对高周疲劳和低周疲劳寿命预测模型进行了研究,提出了一种能够将高周疲劳和低周疲劳统一表征的能量形式参量.用统一的能量形式表征参量对高温合金GH141的760℃高周疲劳和低周疲劳数据进行处理,得到理想的能量-寿命方程.用1Cr11Ni2W2MoV钢500℃和粉末盘材料FGH95的600℃高温低周疲劳和高周疲劳数据对统一表征方法进行验证,验证结果表明,用能量形式的表征参量能够得到理想的能量-寿命方程.
参考文献
| [1] | MANSON S S .A complex subject-some simple approxim-ations[J].J of Experiment Mechanics,1965,57:193-226. |
| [2] | 谢济洲.低循环疲劳手册[M].北京:北京航空材料研究所,1991:28-32. |
| [3] | COFFIN L F.The effect of frequency on high temperaturelow-cycle fatigue[AFDL-TR-70-144][A].,1970:301-312. |
| [4] | OSTERGREN W J .A damage function and associated failure equation for predicting hold time and frequency effects in elevated temperature low cycle fatigue[J].Journal of Testing and Evaluation,1976,4(05):327-339. |
| [5] | MANSON S S;HALFORD G R;HIRSCHBERG M H.Creepfatigue analysis by strain-range partitioning[A].New York ASME,1971:12-28. |
| [6] | COFFIN L F.The concept of frequency separation in life prediction for time-dependent fatigue[ASME-MPC-3][M].New York,1976:349-363. |
| [7] | HE J;DUAN Z;NING Y.Strain energy partitioning and its application to GH33A nickel-base superalloy and 1Cr18Ni9Ti stainless steel[A].New York ASME,1983:27-32. |
| [8] | MIL-HDBK-195J.MIL-HDBK-195J.航空与航天飞行器结构用金属材料与元件[S]. |
| [9] | 傅惠民.三参数幂函数回归分析[J].航空动力学报,1994(02):186. |
| [10] | 韩希鹏,许超,段作祥,刘绍伦.高周疲劳曲线的等效应力法[J].航空材料学报,2003(03):53-57. |
| [11] | 陈凌,蒋家羚,范志超,陈学东,杨铁成.低周疲劳寿命预测的能量模型探讨[J].金属学报,2006(02):195-200. |
| [12] | MILLER M P;MCDOWELL D L;OCHMKE R L F.A life prediction model for thermom-echanical fatigue based on microcrack propagatio-n[ASTM STP 1186][A].Philadelphia:American Society for Testing and Materials,1993:35-49. |
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