首页> 外文会议>Asian Pacific Conference on Fracture and Strength;APCFS; 20061122-25;20061122-25; Sanya(CN);Sanya(CN) >Effect of Mean Stress on Fatigue Strength of Non-combustible Magnesium Alloy
【24h】

Effect of Mean Stress on Fatigue Strength of Non-combustible Magnesium Alloy

机译:平均应力对不燃镁合金疲劳强度的影响

获取原文
获取原文并翻译 | 示例

摘要

Effect of mean stress on fatigue strength at N=10~7 of non-combustible magnesium alloy AMX602B(X=Ca) was investigated. Rotating bending fatigue test and tension-compression fatigue test were carried out on specimens with a small hole or crack. It was clarified that the fatigue strength at N=10~7 of the specimen with the small hole was about 30-150% higher than that of the specimen with the small crack within the range of σ_m=0~100MPa. This is the reason why the fatigue strength at N=10~7 of the specimen with the small hole can be not threshold condition for crack propagation but crack initiation. The fatigue strength at N=107 of the specimens with the small hole decreased within the range of σ_m= 100~195MPa due to a static small crack initiating from the small hole at first loading. The effect of mean stress on fatigue strength at N=10~7 both oh the specimens with the small hole and crack could be estimated using modified Goodman diagram.
机译:研究了平均应力对不燃镁合金AMX602B(X = Ca)在N = 10〜7时疲劳强度的影响。对有小孔或裂纹的试样进行旋转弯曲疲劳试验和拉伸压缩疲劳试验。可以看出,在σ_m= 0〜100MPa范围内,小孔试样在N = 10〜7时的疲劳强度比小裂纹试样在N = 10〜7时高约30-150%。这就是为什么小孔试样在N = 10〜7时的疲劳强度不是裂纹扩展的阈值条件而是裂纹萌生的阈值条件的原因。小孔试样在N = 107时的疲劳强度在σ_m= 100〜195MPa范围内降低,这是由于在第一次加载时从小孔产生的静态小裂纹引起的。在N = 10〜7的情况下,平均应力对具有小孔和裂纹的试样的疲劳强度的影响可以使用修正的Goodman图进行估算。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号