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Fatigue Response of Hubrid Magnesium/Carbon-Fiber/PEEK Nanocomposite Laminates at Elevated Temperature (II)

机译:高温升温(II)的弘武镁/碳纤维/ PEEK纳米复合材料层压层的疲劳响应(II)

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High performance Mg based hybrid five-layered composite laminates were fabricated by means of sandwiching the AZ31 Mg foils with the Carbon/PEEK prepregs, in which the nanoparticles SiO2 were uniformly spreaded at the interfaces, through hot press. The basic mechanical properties of quasi-isotropic hybrid laminates were obtained by tensile tests, and they were found in good agreement with the prediction by the rule of mixture. Then, the response due to constant stress amplitude tension-tension (T-T) cyclic loading at elevated temperature up to 10~6 cycles was investigated.The received S-N curves, when normalized by their corresponding ultimate strength, were found very close to each other. That strongly hints the higher resistance to fatigue of quasi-isotropic hybrid laminates at higher temperature is accomplished.
机译:通过将Az31mg箔与碳/ peek prepregs夹在其中,通过热压均匀地在界面均匀地铺设纳米颗粒SiO 2,通过将纳米颗粒SiO 2均匀地展开,通过将AZ31mg箔夹在其中,通过热压覆盖。通过拉伸试验获得准各向同性杂交层压层的基本力学性能,并与混合物规则的预测吻合良好。然后,研究了由于恒定应力幅度张力张力(T-T)升高温度循环负载的响应,高达10〜6个循环。接收的S-N曲线,当通过相应的最终强度标准化时,彼此非常接近。强烈暗示在较高温度下实现对准各向同性杂交层压材料的较高耐疲劳性。

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