镍基单晶/柱晶高温合金超高周疲劳研究进展

doi:10.7527/S1000-6893.2020.24340

Abstract

Abstract: As the current main material for advanced aero-engine turbine blades, nickel-based single crystal/directionally solidified superalloys have high high-temperature strength, strong oxidation resistance and excellent fatigue resistance. Very-high cycle fatigue (fatigue life>10⁸) is the major problem faced by turbine blades in the middle and late stages of service. This article reviews the very-high cycle fatigue of nickel-based single crystal/directionally solidified superalloys. The analysis results show that single crystal/directionally solidified superalloys have abnormal yielding phenomena at high temperature; comparing fatigue studies at different frequencies finds no obvious frequency effect; analyses of fatigue mechanism find that cracks mainly originate from casting defects such as pores. Finally, the fatigue life prediction model is summarized, and the trends of very high cycle fatigue of nickel-based single-crystal and directionally solidified superalloys are prospected.

Key words: nickel-based single crystal and directionally solidified superalloys, high cycle fatigue, fatigue mechanism, fatigue properties, life prediction

CLC Number:

V252.2

LI Qian, ZHANG Fulu, ZHAO Zihua. Very high cycle fatigue of nickel-based single-crystal and directionally solidified superalloys: Review[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(5): 524340-524340.

