Strain Range Partitioning and Its Evolution
-
摘要: 应变范围区分法(strain range partitioning,SRP)是由Manson等人于20世纪70年代初发展的一种蠕变疲劳寿命预测方法,经过不断发展和完善,成为少数几种获得实际工程应用的方法之一,并被推广应用于热机械疲劳寿命预测。本文中对SRP法的发展和应用状况进行了梳理综述,重点对基于应变范围区分法发展的总应变-应变范围区分法(total strain version of strain range parti-tioning,TS-SRP)的基本思想和建立过程进行了详细介绍,最后总结给出了TS-SRP法的基本方程、材料参数及其相关关系。Abstract: Strain range partitioning(SRP) is a method developed by Manson and his colleagues during the early 1970s for creep-fatigue life prediction.Through years of research and development,SRP method have become one of the few methods gained engineering application,and is extended to thermomechanical fatigue life prediction.To promote further research and application of SRP and the derivative methods in China,the development and application status of the SRP method was reviewed and summarized in this paper.The basic idea and formulating processes of the total strain version of strain range partitioning(TS-SRP) were introduced and explained in detail.Finally,the basic equations,material parameters and their correlations were summarized.
-
Key words:
- strain range partitioning /
- creep-fatigue /
- thermomechanical /
- fatigue life
-
[1] Halford G R. Evolution of creep-fatigue life prediction models Creep-fatigue Interaction at High Temperature[J].ASMEAD,1991.43-57 [2] Goswami T. Low cycle fatigue life prediction a new model[J].Internationa! Journal of Fatigue,1997,(02):109-115 [3] 涂善东著. 高温结构完整性原理[M].北京:科学出版社,2003 [4] He J,Duan Z,Ning Y,Zhao D. Strain energy partitioning andits application to GH33A nickel-base superalloy and lCrl8Ni9Tistainless steel[A].International Conference on Advances in Life Prediction Methods[C],1983:27~321983.27-32 [5] 何晋瑞主编. 金属高温疲劳[M].北京:科学出版社,1988 [6] Halford G H,Hirschberg M H,Manson S S. Considering MetalsInelastic Deformation at High Temperature Due to PlasticFlow[R].NASA TM-X-68023 [7] Halford G R,Hirschberg M H,Manson S S. TemperatureEffects on the Strainrange Partitioning Approach for Creep-fatigue Analysis[ NASA TM-X-68023] [R] [8] Manson S S. The Challenge to Unity Treatment of High Tem-perature Fatigue-a Partisan Proposal Based on StrainrangePartitioning [R] NASA TMX-68171,1973 [9] Hirschberg M H. Review of the AGARD S and M Panel Eval-uation Program of the NASA-Lewis SRP Approach to High-temperature LCF Life Prediction [R].NASA TM 78879,1978 [10] Hirschberg M H,Halford G R. Use of Strainrange Partitioningto Predict High-temperature Low-cycle Fatigue Life [R].NASA TN D-8072.1976 [11] Manson S S,Halford G R. Treatment of Multiaxial Creep-fatigue by Strain Range Partitioning [R].NASA,19770064196,1976 [12] Blass J J,Zamrik S Y. Multiaxial Low-cycle Fatigue of Type304 Stainless Steel [R].Oak Ridge National Laboratory,ORNL /TM-5609, October,1976 [13] Halford G R. Ductility-normalized Strain Range Parti-tioning Life Relations for Creep-fatigue Life Prediction [R].NASA TM-73737 [14] Halford G R,Nachtigall A J. The strainrange partitioning behav-ior of an advanced gas turbine disk alloy[J].Journal of Air-craft,1980,17(08):598-604 [15] Manson S S. The Strain Range Conversion Principle forTreating Cumulative Fatigue Damage in the Creep Range [R].1983.NASA,19850029499 [16] Halford G R,Saltsman J F. Strain Range Partitioning-A TotalStrain Range Version[R].NASA,1983 [17] Saltsman J F,Halford G H. An Update of the Total Strain Version of SRP[R].NASA,1988 [18] Saltsman J F,Halford G R. Life Prediction of Thermome-chanical Fatigue Using the Total Strain Version of Strain-range Partitioning(SRP)-A Proposal [R].NASA TP-2779,1988 [19] Saltsman J F,Halford G R. Ability of the Total Strain Versionof Strain Range Partitioning to Characterize Thermome-chanical Fatigue Behavior [R].NASA TM-45561994 [20] Arya Vinod K,Halford,Gary R. NASA GRC Fatigue CrackInitiation Life Prediction Models] [R].NASA CP-2002-211682,2002 [21] 胡绪腾,宋迎东. 总应变-应变能区分法[J].机械工程学报,2007,43(02):219-224 [22] 胡绪腾,宋迎东,董凤亮. 应用总应变-应变能区分法预测热机械疲劳寿命[A].第14届发动机结构强度振动学术讨论会论文集[C], 2008: 312 ~ 317 [23] 胡绪腾,宋迎东. 修正的应变范围区分法[J].航空动力学报,2005,20(03):418-423 [24] Saltsman J F,Halford G R. Procedures for Characterizing anAlloy and Predicting Cyclic Life with the Total Strain Ver-sion of Strain Range Partitioiiing [R].NASA TM4102,1989 [25] Vogel W H,Soderquist R W,Schlein B C. Application of creep-LCF cracking model to combustor durability prediction[A].In Fatigue Life Technology[C],ASME,NY,1977:22~31 [26] 涡喷六发动机寿命研究[R].北京:航空工业部发动机管理局,1988 [27] Mcgaw M A,Saltsman J F. A high temperature fatigue life pre-diction computer code based on the Total Strain Version of Strain-range Partitioning (SRP)[ A].Creep-Fatigue Interaction at High Temperature[C],ASME AD,1991,21:65~80 [28] Arya V K,Halford G R. FLAPS(Fatigue Life Analysis Pro-grams),Computer Programs to Predict Cyclic Life Usingthe Total Strain Version of Strain Range Partitioning andOther Life Prediction Methods[M].Users'Manual and Exam-ple Problems,Version 1.0,NASA CR 2003 212-530,2003.
点击查看大图
计量
- 文章访问数: 160
- HTML全文浏览量: 26
- PDF下载量: 5
- 被引次数: 0