Creep, fatigue and oxidation in crack growth in advanced nickel base superalloys

被引:104
|
作者
Tong, J
Dalby, S
Byrne, J
Henderson, MB
Hardy, MC
机构
[1] Univ Portsmouth, Dept Mech & Mfg Engn, Portsmouth PO1 3DJ, Hants, England
[2] Def Evaluat & Res Agcy, Struct Mat Ctr, Farnborough GU14 0LX, Hants, England
[3] Rolls Royce PLC, Disc & Lifing Grp, Derby DE24 8BJ, England
基金
英国工程与自然科学研究理事会;
关键词
creep; fatigue crack growth; load-line deflection; nickel base superalloys; oxidation; waveform;
D O I
10.1016/S0142-1123(01)00049-4
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
This paper presents some of our recent results from an on, going collaborative research programme on creep-fatigue behaviour of two advanced nickel base superalloys for turbine disc applications. The role of creep, fatigue and oxidation in crack growth has been investigated at 650 degreesC under typical loading waveforms at selected loading frequencies. Load-line deflections were monitored in selected tests under static and long dwell loading conditions. Scanning electron microscopy was adopted to identify the fracture mode and to facilitate the evaluation of oxidation. The results show that mixed time and cycle dependent crack growth seems to be the predominant crack growth mode in the two PM nickel alloys studied. Whilst limited creep may be present at the crack tip, particularly under static and long dwell loading conditions, oxidation appears to be the predominant mechanism for crack growth under the test conditions examined. (C) 2001 Elsevier Science Ltd. All roghts reserved.
引用
收藏
页码:897 / 902
页数:6
相关论文
共 50 条
  • [41] Deterministic and probabilistic creep-fatigue-oxidation crack growth modeling
    Wei, Zhigang
    Yang, Fulun
    Lin, Burt
    Luo, Limin
    Konson, Dmitri
    Nikbin, Kamran
    PROBABILISTIC ENGINEERING MECHANICS, 2013, 33 : 126 - 134
  • [42] Fatigue crack growth characteristics for powder nickel based metallurgical superalloys at elevated temperatures
    Yoon, D. H.
    Kim, J. H.
    Kim, H. K.
    Kim, D. H.
    MATERIALWISSENSCHAFT UND WERKSTOFFTECHNIK, 2018, 49 (05) : 522 - 529
  • [43] Vacuum Levels Needed to Simulate Internal Fatigue Crack Growth in Titanium Alloys and Nickel-Base Superalloys: Thermodynamic Considerations
    V. Sinha
    J. M. Larsen
    Metallurgical and Materials Transactions A, 2012, 43 : 3433 - 3441
  • [44] Vacuum Levels Needed to Simulate Internal Fatigue Crack Growth in Titanium Alloys and Nickel-Base Superalloys: Thermodynamic Considerations
    Sinha, V.
    Larsen, J. M.
    METALLURGICAL AND MATERIALS TRANSACTIONS A-PHYSICAL METALLURGY AND MATERIALS SCIENCE, 2012, 43A (10): : 3433 - 3441
  • [45] Fatigue crack growth resistant microstructures in polycrystalline Ni-base superalloys for aeroengines
    Boyd-Lee, AD
    INTERNATIONAL JOURNAL OF FATIGUE, 1999, 21 (04) : 393 - 405
  • [46] Elevated Temperature Fatigue Crack Growth rate model for NI-BASE Superalloys
    Evans, J. L.
    Saxena, A.
    INTERNATIONAL JOURNAL OF FRACTURE, 2014, 185 (1-2) : 209 - 216
  • [47] Elevated Temperature Fatigue Crack Growth rate model for NI-BASE Superalloys
    J. L. Evans
    A. Saxena
    International Journal of Fracture, 2014, 185 : 209 - 216
  • [48] Fatigue crack growth mechanisms in superalloys: overview
    Reed, P. A. S.
    MATERIALS SCIENCE AND TECHNOLOGY, 2009, 25 (02) : 258 - 270
  • [49] EFFECTS OF MICROSTRUCTURE ON LONG AND SHORT CRACK-GROWTH IN NICKEL-BASE SUPERALLOYS
    BROWN, CW
    KING, JE
    HICKS, MA
    METAL SCIENCE, 1984, 18 (07): : 374 - 380
  • [50] Effect of environment on the creep crack growth behaviour of superalloys
    Xu, S
    Dickson, JI
    Koul, AK
    Wu, XJ
    ENVIRONMENTALLY INDUCED CRACKING OF METALS, PROCEEDINGS, 2000, : 45 - 57