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Fatigue hysteresis behavior in fiber-reinforced ceramic-matrix composites at room and elevated temperatures

机译:纤维增强陶瓷 - 基质复合材料的疲劳滞后行为在室内和升高的温度下

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摘要

The fatigue hysteresis behavior of different fiber-reinforced ceramic-matrix composites (CMCs), i.e., C/SiC, SiC/SiC, SiC/Si-N-C, SiC/Si B4C and Nextel 610 (TM)(TM)/Aluminosilicate, at room and elevated temperatures has been investigated. Based on the developed hysteresis loops models, the relationships between fatigue hysteresis dissipated energy, interface frictional slip and interface shear stress have been established. The evolution of fatigue hysteresis dissipated energy and interface shear stress versus cycle number curves have been analyzed. For C/SiC, the fatigue hysteresis dissipated energy decreases with increasing cycle number at room temperature, and increases with increasing cycle number at 550 degrees C in air; for SiC/SiC and SiC/Si B4C, the fatigue hysteresis dissipated energy increases with increasing cycle number at room temperature, 800 degrees C and 1200 degrees C in air; and for SiC/Si-N-C and Nextel 610 (TM)/Aluminosilicate, the fatigue hysteresis dissipated energy decreases with increasing cycle number at 1000 degrees C in air. The evolution of fatigue hysteresis dissipated energy versus cycle number can be used to monitor the interface debonding and slipping condition inside of composite.
机译:不同纤维增强陶瓷 - 基质复合材料(CMC),即C / SiC,SiC / SiC,SiC / Si-NC,SiC / Si B4C和Nextel 610(TM)/铝硅酸盐的疲劳滞后行为已经调查了房间和高温的温度。基于开发的滞后环模型,已经建立了疲劳滞后能量,界面摩擦滑移和接口剪切应力之间的关系。已经分析了疲劳滞后能量和界面剪切应力与循环数曲线的演变。对于C / SiC,疲劳滞后耗散能量随着室温下的循环数增加而降低,并且在空气中增加了550℃的循环数增加;对于SiC / SiC和SiC / Si B4c,疲劳滞后耗散能量随着室温下的循环数而增加,800℃和1200摄氏度的空气;对于SiC / Si-N-C和NEXTEL 610(TM)/铝硅酸盐,疲劳滞后能量随着1000℃的空气中的增加而增加。疲劳滞后耗散能量与循环数的演变可用于监测复合材料内部的界面剥离和滑动条件。

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