
  • 2Gmssman E, Gouzman I. Space environment effects polymer in low earth orbit [ J ]. Nuclear instruments and methods in physics research, 2003,208 ( 8 ) :48-57.
  • 3James S Dyer. , Richard C Benson, Terry E Phillips, et al. Outgassing analysis performed during vacuum bakeout of com- ponents painted with chemglaze Z306/9922 [ J ]. SPIR. Optical System Contamination, 1992, 1754:177.
  • 4Claney H M. S R V. SANPE J. 1971,7(4) :17.
  • 5Thorn J. I A, Whipple C L [ C ]//Pooc. 11th National SAMPE Symposium, 1967 : 11217.
  • 6Heinish R P. Light splitter from contaminated space- craft windows[ R]. AIAA, 1971:71-472.
  • 7湛永钟,张国定.低地球轨道环境对材料的影响[J].宇航材料工艺,2003,33(1):1-5. 被引量:32
  • 8Leger L J, Bricker RW. Apollo experience report: win- dow contamination[ R]. NASA TND-6721, 1972.
  • 9Campbell W A et al. An outgassing data compilation of spacecraft materials[ J]. 1978, 1014.
  • 10Haefer R A. Vacuum and cryotechniques in space re- search[J]. Vacuum,1972,22(8):303-314.

二级参考文献63

  • 1顾培韵.聚合物系的脱挥发分设备[J].合成橡胶工业,1994,17(4):195-199. 被引量:11
  • 2童靖宇,刘向鹏,孙刚,姜利祥,李金洪,多树旺,李美栓.原子氧/紫外综合环境模拟实验与防护技术[J].真空科学与技术学报,2006,26(4):263-267. 被引量:13
  • 3都亨 叶宗海.低轨道航天器空间环境手册[M].北京:国防工业,1996..
  • 4.人造地球卫星环境手册[M].工业出版社,1971.43.
  • 5Koontz S, Leger L, Albyn K. Vacuum ultraviolet radiation/atomic oxygen synergism in materials reativity. Journal of Spacecraft, 1990;27(3) : 346 - 348.
  • 6Ayala A, Murr L E. Some observaions of multi-layer penetration by micrometeoroid particles in low-earth orbit. Scripta Metallurgica et Materialia, 1994;31(10): 1409- 1412.
  • 7Zolensky M, Atkinson D, See T et al. Meteoroid and orbital debris record of the Long Duration Exposure Facility' s frame.Journal of Spacecraft, 1991 ; 28(2) : 204-209.
  • 8Berthoud L, Mandeville J C. Material damage in space from microparticle impact. Journal of Materials Science, 1997; 32(11): 3043-3048.
  • 9Heinish R P. Light scatter from contaminated spacecraft windows. ALAA,71 - 472,1971.
  • 10Leger L J, Brieker R W. Apollo experience report: window contamination. NASA TND- 6721,1972.

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