碳纤维增强树脂基复合材料

  • 网络cfrp;carbon fiber reinforced polymer
碳纤维增强树脂基复合材料碳纤维增强树脂基复合材料
  1. 对单向及正交碳纤维增强树脂基复合材料(CFRP)在静态拉伸及动态拉-拉载荷作用下的电阻-应变特性进行了研究。

    The characteristics of electric resistance-strain relationship of unidirectional and cross-ply CFRP laminates were studied under static and tensile-tensile dynamic loading .

  2. 碳纤维增强树脂基复合材料的电阻-应变特性

    Characteristics of Electric Resistance-strain Relationship of CFRP Laminates

  3. 作为重要的先进航空航天结构材料,碳纤维增强树脂基复合材料(CFRP)的性能取决于增强碳纤维与树脂基体的性能以及两者之间的界面结合状况。

    As an important advanced structural materials in the area of aerospace , the properties of carbon fiber reinforced polymer ( CFRP ) highly depend on the properties of the carbon fiber ( CF ) and the resin matrix , and the properties of interface .

  4. 用电化学方法研究碳纤维增强树脂基复合材料的腐蚀失效行为

    Study on corrosive failure behavior of carbon fiber / Epoxy Composites by electrochemical methods

  5. 一个单向碳纤维增强树脂基复合材料导电结构模型

    Model of conductive structure of unidirectional CFRP

  6. 影响碳纤维增强树脂基复合材料腐蚀重要环境因素的研究

    Study of important environmental factors on the corrosion failure of the carbon / epoxy composite

  7. 电阻电容的场量方程及其关系碳纤维增强树脂基复合材料的电阻-应变特性

    The Field Equation of Electric Resistance and Capacitance Characteristics of Electric Resistance - strain Relationship of CFRP Laminates

  8. 为了实现飞行器最小净起飞重量的要求,复合材料在航空航天领域应用越来越广泛,特别是碳纤维增强树脂基复合材料。

    To achieve the requirements of the aircraft minimum take-off weight , composite materials are used in the aerospace field more and more widely , especially carbon fiber reinforced resin matrix composites .

  9. 随着碳纤维增强树脂基复合材料、高聚物复合材料大量应用到航空航天领域,这些材料的粘弹性特征和渐进损伤破坏形式受到人们越来越多的关注。

    With the fibre reinforced composite materials and high polymer composite materials are used in various fields more and more widely , these materials ' viscoelastic character and their progress damage obtain more focus .

  10. 本文报导了一个单向碳纤维增强树脂基复合材料导电结构模型,可用单位截面上邻近碳纤维的搭接点数目和两相邻搭接点的距离来表征这种导电结构的基本特征。

    A Model of conductive structure of unidirectional carbon fiber reinforced polymers ( CFRP ) is studied . The conductive structure of CFRP can be characterized by the contact number of neighbouring carbon fibers per unit section and the distance of two neighbouring contact points .

  11. 本文研究了温度与外加应力因素对碳纤维增强环氧树脂基复合材料在NaCl水溶液中吸湿行为的影响规律。

    The effect of temperature and external stress on the moisture absorption behavior of graphite epoxy composite material in NaCl solution is studied in this paper .

  12. 利用INSTRON实验机和落锤装置对圆筒形碳纤维增强环氧树脂基复合材料结构进行了静、动态压缩实验。

    Cylinder structure of carbon fiber reinforced epoxy resin matrix composite material is compressed by INSTRON and drop weight experimental equipment .

  13. 碳纤维增强的树脂基复合材料在250、288和320℃具有良好的热氧化稳定性,在320℃,经过500h后热氧化失重≤3%;

    The continuous carbon fiber reinforced composites exhibit high thermo-oxidation stability at 250,288 and 320 ℃, and the weight loss is lower than 3 % after 500 hours thermal oxidation at 320 ℃ .

  14. 碳纤维增强环氧树脂基复合材料的性能研究

    Study on performance of composite material based on epoxy resin reinforced by carbon fiber

  15. 结论碳纤维增强型树脂基复合材料对动物无全身毒性作用也无溶血作用。

    Conclusion Carbon-fibre reinforced resin compound had no acute systemic toxic action on animals and haemolysis effect in vitro .

  16. 碳纳米管与连续碳纤维增强树脂基复合材料的制备及其力学性能研究

    Fabrication of Carbon Nanotube and Continuous Carbon Fiber Reinforced Epoxy Resin Matrix Composites and Its Mechanical Property

  17. 短碳纤维是一种重要的复合材料增强体,短碳纤维增强环氧树脂基复合材料由于成本低廉以及良好的加工成型性,在国民工业各领域得到广泛的应用。

    Short carbon fiber ( SCF ) is an important reinforcement . Due to the low cost and good formability , short carbon fiber reinforced epoxy composites are widely used in various fields .