中长寿命轮盘应力寿命及可靠性分析方法
Methods for stress based life and its reliability analyses of discs with medium-long and long life
-
摘要: 针对轮盘榫槽结构理论应力集中系数难确定、采用传统应力寿命法估寿误差大问题, 提出一种改进应力寿命预估法.改进方法包括:提出应力修正系数概念和一种适用于轮盘榫槽结构的理论应力集中系数确定方法, 以及应力比修正方法.一旦确定了试棒的应力修正系数, 改进应力寿命法可采用光滑棒试验数据预估复杂结构寿命, 并考虑应力集中影响.进而建立了基于改进应力寿命法的应力寿命可靠性分析方法, 并对某风扇盘进行了疲劳寿命可靠性分析, 计算概率寿命与试验寿命吻合良好.Abstract: Considering the difficulty in calculating the stress concentration factor of mortise of a disk and the error of life is big by using the traditional stress-life method,an improved stress-life method is proposed to compute the life of disks.It includes the concept of stress correction coefficient,a new method to determine the stress concentration factor of mortise of a disk and a new method for correcting the stress ratio.When once the stress correction coefficient of the bars was computed,the improved Stress-Life method can be used to calculate disk's life with the experimental data of bars without notch,at the same time,the influence of the stress concentration is also considered.Then a new stress-life probabilistic model is built for the purpose of life reliability analysis.Finally,the fatigue life reliability of a fan disk is analyzed by the method given,and the computational results fit well with experimental ones.
-
[1] 陶晓燕,张玉玲,刘晓光.铁路钢桥整体节点双轴疲劳试验研究[J].中国铁道科学,2005,26(2):77-79.TAO Xiaoyan,ZHANG Yuling,LIU Xiaoguang.Biaxial fatigue test research of solid joint in railway steel bridge[J].China Railway Science,2005,26(2):77-79. [2] 姚卫星.结构疲劳寿命分析[M].北京:国防工业出版社,2003. [3] 赵福星,史海秋,耿中行.一种适用于应力疲劳和应变疲劳的通用寿命模型[J].航空动力学报,2003,18(1):140-145.ZHAO Fuxing,SHI Haiqiu,GENG Zhongxing.General life model adapted to both stress fatigue and strain fatigue[J].Journal of Aerospace Power,2003,18(1):140-145. [4] 蔚夺魁,邵丕仁.某型发动机涡轮盘销钉孔边低循环疲劳寿命分析[J].航空发动机,2000,2:37-41.YU Duokui,SHAO Piren.LCF life at edge of pin-hole analysis of some aeroengine turbine disk[J].Aerongine,2000,2:37-41. [5] Suresh S.材料的疲劳[M].北京:国防工业出版社,1999. [6] 韩希鹏,许超,段作祥,等.高周疲劳曲线的等效应力法[J].航空材料学报,2003,23(3):53-57.HAN Xipeng,XU Chao,DUAN Zuoxiang,et al.Modified equivalent stress model for high cyclic fatigue curves[J].Journal of Aeronauticat Materials,2003,23(3):53-57. [7] 北京航空材料研究所.航空发动机设计用材料数据手册[S].北京:中国航空发动机总公司出版,1990. [8] 陆山.多危险部位轮盘寿命可靠性评估中若干问题探讨[A].第三届航空发动机可靠性学术会议文集[C].湖北宜昌:中国航空学会发动机可靠性专业委员会,2005:208-213. -
点击查看大图
计量
- 文章访问数: 1700
- HTML浏览量: 80
- PDF量: 537
- 被引次数: 0

下载: