Research Progress on Low Cycle Fatigue of Powder Metallurgy High Temperature Alloys
摘 要
参考了前人对粉末高温合金低周疲劳的研究成果, 回顾了基于缺陷的裂纹萌生和扩展的研究情况, 介绍了针对粉末高温合金的喷丸强化机理和作用, 总结了几种寿命模型, 其中修正Mitchell模型最适合粉末高温合金的寿命预测; 得出了需加强粉末高温合金低周疲劳寿命模型及喷丸强化研究的结论。
Abstract
The research made by predecessors in the low cycle fatigue of powder metallurgy high temperature alloys was refered to, including the crack initiation and propagation based on the defects, the mechanism and effect of peening; several life model were summarized, the modified Mitchell method was the most suitable method for powder metallurgy high temperature alloys, the conclusion was made that the research about the low cycle fatigue life model and shot peening strengthening should be enhanced.
中图分类号 TG132.3+2 TG113.25+5
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基金项目 航空科学基金资助项目(2009ZF21011)
收稿日期 2011/8/21
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备注林涛(1987-), 男, 硕士研究生。
引用该论文: LIN Tao,HE Yu-huai. Research Progress on Low Cycle Fatigue of Powder Metallurgy High Temperature Alloys[J]. Physical Testing and Chemical Analysis part A:Physical Testing, 2011, 47(11): 697~701
林涛,何玉怀. 粉末高温合金的低周疲劳研究进展[J]. 理化检验-物理分册, 2011, 47(11): 697~701
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参考文献
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【24】BARRIE R L, GABB T P, TELESMAN J. Effectiveness of shot peening in suppressing fatigue cracking at non-metallic inclusions in Udimet 720[J]. Materials Science and Engineering,2008,474:71-81.
【2】KRUEGER D D, KISSINGER R D, MENZIES R G. Development and introduction of a damage tolerant high temperature nickle-base disk alloy Rene’88 DT superalloys[C]//Proceedings of the Seventh International Symposium on Superalloys, [S.l.]:[s.n.],1992:277.
【3】RAUJOL S, PETTINARI F, LOCQ D, et al. Creep straining micro-mechanisms in a powder-metallurgical nickel-based superalloy[J].Materials Science and Engineering A, 2004,387-389:678-682.
【4】SOPHILE D G, RAPHAEL C, LAURE G, et al. Modelling the plastic deformation during high-temperature creep of a powder-metallurgy coarse grained superalloy[J]. Materials Science and Engineering A, 2008,483/484 :598-601.
【5】COUTURIER R, ESCARAVAGE C. Process development and mechanical properties of alloy U720LI for high temperature turbine disks[C]//Proceedings of the Tenth International Symposium on Superalloys, [S.l.]:[s.n.],2004:351-359.
【6】FANG Dai-ning, LIU Tie-qi. On the effect of fiber shape and packing array on elastic properties of fiber-polymer-matrix composites [J]. Inter J Polymeric Mater,1996,34(2): 75-90.
【7】谢济洲, 沈祝闽,侯静泳.粉末合金的高温疲劳断裂性能[J]. 航空材料学报, 1997,17(1): 44-48.
【8】SURESH S. 材料的疲劳[M]. 2版.王中光,译. 北京: 国防工业出版社, 1999.
【9】HALFORD G R. Evolution of creep-fatigue life prediction models[J]. In Creep-Fatigue Interaction at High Temperature,ASME AD, 1991,21:43-57.
【10】MANSON S S.Behavior of Materials Under Conditions of Thermal Stress[R].NACA TN-2933,1954.
【11】MANSON S S.Fatigue at Elevated Temperatures[M]// ASTM STP 520,American Society for Testing and Materials, Philadelphia, 1973:744.
【12】MURALIDHARAN U, MANSON S S.Thermal mechanical technical background[J].Journal of Engineering Materials and Technology, 1988,110:55.
【13】MITCHELL M R. Fatigue and Microstructures[M]. OH:American Society for Metals, Metals Pack, 1979:385.
【14】BUMEL J A, SEEGER T. Materials Data for Cyclic Loading[M]. Amsterdam:Elsevier Science Publishers, 1990.
【15】GRISON J. Fatigue crack initiation at inclusions in a powder metallurgy superalloy (in French)[C]// Thesis, Ecole des Mines de Paris. [S.l.]:[s.n.],1994.
【16】LEE K O, BAE K H, LEE S B.Comparison of prediction methods for low-cycle fatigue life of HIP superalloys at elevated temperatures for turbopump reliability[J]. Materials Science and Engineering A,2009,519:112-120.
【17】LAUTRIDOU J C, GU’EDOU J Y, HONNORAT Y, et al.High Temperature Materials for Power Engineering[M].[S.l.]:[s.n.],1990:1163.
【18】BOETTNER R C, LAIRD C, MCEVILY A J. Trans AIME[J].1965(233):379.
【19】MCEVILY A J, BOETTNER R C. Acta Metall, 1963(11):725.
【20】MINAKAWA K, NEWMAN J C, MCEVILY A J. A critical study of the crack closure effect on near-threshold fatigue crack growth [J].Fatigue and Fracture of Engineering Materials and Structure. 1983,6(4):359-365.
【21】DOWLING N E, BEGLEY J A. Fatigue Crack Growth during Gross Plasticity and the J-integral[M]// Mechanics of Crack Growth, ASTM STP 590.[S.l.]:[s.n.],1976:82.
【22】R′EMY A, ALAM A.Growth of small cracks and prediction of lifetime in high-temperature alloys[J].Materials Science and Engineering A, 2007,468-470:40-50.
【23】汝继来,王仁智,李向斌.Rene95粉末合金喷丸强化研究[J].航空材料学报, 1996,16(3): 12-18.
【24】BARRIE R L, GABB T P, TELESMAN J. Effectiveness of shot peening in suppressing fatigue cracking at non-metallic inclusions in Udimet 720[J]. Materials Science and Engineering,2008,474:71-81.
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