欢迎登录材料期刊网

材料期刊网

高级检索

先进复合材料以其轻质高强、可设计性等特点,在航空航天等领域得到了广泛的应用.本文概述了复合材料在航空航天领域用作飞行器结构的发展历程,进而从更高效、可靠及大量应用角度,重点介绍了复合材料结构设计、增强体与基体材料、复合成型工艺及性能检测评价等结构复合材料之四大方面核心技术的研究动向与发展趋势.同时展望了新一代复合材料——碳纳米管复合材料发展及其在航空航天领域的应用前景.

参考文献

[1] 陈绍杰.复合材料技术与大型飞机[J].航空学报,2008(03):605-610.
[2] 曹春晓.一代材料技术,一代大型飞机[J].航空学报,2008(03):701-706.
[3] 王兴刚,于洋,李树茂,王明寅.先进热塑性树脂基复合材料在航天航空上的应用[J].纤维复合材料,2011(02):44-47.
[4] Deo R B;Starnes J H;Holzwarth R C.Low-cost composite materials and structures for aircraft applications[A].Norway,2001
[5] Hinrichsen J;Bautista C .The challenge of reducing both airframe weight and manufacturing cost[J].Air & Space Europe,2001,3(03):119-121.
[6] 张佐光,李敏,陈绍杰.飞机结构用先进复合材料的应用与发展[C].第十四届全国复合材料学术会议论文集(上),2006:28-34.
[7] 姚俊,孙达,姚振强,张普,张满朝,史瑞航.复合材料自动铺带技术现状与研究进展[J].机械设计与研究,2011(04):60-65.
[8] Marsh G .Automating aerospace composites production with fiber placement[J].REINFORCED PLASTICS,2011,55(03):32-37.
[9] Bruce M .Automating Composites Fabrication to Meet IncreasedThroughut Required by Industries Ranging from AerospacetoWind Energy,Automation Speeds Composite Production[J].MANUFACTURING ENGINEERING,2008,140(04)
[10] Bond G G;Griffith J M;Hahn G L et al.Non-Autoclave (Prepreg) Manufacturing Technology[R].BOEING CO SEATTLE WA PHANTOM WORKS,2008.
[11] Sutter J K;Kenner W S;Pelham L.Comparison of autoclave and out-of-autoclave composites[A].,2010
[12] Schwartz M.Innovations in materials manufacturing,fabrication,and environmental safety[M].CRC press,2010:507-508.
[13] Kaps R;Herbeck L;Herrmann A.Hybrid fabrication route-cost efficient CFRP primary airframe structures[A].,2006
[14] Aoki Y;Nagao Y;Takeda SI;Kuratani Y.Integral fabrication of composite fuselage structure using VARTMprepreg hybrid process[A].Paris,France,2011
[15] C. Di Fratta;M. Danzi;V. Gabathuler .Approach to Optimizing a Combined Out-of-Autoclave (OOA) Prepreg/Liquid Composite Molding (LCM) Process for Integrated Structures[J].SAMPE Journal,2012(5):40-46.
[16] Xu W;Gu Y;Li M et al.Co-curing process combining resin film infusion with prepreg and co-cured interlaminar properties of carbon fiber composites[J].Journal of Composite Materials,2013,48(14):1709-1724.
[17] X.Q. Ma;Y.Z. Gu;M. Li .Properties of Carbon Fiber Composite Laminates Fabricated by Coresin Film Infusion Process for Different Prepreg Materials[J].Polymer Composites,2013(12):2008-2018.
[18] Ma X;Gu Y.Manufacture and characterization of carbon fiber composite stiffened skin by resin film iufusion/prepreg co-curing process[J].Journal of Reinforced Plastics and Composites,2014:0731684414543213.
[19] Delaloye S;Niedermeier M .Optimization of the diaphragm forming process for continuous fibre-reinforced advanced thermoplastic composites[J].COMPOSITES MANUFACTURING,1995,6(03):135-144.
[20] S. G. Pantelakis;E. A. Baxevani .Optimization of the diaphragm forming process with regard to product quality and cost[J].Composites, Part A. Applied science and manufacturing,2002(4):459-470.
[21] Yu X;Ye L;Mai Y.W et al.Finite element simulations of the double diaphragmforming process[J].Revue Européenne des (E)léments,2005,14(6-7):633-651.
[22] Jing Sun;Yizhuo Gu;Min Li .Effect of forming temperature on the quality of hot diaphragm formed C-shaped thermosetting composite laminates[J].Journal of Reinforced Plastics and Composites,2012(16):1074-1087.
[23] X. X. Bian;Y. Z. Gu;J. Sun .Effects of Processing Parameters on the Forming Quality of C-Shaped Thermosetting Composite Laminates in Hot Diaphragm Forming Process[J].Applied composite materials,2013(5):927-945.
[24] 马保全,周正干.航空航天复合材料结构非接触无损检测技术的进展及发展趋势[J].航空学报,2014(7):1787-1803.
[25] Palmer S B;Dixon S .Industrially viable non-contact ultrasound[J].Insight-Non-Destructive Testing and Condition Monitoring,2003,45(03):211-217.
[26] Ryley A C;Kharkovsky S;Daniels D.Comparison of X-ray,millimeter wave,shearography and through-transmission ultrasonic methods for inspection of honeycomb composites[A].,2007
