空间环境与碳/环氧复合材料交互作用的研究现状*

摘要
参考文献
相关文章 (1)

全文: PDF (2304 KB)
输出: BibTeX | EndNote (RIS)

摘要随着航天技术的迅速发展，要求航天器长寿命、高可靠性、高精度和多用途，这对航天器所用材料的性能提出了越来越高的要求。碳/环氧复合材料不仅具有密度小、比强度和比刚度高等特点，而且在真空条件下质损率低，热膨胀系数小，在航天领域得到了越来越广泛的应用。在大多数的空间环境因素的长期作用下，碳/环氧复合材料的各项性能将发生变化，进而会对航天器在轨服役的可靠性及寿命产生影响。

	服务

	把本文推荐给朋友
	加入我的书架
	加入引用管理器
	E-mail Alert
	RSS
	作者相关文章
	高禹
	徐晋伟
	王伯臣
	董尚利
	包建文

关键词 ：碳/环氧复合材料, 空间带电粒子辐射, 真空热循环, 辐照损伤

基金资助:*国家自然科学基金项目（50603014和51073094）、航空科学基金项目（2011ZF54019）、辽宁省高等学校杰出青年学者成长计划项目（LJQ2011013）资助。

引用本文:

高禹，徐晋伟，王伯臣，董尚利，包建文. 空间环境与碳/环氧复合材料交互作用的研究现状*[J]. 航空制造技术, 2012, 55(15): 66-69.

链接本文:

http://www.amte.net.cn/CN/ 或 http://www.amte.net.cn/CN/Y2012/V55/I15/66

[1]　Grossman E, Gouzman I. Space environment effects on polymers in low earth orbit. Nuclear Instruments and Methods in Physics Research B, 2003, 208: 48-57.
[2]　Dauphin J. Materials in space: working in a vacuum. Vacuum. 1982, 32 (10/11): 669.
[3]　薛大同，张景钦. 航天材料的真空性能. 中国国防科学技术报告. GF-A0017381G，1995.
[4]　达道安. 空间真空技术. 北京：宇航出版社，1995：12-27，335-411.
[5]　Sperber R S. Analysis of the public record of spacecraft Anomalies. AIAA-90-0781, 1990.
[6]　Wang B S, Chun G K, Chang S H, et al. Prediction of failure thermal cycles in graphite/epoxy composite materials under simulated low earth orbit environments. Composites Part B, 2000, 31: 223-235.
[7]　Gao Y, He S, Yang D, et al. Effect of vacuum thermo-cycling on physical properties of unidirectional M40J/AG-80 composites. Composites Part B-Engineering, 2005, 36: 351-358.
[8]　Guo Y, Dong S L, He S, et al. Characterization on stress distribution and thermal expansion behavior for M40J/AG-80 composites experienced vacuum thermo-cycling. Journal of Reinforced Plastics and Composites, 2006, 25(16): 1647-1657.
[9]　[苏联] T. C. 尼基季娜. 电离辐射对高聚物的作用. 杨昌正，译. 北京：中国工业出版社，1964.
[10]　张建可，冀勇夫，李智华，等. 粒子辐照对碳纤维复合材料力学性能的影响.中国空间科学技术, 1998，18(1)：56-59.
[11]　Evans D, Morgan J H. A review of the effects of ionizing radiation on plastic materials at low temperatures. Adv. Cryogenic Engng. (Materials), 1982, 28: 147-164.
[12]　Egusa S. Irradiation effects and degradation mechanism on the mechanical properties of polymer matrix composites at low temperatures. Adv. Cryogenic Eng. (Materials), 1990, 36: 861-868.
[13]　Megusar J. Low temperature fast-neutron and gamma irradiation of glass fiber/epoxy composite. Part 1: Deformation and Fracture. Journal of Nuclear Materials, 1996, 228: 168-175.
[14]　Gao Y, Dong S L, Yang D Z, et al. Damage effects of 120- keV electron radiation on AG-80 resin. Journal of Polymer Science: Part B: Polymer Physics, 2006, 44(1): 177-184.
[15]　Gao Y, Jiang S L, Sun M R, et al. Effect of Irradiation with < 200 keV electrons on AG-80 resin. Radiation Physics and Chemistry, 2005, 73(6): 348-354.
[16]　Wu S, Gedeon S, Fourecer R A, et al. The effect of γ-irradiation of the electrical properties of epoxy resin system. J. Uncler Materials, 1988 (151): 141-150.
[17]　Evans D, Reed R P. The permeability of resin based composite materials to radiolytic gases. Cryogenics, 1998, 38(1): 149-154.
[18]　Romanov V A, Khorasanov G L, Konstantinov I O, et al. Durability changes of epoxy resins under action of protons and gamma rays. Radiation Physics and Chemistry, 1995, 46(4-6): 863-866.
[19]　Snead C L, Morena J J, Czajkowski C J, et al. Mechanical-property changes of polymeric and composite materials after low-temperature proton irradiation. Materials Characterization, 1999, 42: 73-91.
[20]　Mishra R, Tripathy S P, et al. Optical and electrical properties of some electron and proton irradiated polymers. Nuclear Instruments and Methods in Physics Research B, 2000, 168: 59-64.
[21]　Gao Y, Jiang S P, Yang D Z, et al. A study on radiation effect of < 200 keV protons on M40J/Epoxy composites. Nuclear Instruments and Methods in Physics Research - Section B, 2005, 229(2): 261-268.
[22]　Gao Y, Jiang S L, Dong S L, et al. Effect of 120 keV proton irradiation on mass loss and chemical structure of AG-80 epoxy resin. Radiation Effects and Defects in Solids: Incorporating Plasma Science and Plasma Technology, 2010, 165(11): 857-867.