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Thermal fatigue of particle reinforced metal-matrix composite induced by laser heating and mechanical load

机译:激光加热和机械载荷引起的颗粒增强金属基复合材料的热疲劳

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摘要

The thermal fatigue of particle reinforced metal-matrix composite induced by repetition-pulsed laser heating and mechanical load was experimentally and numerically studied. It is found that the fatigue damage is initial at the intersection region of laser irradiated brim region and the perpendicular direction of tensile load. The initial damage is induced by void nucleation, growth and subsequent coalescence in the matrix material or interface separation. The fatigue cracks are constituted of void in the matrix, interface separation and particle fracture. The propagation direction of fatigue crack is the perpendicular direction of the tensile load. The fields of temperature, macroscopical stress and microscopical stress and the histories of temperature, macroscopical stress and microscopical stress induced by the repetition pulsed laser and tensile load were simulated by ANSYS-DYNA finite element code. It is found that with the times of laser-irradiated increasing, the maximum temperature within every pulsed laser is increasing. The time of the maximum temperature lagged in the time of the maximum intensity of laser. The maximum stress took place at the intersection region of laser heating brim region and the perpendicular direction of tensile load. Therefore, the damage would be initial at these regions. The results are agreement with the experiment results.
机译:对重复脉冲激光加热和机械载荷引起的颗粒增强金属基复合材料的热疲劳进行了实验和数值研究。发现疲劳损伤始于激光照射边缘区域与拉伸载荷垂直方向的交点区域。初始损伤是由基体材料或界面分离中的空位成核,生长和随后的聚结引起的。疲劳裂纹由基体中的空隙,界面分离和颗粒断裂组成。疲劳裂纹的传播方向是拉伸载荷的垂直方向。利用ANSYS-DYNA有限元代码模拟了重复脉冲激光和拉伸载荷引起的温度,宏观应力和微观应力场,以及重复脉冲激光引起的温度,宏观应力和微观应力的历史。发现随着激光照射时间的增加,每个脉冲激光器内的最高温度都在增加。最高温度的时间滞后于激光最大强度的时间。最大应力发生在激光加热边缘区域与拉伸载荷垂直方向的交点区域。因此,损坏将在这些区域开始。结果与实验结果吻合。

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