近年来先进复合材料已经成为航空航天结构的基本材料之一.为满足航空业对高性能低成本制备工艺技术和减重方面的高要求,先进复合材料以其相对密度小、质损率低、比强度比模量高、耐高温性能好、热膨胀系数小、耐疲劳性能优越等独特优点获得广泛应用,并具有极大的发展潜力.文中从应用状况、环境损伤行为与机理、国内外发展形势等角度对炭/双马复合材料的研究进展进行了全面系统的回顾与总结,并对今后的发展和研究方向作了探讨,供我国在该领域的研究和应用参考.
参考文献
| [1] | 张小达,吕维鉴.国外运载器、航天器从地面到空间自然环境标准综述[J].航天标准化,2001(01):29-33. |
| [2] | 谭立忠,朱风云.美国X-37B轫道试验飞行器发展研究[J].飞航导弹,2011(06):33-36. |
| [3] | 夏群力,何镜,徐平,温求遒.高超声速临近空间飞行器发展现状与研究措施[C].第三届中国航空学会青年科技论坛论文集,2008:72-77. |
| [4] | Joo-Hyun Han;Chun-Gon Kim .Low earth orbit space environment simulation and its effects on graphite/epoxy composites[J].Composite structures,2006(2):218-226. |
| [5] | 王汝敏,蓝立文.先进复合材料用热固性树脂基体的发展[J].热固性树脂,2001(01):36-38. |
| [6] | 于翘.复合材料在航天领域发展的新动向[C].中国复合材料学会2003年学术年会论文集,2003:24-27. |
| [7] | Satoshi Kobayashi;Nobuo Takeda .Experimental characterization of microscopic damage behavior in carbon/bismaleimide composite--effects of temperature and laminate configuration[J].Composites, Part A. Applied science and manufacturing,2002(11):1529-1538. |
| [8] | Awaja, F.;Moon, J.B.;Gilbert, M.;Zhang, S.;Kim, C.G.;Pigram, P.J. .Surface molecular degradation of selected high performance polymer composites under low earth orbit environmental conditions[J].Polymer Degradation and Stability,2011(7):1301-1309. |
| [9] | 高禹,李志君,杨德庄,何世禹,覃耀春.真空热循环对单向M40J/5228A复合材料质损率和线膨胀系数的影响[J].复合材料学报,2004(06):108-113. |
| [10] | Gao Yu;Yang De-zhuang;Xiao Jing-dong;He Shi-yu;Li Zhi-jun .Effect of Proton Irradiation on Mechanical Properties of Carbon/Epoxy Composites[J].Journal of spacecraft and rockets,2006(3):505-508. |
| [11] | Yann Goueffon;Gregory Aldebert;Catherine Mabru;Laurent Arurault;Claire Tonon;Pascale Guigue .Flaking of black anodic films in space environment: Ageing and numerical simulation[J].Mechanics of materials,2012(Feb.):72-82. |
| [12] | Peterson EC;Patil RR;Kallmeyer AR;Kellogg KG .A micromechanical damage model for carbon fiber composites at reduced temperatures[J].Journal of Composite Materials,2008(19):2063-2082. |
| [13] | 高禹,代小杰,董尚利,陆春,包建文.热循环作用下单向炭纤维/环氧树脂复合材料的热应力[J].高分子材料科学与工程,2012(09):178-181. |
| [14] | Vernon T. Bechel;Mark B. Fredin;Steven L. Donaldson .Effect of stacking sequence on micro-cracking in a cryogenically cycled carbon/bismaleimide composite[J].Composites, Part A. Applied science and manufacturing,2003(7):663-672. |
| [15] | Kwang--Bok Shin;Chun-Gon Kim;Chang--Sun Hong .Prediction of failure thermal cycles in graphite/epoxy composite materials under simulated low earth orbit environments[J].Composites, Part B. Engineering,2000(3):223-235. |
| [16] | Gao Y;Dong SL;He S;Yang DZ;Li ZJ .Characterization of stress distribution and thermal expansion behavior for M40J/AG-80 composites experienced vacuum thermo-cycling[J].Journal of Reinforced Plastics and Composites,2006(16):1647-1657. |
| [17] | Yu Gao;Song He;Dezhuang Yang;Yong Liu;Zhijun Li .Effect of vacuum thermo-cycling on physical properties of unidirectional M40J/AG-80 composites[J].Composites, Part B. Engineering,2005(4):351-358. |
| [18] | Schutz JB. .Properties of composite materials for cryogenic applications[J].Cryogenics,1998(1):3-12. |
| [19] | T. Ueki;S. Nishijima;Y. Izumi .Designing of epoxy resin systems for cryogenic use[J].Cryogenics,2005(2):141-148. |
| [20] | Ran Y. Kim;Steve L. Donaldson .Experimental and analytical studies on the damage initiation in composite laminates at cryogenic temperatures[J].Composite structures,2006(1/2):62-66. |
| [21] | 王绍权 .液氮浸渍对C/BMI复合材料性能的影响[D].哈尔滨工业大学,2012. |
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