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    范金娟, 陶春虎, 张宝才, 赵旭. 树脂基碳纤维复合材料壁板前缘的断裂原因[J]. 机械工程材料, 2008, 32(12): 85-87.
    引用本文: 范金娟, 陶春虎, 张宝才, 赵旭. 树脂基碳纤维复合材料壁板前缘的断裂原因[J]. 机械工程材料, 2008, 32(12): 85-87.
    FAN Jin-juan, TAO Chun-hu, ZHANG Bao-cai, ZHAO Xu. Fracture Analysis of Front Edge of Resin Based Carbon Fiber Composite Wainscot[J]. Materials and Mechanical Engineering, 2008, 32(12): 85-87.
    Citation: FAN Jin-juan, TAO Chun-hu, ZHANG Bao-cai, ZHAO Xu. Fracture Analysis of Front Edge of Resin Based Carbon Fiber Composite Wainscot[J]. Materials and Mechanical Engineering, 2008, 32(12): 85-87.

    树脂基碳纤维复合材料壁板前缘的断裂原因

    Fracture Analysis of Front Edge of Resin Based Carbon Fiber Composite Wainscot

    • 摘要: 某飞机上碳纤维T300增强的树脂基复合材料壁板前缘在使用过程中发生断裂,通过外观检查和断口观察分析了壁板前缘的断裂性质,并阐述了前缘的断裂过程;结合壁板的静力试验、有限元计算与无损检测,分析了断裂产生的原因.结果表明:壁板气流表面与横梁交界处是结构的薄弱部位,受到较大载荷后,主铺层组与弯曲铺层组之间存在的缺陷使得该部位首先开裂,然后发生分层剥离,最后在金属铆接与壁板气流表面交界处发生断裂.指出复合材料结构在设计上应充分考虑工艺是否能满足结构完整性的要求及结构可能受到的突发外载.

       

      Abstract: The front edge of T300 carbon fiber reinforced resin based composite wainscot fractured during service.The fracture mode and fracture course of the front edge of the composite wainscot were analyzed by inspecting the appearance and fracture surface.Static experiments,finite element analysis and nondestructive examination were also carried out and the fracture reason of the composite wainscot was concluded.The results show that the junction of wainscot air flow surface and beam was the weak region,and when received force the defects between main layer group and bend layer group made it cracked first,then delaminated,and finally fractured.It is suggested that whether the process can satisfy the demand of structure integrity and accidental external loads should be paid more attention in design of the structure of the composite materials.

       

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