IN718镍基高温合金的热机械疲劳性能

被引:17
作者
邓文凯 [1 ,2 ]
徐睛昊 [1 ,2 ]
江亮 [1 ,2 ]
机构
[1] 中南大学粉末冶金国家重点实验室
[2] 中南大学粉末冶金研究院
关键词
IN718镍基高温合金; 热机械疲劳; 同相; 反相; 疲劳寿命; 断口;
D O I
10.19476/j.ysxb.1004.0609.2019.05.11
中图分类号
TG132.3 [特种热性质合金];
学科分类号
080502 ;
摘要
对IN718镍基高温合金进行温度循环为350~650℃及不同应变幅条件下的同相(IP)和反相(OP)热机械疲劳试验;比较同相和反相的热机械疲劳循环应力响应行为、滞后回线以及疲劳寿命;运用金相显微镜、扫描电子显微镜对材料的微观结构以及断口特征进行分析。结果表明:IN718合金的热机械疲劳应力-应变滞后回线最大拉应力与压应力不对称,表明合金在350~650℃范围内高温时抵抗变形阻力较小;合金的循环应力响应行为在低应变幅的同相热机械疲劳的高温半周呈现循环硬化现象,其余情况均为循环软化现象;合金的同相热机械疲劳寿命明显低于反相热机械疲劳寿命,合金热机械疲劳寿命在应变幅超过0.6%的条件下符合Coffin-Manson方程,在应变幅0.4%的情况下实际疲劳寿命值偏高;IN718合金的同相热机械疲劳的疲劳源处断口为沿晶断裂,反相热机械疲劳的为穿晶断裂,裂纹扩展区和瞬断区均为韧窝断裂。
引用
收藏
页码:983 / 989
页数:7
相关论文
共 16 条
[1]  
Influence of crystal orientation on the thermomechanical fatigue behaviour in a single-crystal superalloy.[J].Mikael Segersäll;Daniel Leidermark;Johan J. Moverare.Materials Science & Engineering A.2015,
[2]  
A load history dependent model for fatigue crack propagation in Inconel 718 under hold time conditions.[J].E. Lundström;K. Simonsson;D. Gustafsson;T. Månsson.Engineering Fracture Mechanics.2014,
[3]  
An approach to life prediction for a nickel-base superalloy under isothermal and thermo-mechanical loading conditions.[J].F. V?se;M. Becker;A. Fischersworring-Bunk;H.-P. Hackenberg.International Journal of Fatigue.2013,
[4]   A review of thermo-mechanical fatigue behaviour in polycrystalline nickel superalloys for turbine disc applications [J].
Lancaster, R. J. ;
Whittaker, M. T. ;
Williams, S. J. .
MATERIALS AT HIGH TEMPERATURES, 2013, 30 (01) :2-12
[5]  
Hold-time effect on the thermo-mechanical fatigue crack growth behaviour of Inconel 718.[J].Johan J. Moverare;David Gustafsson.Materials Science & Engineering A.2011, 29
[6]  
Thermo-mechanical fatigue crack propagation experiments in Inconel 718.[J].Lars Jacobsson;Christer Persson;Solveig Melin.International Journal of Fatigue.2009, 8
[7]   Ratcheting behaviour and mean stress considerations in uniaxial low-cycle fatigue of Inconel 718 at 649 °C [J].
Park, S. J. ;
Kim, K. S. ;
Kim, H. S. .
FATIGUE & FRACTURE OF ENGINEERING MATERIALS & STRUCTURES, 2007, 30 (11) :1076-1083
[8]  
Effect of boron and carbon on thermomechanical fatigue of IN 718 superalloy.[J].L. Xiao;D.L. Chen;M.C. Chaturvedi.Materials Science & Engineering A.2006, 2
[9]  
Effect of boron on the low-cycle fatigue behavior and deformation structure of INCONEL 718 at 650 °C.[J].L. Xiao;M. C. Chaturvedi;D. L. Chen.Metallurgical and Materials Transactions A.2004, 11
[10]   LOW-CYCLE FATIGUE BEHAVIOR OF INCONEL 718 AT 298 K AND 823 K [J].
FOURNIER, D ;
PINEAU, A .
METALLURGICAL TRANSACTIONS A-PHYSICAL METALLURGY AND MATERIALS SCIENCE, 1977, 8 (07) :1095-1105