Fatigue-crack-propagation thresholds in a nickel-base superalloy at high frequencies and temperatures

被引:16
|
作者
Shyam, A [1 ]
Padula, SA
Marras, SI
Milligan, WW
机构
[1] Michigan Technol Univ, Dept Mat Sci & Engn, Houghton, MI 49931 USA
[2] NASA, Clenn Res Ctr, Cleveland, OH 44135 USA
[3] Michigan Technol Univ, Dept Mech Engn & Engn Mech, Houghton, MI 49931 USA
关键词
D O I
10.1007/s11661-002-0028-2
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
Fatigue-crack-propagation (FCP) tests were conducted on the powder metallurgy nickel-base super-alloy KM4 at temperatures of 20 degreesC, 550 degreesC, and 650 degreesC. Two different heat treatments were investigated, one yielding a relatively coarse grain size of 55 mum and another yielding a fine grain size of 6 mum. Tests were conducted at 100 Hz and 1000 Hz and at load ratios between 0.3 and 0.7. In the Paris regime, trends observed at high frequencies for KM4 were identical to those observed by earlier investigators at lower frequencies: coarse grains. low load ratios, low temperatures, and higher frequencies generally resulted in lower crack-propagation rates. However, in contrast to the Paris-regime behavior, thresholds were a complicated function of microstructure, load ratio, temperature, and frequency, and the only variable that resulted in a consistent trend in threshold was the load ratio. For example, thresholds increased from 100 to 1000 Hz for the fine-grained material at 550 degreesC, but decreased with the same frequency variation at 650 degreesC. One reason for this complexity was a change to intergranular fracture in the fine-grained microstructure at 650 degreesC, which was beneficial for high-frequency thresholds. Higher load ratios and lower frequencies promoted intergranular fracture. However, not all of the complexity could be explained by changing fracture mechanisms. Scanning electron microscope (SEM) stereofractography was utilized to determine quantitative measures of fracture-surface roughness. The most useful quantitative measure was found to be the standard deviation of the fracture-surface height, which is a physically meaningful length parameter and which corresponded to about half the grain size during room-temperature fatigue at near-threshold DeltaK levels. The roughness of the fracture surface was found to increase as the load ratio was increased for both microstructures. For the coarse-grained microstructure, there was a direct correlation between fracture-surface roughness and FCP threshold over the entire range of temperatures, frequencies, and load ratios. However, measurements of closure loads indicated that roughness-induced closure was not the sole reason for the varying FCP thresholds.
引用
收藏
页码:1949 / 1962
页数:14
相关论文
共 50 条
  • [1] Fatigue-crack-propagation thresholds in a nickel-base superalloy at high frequencies and temperatures
    A. Shyam
    W. W. Milligan
    S. A. Padula
    S. I. Marras
    [J]. Metallurgical and Materials Transactions A, 2002, 33 : 1949 - 1962
  • [2] Initiation and growth behavior of a small fatigue crack in nickel-base superalloy at elevated temperatures
    Chen, Q
    Kawagoishi, N
    Nisitani, H
    Goto, M
    Kondo, E
    [J]. SMALL FATIGUE CRACKS: MECHANICS, MECHANISMS, AND APPLICATIONS, 1999, : 223 - 230
  • [3] A TEM INVESTIGATION INTO SOME MICROSTRUCTURAL EFFECTS OF FATIGUE CRACK-PROPAGATION IN A NICKEL-BASE SUPERALLOY
    RICKS, RA
    NEWCOMB, SB
    PORTER, AJ
    [J]. INSTITUTE OF PHYSICS CONFERENCE SERIES, 1983, (68): : 363 - 366
  • [4] A model for slip irreversibility, and its effect on the fatigue crack propagation threshold in a nickel-base superalloy
    Shyam, A
    Milligan, WW
    [J]. ACTA MATERIALIA, 2005, 53 (03) : 835 - 844
  • [6] Crack initiation and propagation induced by inclusions in a nickel-base P/M superalloy under fatigue load
    ZENG Yanping1)
    [J]. Rare Metals, 2005, (03) : 298 - 300
  • [7] Crack initiation and propagation induced by inclusions in a nickel-base P/M superalloy under fatigue load
    Zeng, YP
    Zhang, MC
    Dong, JX
    Zhang, L
    Xie, XS
    [J]. RARE METALS, 2005, 24 (03) : 298 - 300
  • [9] High frequency fatigue crack propagation behavior of a nickel-base turbine disk alloy
    Padula, SA
    Shyam, A
    Ritchie, RO
    Milligan, WW
    [J]. INTERNATIONAL JOURNAL OF FATIGUE, 1999, 21 (07) : 725 - 731
  • [10] Fatigue crack propagation behaviour of a nickel based superalloy at elevated temperatures
    Wang, L.
    Huang, X.
    Guo, G.
    Hu, Y.
    Zhang, L.
    [J]. MATERIALS RESEARCH INNOVATIONS, 2014, 18 : 1087 - 1090