航空学报 > 2007, Vol. 28 Issue (3): 582-585

疲劳分散系数随应力的变化规律

张福泽   

  1. 北京航空工程技术研究中心
  • 收稿日期:2006-01-17 修回日期:2006-10-12 出版日期:2007-05-10 发布日期:2007-05-10
  • 通讯作者: 张福泽

Law of Fatigue Scatter Factor Versus Test Stress

ZHANG Fu-ze   

  1. Beijing Aeronautical Technology Research Center
  • Received:2006-01-17 Revised:2006-10-12 Online:2007-05-10 Published:2007-05-10
  • Contact: ZHANG Fuze

摘要:

从《航空金属材料疲劳性能手册》中取出267个铝合金试件和139个钢合金试件的疲劳试验数据,研究了疲劳分散系数随疲劳试验应力的变化规律,即在一定应力范围内,疲劳分散系数随着应力的减小而增加。由此变化规律,绘制出它们的变化规律曲线。

关键词: 固体力学, 疲劳分散系数, 试验应力, 变化规律

Abstract:

On the basis of fatigue test data on 267 aluminum alloy test pieces and 139 steel alloy test pieces extracted from Handbook of Fatigue Properties of Aerial Metals, this thesis studies the law of change of the fatigue scatter factor with fatigue test stress, i.e., within a given range of stress, the fatigue scatter factor increases as the stress decreases. A curve of the law of change wise drawn accordingly.

Key words: olid , mechanics,  , fatigue , scatter , factor,  , test , stress,  , law , of , change

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