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    • 5. 发明专利
    • Carbon fiber and composite material containing the same
    • 碳纤维和含有它的复合材料
    • JP2005133274A
    • 2005-05-26
    • JP2004057723
    • 2004-03-02
    • Mitsubishi Rayon Co Ltd三菱レイヨン株式会社
    • IWAMOTO MASAKOIZUMI JINKO
    • D01F9/22
    • PROBLEM TO BE SOLVED: To provide a carbon fiber having a high strength-exhibiting property as a composite material used for an aircraft and particularly having a high CAI value and also inexpensive by elucidating the relationships of the fine unevenness of the surface of the carbon fiber with oxygen concentration at the surface, and nitrogen concentration with the CAI value, and a composite material consisting of the carbon fiber.
      SOLUTION: This carbon fiber is provided with that it has many wrinkles extending in its longitudinal direction, also 1.0-10.0 nm Ra mean surface coarseness, 20-110 nm diameter (a) of an incircle attaching to the projecting part of the fine unevenness of the surface of the wrinkles, 20-220 nm diameter (b) of a circumcircle attaching to the projecting part and also 0.3≤a/b
    • 要解决的问题:提供具有高强度显示性能的碳纤维作为用于飞机的复合材料,特别是具有高的CAI值,并且通过阐明表面的微细不均匀性的关系也是便宜的 表面具有氧浓度的碳纤维和具有CAI值的氮浓度,以及由碳纤维组成的复合材料。 解决方案:该碳纤维具有在其纵向方向上延伸的许多皱纹,还具有1.0-10.0nm的Ra平均表面粗糙度,附着到凸出部分的附近的直径为20-110nm的直径(a) 皱纹表面的微细凹凸,附着于突出部的外接圆20〜20nm直径(b)以及(a)和(b)之间的0.3≤a/ b <1关系满足5-70nm 满足上述公式的微细凹凸的突出部分的纤维半径方向的高度在突出部分的中心和与前一个突出部分最接近的突出部分之间具有50-100nm的距离,并且表现出0.01≤N/ C ≤0.30表面氮浓度(N / C)。 版权所有(C)2005,JPO&NCIPI
    • 8. 发明专利
    • Carbon fiber and method for producing the same
    • 碳纤维及其制造方法
    • JP2006183173A
    • 2006-07-13
    • JP2004377190
    • 2004-12-27
    • Mitsubishi Rayon Co Ltd三菱レイヨン株式会社
    • IWAMOTO MASAKOIZUMI JINKOKOTANI TOMOYUKI
    • D06M10/00D01F9/22D06M11/58
    • PROBLEM TO BE SOLVED: To provide an inexpensive carbon fiber having high strong expression as a composite material as an aircraft application, especially having a high CAI value according to the SACMA method, and having good reproducibility in CAI strength expression according to the SACMA method by elucidating relation between surface oxygen/nitrogen concentrations and nitrogen peak half value and a nitrogen peak shape, the CAI value according to the SACMA method and its dispersion, and a method for producing the same.
      SOLUTION: The carbon fiber has 0.01-0.3 N
      1S /C
      1S : nitrogen concentration on the surface of the carbon fiber, 2-4eV N
      1S peak half value and 0.04-0.2 O
      1S /C
      1S : oxygen concentration on the surface of the carbon fiber, measured by X ray photoelectron spectroscopy and 1-1.028 specific area of the carbon fiber measured by scanning probe microscope.
      COPYRIGHT: (C)2006,JPO&NCIPI
    • 要解决的问题:为了提供作为飞机应用的复合材料具有高强表现的便宜的碳纤维,特别是根据SACMA方法具有高的CAI值,并且根据所述的CAI强度表达具有良好的再现性 SACMA方法通过阐明表面氧/氮浓度与氮峰值半值和氮峰形状之间的关系,根据SACMA方法的CAI值及其分散性及其制备方法。 解决方案:碳纤维具有0.01-0.3N≤SBS / C 1S :碳纤维表面上的氮浓度,2-4eV N <1S> 峰值半值和0.04-0.2 O 1S / SB / 1S :通过X射线光电子能谱测量碳纤维表面上的氧浓度, 通过扫描探针显微镜测量的1.028比表面积的碳纤维。 版权所有(C)2006,JPO&NCIPI