期刊文献+

形状参数选值对细节疲劳额定强度的影响

Influence of Shape Parameters on Detail Fatigue Rating
下载PDF
导出
摘要 针对细节疲劳额定强度(DFR)的威布尔分布统计理论所涉及的形状参数α选值问题,提出了基于随机数学的DFR-α模型。基于该模型,对比了选用波音许用α值与国产材料实测α值获得的DFR计算误差。结果表明:若直接使用波音α设计许用值,国产铝合金材料DFR计算相对误差在5%以内,国产钛合金DFR计算相对误差在10%以内;σb≤1700 MPa的国产钢,DFR计算相对误差在5%以内。 Aiming at the problem of shape parameter a selection involved in Weibull distribution statistical theory of detail fatigue rating(DFR),a DFR-αmodel based on stochastic mathematics is proposed.Based on the model,the calculation error of DFR is compared between the allowable value of Boeing and the measured value of domestic materials.The results show that the relative error of DFR calculation of domestic aluminum alloy material can be controlled within 5%,and that of domestic titanium alloy can be controlled within 10%.For domestic steel withσb≤1700 MPa,the relative error of DFR calculation can be controlled within 5%.
作者 白士刚 沙宇 BAI Shigang;SHA Yu(College of Architectural Engineering, Guangdong University of Petrochemical Technology, Maoming 525000, China;School of Engineering, Northeast Agricultural University, Harbin 150030, China)
出处 《广东石油化工学院学报》 2021年第3期58-60,共3页 Journal of Guangdong University of Petrochemical Technology
基金 黑龙江省科学基金(LC2018010) 中国博士后科学基金(2017M611342) 广东石油化工学院自然科学研究项目(519191)。
关键词 疲劳 细节疲劳额定强度 威布尔分布 形状参数 随机模拟 fatigue detail fatigue rating Weibull distribution shape parameter stochastic simulation
  • 相关文献

参考文献3

二级参考文献27

  • 1Goranson G. Elements of structural integrity assurance. Fatigue, 1994, 16(1): 43-65.
  • 2Whittaker I C. Besuner P M. A reliability analysis approach to fatigue life of aircraft structures. AD-853263, 1969.
  • 3Whittaker I C. Development of titanium and steel fatigue variability model for application of reliability analysis approach to aircraft structures. AD-758219, 1972.
  • 4郭洪全.关于标准S-N曲线两个参数σm0和s的研究.北京:北京航空材料研究院,1988.
  • 5Schijve J. Fatigue of structures and materials. Berlin and Heidelberg: Springer-Verlag, 2008: 150-153.
  • 6郭洪全.四种国产材料DFR截止值.北京:北京航空材料研究院,1988.
  • 7陈一坚.飞机结构耐久性及损伤容限设计手册.北京:航空航天工业部科学技术研究院,1989:10.
  • 8Goodman J. Mechanics applied to engineering. London: Longmans, Green & Company, 1899:455.
  • 9Gerber W Z. Calculation of the allowable stresses in iron structures. Bayer Archif Engineering, 1874, 6(6): 101-110.
  • 10鞠静敏,航空材料,1988年,1期

共引文献31

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部