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高纯铝单晶在拉压疲劳早期过程中的行为 被引量:3

BEHAVIOUR OF AI-SINGLE CRYSTAL DURING EARLY STAGE OF PUSH-PULL FATIGUE
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摘要 系统地研究了[110]与[100]两种特殊晶轴取向的高纯铝单晶在1×10(-4)-6×10(-4)室温拉压疲劳应变振幅条件下的应力σm、内耗Q(-1)和加载最大处超声衰减△αt,的循环响应行为,对疲劳不同阶段的位错组态作了详细的TEM观察。结果表明:两种单晶的循环应力均显示出“硬化-软化-二次硬化”的三个阶段特征。内耗的变化和应力进程同步,但趋势相反.超声衰减开始随圈数增大,达到一极大值后减小。这三种参数的变化是由位错与位错的相互作用机制控制。 Push-pull fatigue deformation of [110] and [100] Al-single crystals was performed at room temperature at strain amplitudes in the range (1 to 6) × 10 ̄(-4). Variation of the stress σ, internal friction Q ̄(-1), and ultrasonic attenuation △α vs cycle number N under various strain amplitudes were measured systematically, and the relative dislocation configuration at different stages of fatigue was observed by TEM. The results indicate that the σ-N curve goes through a hardening -softening-secondary hardening sequence during push-pull fatigue in the two kinds of Al-single crystals. The change in the internal friction vs cycle N is synchronous and reverse with that of the stress. The ultrasonic attenuation △α increases with N at the beginning, after reaching a hump, decreases gradually. The variation of this three parameter is controled by the mechanism of interaction between dislocation segments.
出处 《金属学报》 SCIE EI CAS CSCD 北大核心 1996年第5期510-515,共6页 Acta Metallurgica Sinica
关键词 铝单晶 拉压疲劳 超声衰减 位错 Al-single crystal, push-pull fatigue, ultrasonic attenuation, dislocation configuration
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参考文献3

  • 1王中光,材料的疲劳,1993年
  • 2朱震刚,仪器仪表学报,1988年,9卷,396页
  • 3Jin N Y,Acta Metall,1984年,32卷,989页

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