期刊文献+

考虑应力梯度的轮盘疲劳寿命预测 被引量:13

Fatigue life prediction of turbine disk based on stress gradient
原文传递
导出
摘要 考虑应力梯度和尺寸效应对寿命的影响,通过引入应力梯度影响因子,将缺口试件与光滑试件的疲劳寿命相关联,建立了基于Walker平均应力修正的缺口试件寿命预测模型,进而结合三维弹性有限元分析对发动机涡轮盘进行了寿命预测.结果表明:所发展的寿命模型能较好地反映影响疲劳寿命的多种因素,尤其是应力集中对试件疲劳寿命的影响,综合考虑平均应力、应力梯度和尺寸效应的轮盘寿命预测结果更接近试验值,对GH901标准试件和轮盘的疲劳寿命预测结果都在2倍分散带以内. The effects of stress gradient and dimensional size on fatigue life were investigated.The relationship between the notched specimen and the smooth specimen was correlated by introducing the stress gradient effect factor,and a new model of predicting notched specimen based on the Walker modification for the mean stress effect was established.Three-dimensional elastic finite element(FE) analysis of a turbine disk was carried out to obtain the fatigue parameters for predicting its life.The result shows that this model can well reflect several effects on fatigue life,especially the effect of stress concentration on the fatigue life of specimen.If the mean stress,stress gradient and size effect are considered comprehensively,the prediction result of the disk is closer to the experiment result.This model gives a prediction falling within a scatter of two for both GH901 standard specimen and the disk.
出处 《航空动力学报》 EI CAS CSCD 北大核心 2013年第6期1236-1242,共7页 Journal of Aerospace Power
基金 国家自然科学基金(51105023)
关键词 疲劳寿命 缺口疲劳 应力梯度 尺寸效应 轮盘 fatigue life notch fatigue stress gradient size effect disk
  • 相关文献

参考文献15

  • 1Neuber H. Theory of notch stresses: principles for exact calculation of strength with reference to structural form and material[M]. 2nd ed. Berlin : Springer-Verlag, 1958.
  • 2Peterson R E. Metal fatigue= notch-sensitivity[M]//New York : McGraw- Hill, 1959.
  • 3Taylor D. Geometrical effects in fatigue: a unifying theo- retical model[J]. International Journal of Fatigue, 1999,21 (5) :413-420.
  • 4Tanaka K. Engineering formulae for fatigue strength re- duction due to crack-like notches[J]. International Journal of Fatigue, 1983,22(5) :39-46.
  • 5Chiandussi G, Rossetto M. Evaluation of the fatigue strength of notched specimens by the point and line meth- ods with high stress ratios[J]. International Journal of Fa-tigue, 2005,27(6) : 639-650.
  • 6Yamashita Y, Ueda Y, Kuroki H, et al. Fatigue life predic- tion of small notched T:-6A[-4V specimens using critical distance[J]. Engineering Fracture Mechanics, 2010, 77 (9) : 1439-1453.
  • 7曾攀,愈新陆,颜永年,等.疲劳绝对尺寸效应[J].航空学报,1988,9(2):144-147.
  • 8陈勃,刘建中,吴学仁,胡本润,王利发.初始缺陷尺寸分布的尺寸效应研究[J].航空学报,2006,27(1):44-49. 被引量:9
  • 9陆山,张鸿,唐俊星,王春光.考虑尺寸效应的轮盘应力疲劳概率寿命分析方法[J].航空动力学报,2011,26(9):2039-2043. 被引量:10
  • 10Soderherg C R, Sweden V. Factor of safety at:d vmrking stress[J]. ASME Trans,AER-IS,1930,52(2) :13-28.

二级参考文献26

  • 1陈赤囡,苏梅,钱友荣.GH901轮盘变幅低循环疲劳断口反推扩展寿命[J].物理测试,1996,14(4):20-22. 被引量:1
  • 2王卫国,古远兴,卿华,滕光蓉,温卫东.轮盘低循环疲劳寿命预测方法研究及试验验证[J].航空动力学报,2006,21(5):862-866. 被引量:14
  • 3中国航空材料手册:第2卷[M].第2版:北京:中国标准出版社.2002.
  • 4Dowling N E. Mechanical Behavior of Materials: Engineering Methods for Deformation, Fracture and Fatigue[ M]. Prentice-Hall, Second Edition, 1999.
  • 5应力标准(EDG-3)[S].国际航空编辑部,1979,9.
  • 6Peterson R E. Stress concentration factors[ M]. New York: John Wiley & Sons,1974.
  • 7Neuber H. Theory of notch stresses[M]. Virginia : USAEC Office of Technical Information, 1961.
  • 8Kuhn P,Hardran H F. An engineering method for estimating notch size effect in fatigue tests of steel[R~. Report NACA TN 2805,1952.
  • 9Siebel E,Stieler M. Significance of dissimilar stress distributions for cyclic loading [J ]. Zeitschrift des Vereines Deutscher Ingenieure, 1955,97(5) : 121- 131.
  • 10Buch A. Evaluation of size effect in fatigue tests on un- notched specimens and components[J~. Archiv Furdas Eis- enhuttenwesen, 1972,43 (4) :885-900.

共引文献22

同被引文献195

引证文献13

二级引证文献57

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