锻压技术

巨型压机C型机架的疲劳综合系数修正计算

英文标题：Modification calculation on fatigue comprehensive coefficient for C-type frame of huge hydraulic pressure machine

作者：黄宁杨建湘李素云

单位：贺州学院

分类号：O346

出版年,卷(期):页码：2017,42(8):93-96

摘要：

应用名义应力法估算巨型压机C型机架的疲劳寿命时，疲劳综合系数是关键参数。基于疲劳模拟试验原理和相似性准则，建立缩小的相似模型。在此基础上，同时考虑实际零件的应力集中、尺寸和表面加工的相互影响，推导出拉伸作用下的疲劳综合系数修正表达式。利用新表达式分析和计算缺口试样的疲劳寿命，与测试结果基本一致，并通过对两种系数修正结果的对比，进一步说明经新表达式修正后效果更好。运用此计算式可方便地得到C型机架疲劳综合系数，可为其疲劳寿命评估提供参考。

When the fatigue life of C-type frame of huge pressure machine is estimated by nominal stress method, the fatigue comprehensive coefficient is a critical parameter. Based on the principle of fatigue simulation test and principle of similarity, the simulated scaled-model was established. On this basis, simultaneously considering interactions between three factors (stress concentration, size, and surface processing), a fatigue comprehensive coefficient modified expression was presented. A notched-sample fatigue life was analyzed and calculated by new expression, and it was basically accord with the test value. Furthermore, comparing modification results of the two coefficients, the new modified expression is more effective. The fatigue comprehensive coefficient of C-type frame can be conveniently obtained by new modification formula, which provides important basis for its fatigue life assessment.

基金项目：

贺州学院博士基金启动项目（HZUBS201303）；贺州市科技开发项目（贺科能1408013）；广西高校科研项目（KY2015ZD128）

黄宁（1974-），男，博士，讲师

参考文献：

［1］姚卫星. 结构疲劳寿命分析[M]. 北京: 国防工业出版社, 2003.Yao W X. Fatigue Life Prediction of Structures [M].Beijing: National Defense Industry Press, 2003.
［2］奚蔚,姚卫星. 一种考虑尺寸效应的缺口件疲劳寿命预测方法[J].南京航空航天大学学报,2013,45(4): 497-502.Xi W, Yao W X. Method for fatigue life prediction of notched specimen considering size effect [J]. Journal of Nanjing University of Aeronautics & Astronautics,2013,45(4): 497-502.
［3］Bruder T, Strzel K, Baumgartner J, et al. Evaluation of nominal and local stress based approaches for the fatigue assessment of seam welds [J]. International Journal of Fatigue, 2012, 34: 86-102.
［4］张小丽,陈雪峰,李兵，等. 机械重大装备寿命预测综述[J]. 机械工程学报, 2011, 47(11): 100-116.Zhang X L, Chen X F, Li B, et al. Review of life prediction for mechanical major equipment [J]. Chinese Journal of Mechanical Engineering, 2011, 47(11): 100-116.
［5］Zheng J Y，Wu L L, Shi J F. Extreme pressure equipments [J]. Chinese Journal of Mechanical Engineering, 2011, 24(2): 202-206.
［6］黄宁,杨健湘,李素云. 巨型压机C型机架的疲劳寿命预测研究[J]. 锻压技术, 2016,41(5):136-141.Huang N, Yang J X, Li S Y. Study on fatigue life prediction for C-type frame of huge pressure machine[J]. Forging ＆ Stamping Technology, 2016,41(5):136-141.
［7］熊峻江.飞行器结构疲劳与寿命设计[M].北京:北京航天航空大学出版社,2004.Xiong J J. Aircraft Structural Fatigue and Life Design [M]. Beijing: Beijing Aerospace University Press, 2004.
［8］黄宁, 黄明辉, 湛利华. 新的缺口试样尺寸系数经验公式[J]. 华南理工大学学报:自然科学版, 2012, 40(12): 35-40.Huang N, Huang M H, Zhan L H. New empirical formula of size coefficient of notched samples [J]. Journal of South China University of Technology: Natural Science Edition, 2012, 40(12): 35-40.
［9］Lipson C, Juvinall R C. Handbook of Stress and Strength[M]. Neuyork: McMillan Company,1963.
［10］Rosenkranz P, Humer K, Weber H W. Influence of specimen size on the tension-tension fatigue behavior of fibre-reinforced plastics at room temperature and at 77 K[J]. Cryogenics, 2000, 40:155-158.
［11］Fatemi A, Fang D, Zeng Z. Notched fatigue behavior under axial and torsion loads: experiments and predictions [A]. The Eight International Fatigue Congress[C].Stockholm, Sweden, 2002.
［12］丁遂栋.结构钢光试样非对称循环疲劳极限的估算[J].机械强度,1997,19(1):45-47.Ding S D. The estimation of nonsymmetry cycle fatigue limits for structural steel smooth specimens[J]. Journal of Mechanical Strength, 1997,19(1):45-47.

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