[27] W. Hillger;R. Meier;R. Henrich .Inspection of CFRP components by ultrasonic imaging with air-coupling[J].Insight: Non-Destructive Testing and Condition Monitoring,2004(3):147-150.
[28] Holland S D;Uhl C;Renshaw J.Vibrothermographic crack heating:A function of vibration and crack size[A].AIP Publishing,2009:489-494.
[29] Damage characterization of a cross-ply carbon fiber/epoxy laminate by an optical measurement of the displacement field[J].Composites science and technology,2010(1):94.
[30] R. Ambu;F. Aymerich;F. Ginesu .Assessment of NDT interferometric techniques for impact damage detection in composite laminates[J].Composites science and technology,2006(2):199-205.
[31] Iijima S .Helical microtubules of graphitic carbon[J].NATURE,1991,354(07):56-58.
[32] Qingwen Li;Xiefei Zhang;Raymond F. DePcuila;Lianxi Zheng;Yonghao Zhao;Liliana Stan;Terry G. Holesinger;Paul N. Arendt;Dean E. Peterson;Yuntian T. Zhu .Sustained Growth of Ultralong Carbon Nanotube Arrays for Fiber Spinning[J].Advanced Materials,2006(23):3160-3163.
[33] Ya-Nan Liu;Min Li;Yizhuo Gu.The interfacial strength and fracture characteristics of ethanol and polymer modified carbon nanotube fibers in their epoxy composites[J].Carbon: An International Journal Sponsored by the American Carbon Society,2013:550-558.
[34] Ya-Nan Liu;Min Li;Yizhuo Gu.A modified spray-winding approach to enhance the tensile performance of array-based carbon nanotube composite films[J].Carbon: An International Journal Sponsored by the American Carbon Society,2013:187-195.
[35] Zhang M;Atkinson KR;Baughman RH .Multifunctional carbon nanotube yarns by downsizing an ancient technology[J].Science,2004(5700):1358-1361.
[36] Jingjing Jia;Jingna Zhao;Geng Xu .A comparison of the mechanical properties of fibers spun from different carbon nanotubes[J].Carbon: An International Journal Sponsored by the American Carbon Society,2011(4):1333-1339.
[37] Zhang M;Fang S;Zakhidov A.A et al.Strong,transpa-rent,multifunctional,carbon nanotube sheets[J].SCIENCE,2005,309(5738):1215-1219.
[38] Qianli Liu;Min Li;Yizhuo Gu .Highly aligned dense carbon nanotube sheets induced by multiple stretching and pressing[J].Nanoscale,2014(8):4338-4344.
[39] Cheng Q F;Bao J W;Park J G et al.High gechanical performance composite conductor:multi-walled carbon nanotube sheet/bismaleimidenanocomposites[J].Advanced Functional Materials,2009,19(20):3219-3225.
[40] Cheng, QF;Wang, B;Zhang, C;Liang, ZY .Functionalized Carbon-Nanotube Sheet/Bismaleimide Nanocomposites: Mechanical and Electrical Performance Beyond Carbon-Fiber Composites[J].Small,2010(6):763-767.
[41] LeGauh M R .Near commercialization:CNT yarn,tape and sheet[EB/OL].http://www.compositesworld.com/articles/near-commercialization-cnt-yarn-tape-and-sheet,2014-07-29.
[42] Park, JG;Louis, J;Cheng, QF;Bao, JW;Smithyman, J;Liang, R;Wang, B;Zhang, C;Brooks, JS;Kramer, L;Fanchasis, P;Dorough, D .Electromagnetic interference shielding properties of carbon nanotube buckypaper composites[J].Nanotechnology,2009(41):415702:1-415702:7.
[43] Li M;Gu Y;Liu Y et al.Interfacial improvement of carbon fiber/epoxy composites using a simple process for depositing commercially functionalized carbon nanotubes on the fibers[J].CARBON,2013,52:109-121.
[44] Limim Gao;Erik T. Thostenson;Zuoguang Zhang;Tsu-Wei Chou .Sensing of Damage Mechanisms in Fiber-Reinforced Composites under Cyclic Loading using Carbon Nanotubes[J].Advanced functional materials,2009(1):A7.
[45] Limin Gao;Tsu-Wei Chou;Erik T. Thostenson .A comparative study of damage sensing in fiber composites using uniformly and non-uniformly dispersed carbon nanotubes[J].Carbon: An International Journal Sponsored by the American Carbon Society,2010(13):3788-3794.
上一张 下一张
上一张 下一张
计量
  • 下载量()
  • 访问量()
文章评分
  • 您的评分:
  • 1
    0%
  • 2
    0%
  • 3
    0%
  • 4
    0%
  • 5
    0%