Hashim Mohd Khairul Rabani, Majid Mohd Shukry Abdul, Jamir Mohd Ridzuan Mohd, Kasim Farizul Hafiz, Sultan Mohamed Thariq Hameed, Shah Ain Umaira Md, Ahmad Kamarul Arifin, Basri Adi Azriff
Faculty of Mechanical Engineering Technology, Universiti Malaysia Perlis (UniMAP), Kangar 02100, Malaysia.
Faculty of Chemical Engineering Technology, Universiti Malaysia Perlis (UniMAP), Kangar 02100, Malaysia.
Polymers (Basel). 2021 Nov 15;13(22):3936. doi: 10.3390/polym13223936.
This study examined the fatigue behaviour of pineapple leaf fibre/carbon hybrid laminate composites under various stacking sequences. The vacuum infusion technique was used to fabricate the symmetric quasi-isotropic oriented laminates, in which the stacking was varied. The laminate was tested under static and fatigue tensile load according to ASTM D3039-76 and ASTM D3479-96, respectively. Maximum tensile strength and modulus of 119.34 MPa and 6.86 GPa, respectively, were recorded for the laminate with external PALF ply and internal carbon ply oriented at [± 45°, 0°/90°] (PCCP_45090). The fatigue tests showed that PCCP_45090 and CPPC_09045 (with internal PALF ply and external carbon ply oriented at [0°/90° ± 45°]) exhibited a higher useful life, especially at the high-stress level of the ultimate tensile strength. The normalised stress against the number of cycles showed that the stacking sequences of different ply orientations affected the fatigue behaviour more than the stacking sequences of the material. The laminate stacking sequence significantly affected the hysteresis energy and stiffness evolution. The scanning electron microscopy images showed that the fatigue failure modes included fibre pull-out, fibre breakage, matrix cracking, debonding, and delamination. The study concluded that PCCP_45090 exhibited an outstanding fatigue performance.
本研究考察了菠萝叶纤维/碳混杂层合复合材料在不同铺层顺序下的疲劳行为。采用真空灌注技术制备对称准各向同性取向层合板,其中铺层方式有所变化。根据ASTM D3039 - 76和ASTM D3479 - 96标准,分别对层合板进行静态和疲劳拉伸载荷测试。对于外部为菠萝叶纤维层、内部为碳层且取向为[±45°, 0°/90°]的层合板(PCCP_45090),记录到的最大拉伸强度和模量分别为119.34 MPa和6.86 GPa。疲劳试验表明,PCCP_45090和CPPC_09045(内部为菠萝叶纤维层、外部为碳层且取向为[0°/90° ± 45°])具有更长的使用寿命,尤其是在极限拉伸强度的高应力水平下。归一化应力与循环次数的关系表明,不同铺层取向的铺层顺序对疲劳行为的影响大于材料的铺层顺序。层合板铺层顺序显著影响滞后能量和刚度演变。扫描电子显微镜图像显示,疲劳失效模式包括纤维拔出、纤维断裂、基体开裂、脱粘和分层。研究得出结论,PCCP_45090表现出优异的疲劳性能。