References 42

[1]	WU R H, YUE Z F, WANG M. Effect of initial γ/γ' microstructure on creep of single crystal nickel-based superalloys:A phase-field simulation incorporating dislocation dynamics[J]. Journal of Alloys and Compounds, 2019, 779:326-334.
[2]	MENOU E, RAME J, DESGRANGES C, et al. Computational design of a single crystal nickel-based superalloy with improved specific creep endurance at high temperature[J]. Computational Materials Science, 2019, 170:109194.
[3]	LI Y F, WANG L, ZHANG G, et al. Creep anisotropy of a 3rd generation nickel-base single crystal superalloy at 850℃[J]. Materials Science and Engineering:A, 2019, 760:26-36.
[4]	QI D Q, WANG D, DU K, et al. Creep deformation of a nickel-based single crystal superalloy under high stress at 1033 K[J]. Journal of Alloys and Compounds, 2018, 735:813-820.
[5]	HU Y B, ZHANG L, CAO T S, et al. The effect of thickness on the creep properties of a single-crystal nickel-based superalloy[J]. Materials Science and Engineering:A, 2018, 728:124-132.
[6]	岳全召, 刘林, 杨文超, 等. 先进镍基单晶高温合金蠕变行为的研究进展[J]. 材料导报, 2019, 33(3):479-489. YUE Q Z, LIU L, YANG W C, et al. Research progress of creep behaviors in advanced Ni-based single crystal superalloys[J]. Materials Reports, 2019, 33(3):479-489(in Chinese).
[7]	曹刚, 张旭辉, 徐涛, 等. 镍基单晶合金高温低周疲劳微观损伤及断裂机制[J]. 热加工工艺, 2017, 46(22):48-51. CAO G, ZHANG X H, XU T, et al. Microscopic damage and fracture mechanism of nickel-based single crystal superalloy during low cycle fatigue at elevated temperature[J]. Hot Working Technology, 2017, 46(22):48-51(in Chinese).
[8]	ZHANG L, ZHAO L, ROY A, et al. Low-cycle fatigue of single crystal nickel-based superalloy-Mechanical testing and TEM characterisation[J]. Materials Science and Engineering:A, 2019, 744:538-547.
[9]	LIU L, MENG J, LIU J L, et al. Effects of crystal orientations on the cyclic deformation behavior in the low cycle fatigue of a single crystal nickel-base superalloy[J]. Materials & Design, 2017, 131:441-449.
[10]	LI S, PING L. Low-cycle fatigue behavior of a nickel base single crystal superalloy at high temperature[J]. Rare Metal Materials and Engineering, 2015, 44(2):288-292.
[11]	MORRISSEY R J, GOLDEN P J. Fatigue strength of a single crystal in the gigacycle regime[J]. International Journal of Fatigue, 2007, 29(9-11):2079-2084.
[12]	NIE B H, ZHAO Z H, LIU S, et al. Very high cycle fatigue behavior of a directionally solidified Ni-base superalloy DZ4[J]. Materials, 2018, 11(1):98.
[13]	ZHAO Z H, ZHANG F L, DONG C, et al. Initiation and early-stage growth of internal fatigue cracking under very-high-cycle fatigue regime at high temperature[J]. Metallurgical and Materials Transactions A, 2020, 51(4):1575-1592.
[14]	CERVELLON A, CORMIER J, MAUGET F, et al. Very high cycle fatigue of Ni-based single-crystal superalloys at high temperature[J]. Metallurgical and Materials Transactions A, 2018, 49(9):3938-3950.
[15]	CERVELLON A, CORMIER J, MAUGET F, et al. VHCF life evolution after microstructure degradation of a Ni-based single crystal superalloy[J]. International Journal of Fatigue, 2017, 104:251-262.
[16]	YI J Z, TORBET C J, FENG Q, et al. Ultrasonic fatigue of a single crystal Ni-base superalloy at 1000℃[J]. Materials Science and Engineering:A, 2007, 443(1-2):142-149.
[17]	骆宇时, 郭会明, 赵云松, 等. 热等静压对第二代DD6单晶高温合金高温高周疲劳性能的影响[J]. 机械工程材料, 2016, 40(7):51-55, 118. LUO Y S, GUO H M, ZHAO Y S, et al. Effect of hot isostatic pressing on high-temperature high cycle fatigue properties of a second generation single crystal superalloy DD6[J]. Materials for Mechanical Engineering, 2016, 40(7):51-55, 118(in Chinese).
[18]	Department of Defense Handbook. Engine structural integrity programs (ENSIP):MIL-HDBH-1783B[S]. Washington, D.C.:Department of Defense, 2002.
[19]	张琴, 许巍, 范金娟, 等. 材料及构件振动疲劳研究进展[J]. 材料开发与应用, 2020, 35(1):14-22, 31. ZHANG Q, XU W, FAN J J, et al. Research progress of vibration fatigue of materials and components[J]. Development and Application of Materials, 2020, 35(1):14-22, 31(in Chinese).
[20]	洪友士, 孙成奇, 刘小龙. 合金材料超高周疲劳的机理与模型综述[J]. 力学进展, 2018, 48(1):1-65. HONG Y S, SUN C Q, LIU X L. A review on mechanisms and models for very-high-cycle fatigue of metallic materials[J]. Advances in Mechanics, 2018, 48(1):1-65(in Chinese).
[21]	HONG Y S, SUN C Q. The nature and the mechanism of crack initiation and early growth for very-high-cycle fatigue of metallic materials-An overview[J]. Theoretical and Applied Fracture Mechanics, 2017, 92:331-350.
