航空学报 > 1994, Vol. 15 Issue (5): 611-615

航空发动机减速器轴系零件的强度可靠性计算方法

尹明德, 欧阳祖行   

  1. 南京航空航天大学机械工程系,南京,210016
  • 收稿日期:1992-08-14 修回日期:1993-03-01 出版日期:1994-05-25 发布日期:1994-05-25

A METHOD FOR THE STRENGTH RELIABILITY CALCULATION OF AXIAL LMACHING PARTS OF AIRLINE ENGINE REDUCER

Yin Mingde, Ouyang Zhuxing   

  1. Department of Mechanical Engineering,Nanjing University of Aeronautics and Astronautics,Nanjing,210016
  • Received:1992-08-14 Revised:1993-03-01 Online:1994-05-25 Published:1994-05-25

摘要: 以古德曼(Goodman)应力线图和第四强度理论为基础,提出了等效高、低周复合循环应力的方法。采用蒙特卡罗(MonteCarlo)法对应力和强度进行了统计模拟,同时拟合了应力和强度的分布规律。运用应力-强度干涉模型,提出了评估轴在单一工作状态和多工作状态下,屈服、破坏和疲劳强度的可靠度计算方法,并编制了计算机程序。计算实例表明,该方法是令人满意的。

关键词: 高频-低频-应力循环, 轴强度-可靠性, 蒙特卡罗法

Abstract: On the basis of the Goodman stress diagram and the fourth strength theory,a method is suggested to get an equivalent stress for high-low frequency compound circulating stress,The stress and strength are simulated statisitcally with the Monte-Carlo method,and their distributions are fitted.The model of stress-strength interference is applied to the strength reliability calcula-tion,A method is put forward to calculate the yield,fracture and fatigue reliability of axial rnachine parts under single-working and multiworking conditions. and the calculation program is compiled.The calcuktion results indicate that the method is satisfactory.

Key words: high frequencies-low frequencies-cycles stress, shafts (maehina elements) strength-re-liability, Monte-Carlo method

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