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应变范围区分法及其发展

胡绪腾 宋迎东

胡绪腾, 宋迎东. 应变范围区分法及其发展[J]. 机械科学与技术, 2012, 31(12): 1967-1973.
引用本文: 胡绪腾, 宋迎东. 应变范围区分法及其发展[J]. 机械科学与技术, 2012, 31(12): 1967-1973.
Hu Xuteng, Song Yingdong. Strain Range Partitioning and Its Evolution[J]. Mechanical Science and Technology for Aerospace Engineering, 2012, 31(12): 1967-1973.
Citation: Hu Xuteng, Song Yingdong. Strain Range Partitioning and Its Evolution[J]. Mechanical Science and Technology for Aerospace Engineering, 2012, 31(12): 1967-1973.

应变范围区分法及其发展

基金项目: 

国防基础科研计划项目资助

详细信息
    作者简介:

    胡绪腾(1980-),博士讲师,研究方向为结构强度、耐久性、损伤容限等,xthu@nuaa.edu.cn

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。
  • [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.
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出版历程
  • 收稿日期:  2011-05-24
  • 刊出日期:  2015-06-10

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