[22]	许罗鹏, ZHOU Min, 王清远. DZ125合金超高周疲劳微观裂纹萌生机制[J]. 工程科学与技术, 2018, 50(6):245-250. XU L P, ZHOU M, WANG Q Y. Micro-crack initiation mechanism of DZ125 Ni-based alloy during very high cycle fatigue[J]. Advanced Engineering Sciences, 2018, 50(6):245-250(in Chinese).
[23]	CHU Z K, YU J J, SUN X F, et al. High cycle fatigue behavior of a directionally solidified Ni-base superalloy DZ951[J]. Materials Science and Engineering:A, 2008, 496(1-2):355-361.
[24]	LIU Y, YU J J, XU Y, et al. High cycle fatigue behavior of a single crystal superalloy at elevated temperatures[J]. Materials Science and Engineering:A, 2007, 454-455:357-366.
[25]	REED R C. The superalloys[M]. Cambridge:Cambridge University Press, 2006.
[26]	BATHIAS C, PARIS P C. Gigacycle fatigue in mechanical practice[M]. New York:CRC Press, 2004.
[27]	WRIGHT P K, JAIN M, CAMERON D. High cycle fatigue in a single crystal superalloy:Time dependence at elevated temperature[C]//Superalloys 2004(Tenth International Symposium). Warrendale:TMS, 2004:657-666.
[28]	CHEN Q, KAWAGOISHI N, WANG Q Y, et al. Small crack behavior and fracture of nickel-based superalloy under ultrasonic fatigue[J]. International Journal of Fatigue, 2005, 27(10-12):1227-1232.
[29]	FURUYA Y, KOBAYASHI K, HAYAKAWA M, et al. High-temperature ultrasonic fatigue testing of single-crystal superalloys[J]. Materials Letters, 2012, 69:1-3.
[30]	胡远培, 洪友士. 加载频率对高强钢超高周疲劳行为的影响[C]//第三届中国超高周疲劳学术会议论文集. 成都:中国科学院力学研究所, 2016:34. HU Y P, HONG Y S. Effect of loading frequency on very high cycle fatigue behavior of high strength steel[C]//Proceedings of the 3rd China Very High Cycle Fatigue Academic Conference. Chengdu:Institute of Mechanics, Chinese Academy of Sciences, 2016:34(in Chinese).
[31]	SCHNEIDER N, BÖDECKER J, BERGER C, et al. Frequency effect and influence of testing technique on the fatigue behaviour of quenched and tempered steel and aluminium alloy[J]. International Journal of Fatigue, 2016, 93:224-231.
[32]	GUENNEC B, UENO A, SAKAI T, et al. Effect of the loading frequency on fatigue properties of JIS S15C low carbon steel and some discussions based on micro-plasticity behavior[J]. International Journal of Fatigue, 2014, 66:29-38.
[33]	BORTOLUCI ORMASTRONI L M, MATAVELI SUAVE L, CERVELLON A, et al. LCF, HCF and VHCF life sensitivity to solution heat treatment of a third-generation Ni-based single crystal superalloy[J]. International Journal of Fatigue, 2020, 130:105247.
[34]	RANC N, WAGNER D, PARIS P C. Study of thermal effects associated with crack propagation during very high cycle fatigue tests[J]. Acta Materialia, 2008, 56(15):4012-4021.
[35]	CERVELLON A, HEMERY S, KURNSTEINER P, et al. Crack initiation mechanisms during very high cycle fatigue of Ni-based single crystal superalloys at high temperature[J]. Acta Materialia, 2020, 188:131-144.
[36]	CHAI G C. Analysis of microdamage in a nickel-base alloy during very high cycle fatigue[J]. Fatigue & Fracture of Engineering Materials & Structures, 2016, 39(6):712-721.
[37]	CHAI G C, ZHOU N, CIUREA S, et al. Local plasticity exhaustion in a very high cycle fatigue regime[J]. Scripta Materialia, 2012, 66(10):769-772.
[38]	燕怒, 韩晓琪, 余泳华, 等. GH4169镍基高温合金的超高周疲劳性能[J]. 机械工程材料, 2016, 40(4):9-12. YAN N, HAN X Q, YU Y H, et al. Very high cycle fatigue properties of GH4169 Ni-based superalloy[J]. Materials for Mechanical Engineering, 2016, 40(4):9-12(in Chinese).
[39]	STINVILLE J C, LENTHE W C, MIAO J, et al. A combined grain scale elastic-plastic criterion for identification of fatigue crack initiation sites in a twin containing polycrystalline nickel-base superalloy[J]. Acta Materialia, 2016, 103:461-473.
[40]	CASTELLUCCIO G M, MUSINSKI W D, MCDOWELL D L. Computational micromechanics of fatigue of microstructures in the HCF-VHCF regimes[J]. International Journal of Fatigue, 2016, 93:387-396.
[41]	FATEMI A, SOCIE D F. A critical plane approach to multiaxial fatigue damage including out-of-phase loading[J]. Fatigue & Fracture of Engineering Materials and Structures, 1988, 11(3):149-165.
[42]	STEUER S, VILLECHAISE P, POLLOCK T M, et al. Benefits of high gradient solidification for creep and low cycle fatigue of AM1 single crystal superalloy[J]. Materials Science and Engineering:A, 2015, 645:109-115.

Very high cycle fatigue of nickel-based single-crystal and directionally solidified superalloys: Review

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