4.7 Article

Thermomechanical fatigue crack growth in a single crystal nickel base superalloy

期刊

INTERNATIONAL JOURNAL OF FATIGUE
卷 122, 期 -, 页码 184-198

出版社

ELSEVIER SCI LTD
DOI: 10.1016/j.ijfatigue.2019.01.014

关键词

Single crystal superalloy; Thermomechanical fatigue; Crack growth; Crack closure

资金

  1. Siemens Industrial Turbomachinery AB in Finspang, Sweden
  2. Swedish Energy Agency, via the Research Consortium of Materials Technology for Thermal Energy Processes [KME-702]

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Thermomechanical fatigue crack growth in a single crystal nickel base superalloy was studied. Tests were performed on single edge notched specimens, using in phase and out of phase thermomechanical fatigue cycling with temperature ranges of 100-750 degrees C and 100-850 degrees C and hold times at maximum temperature ranging from 10 s to 6 h. Isothermal testing at 100 degrees C, 750 degrees C and 850 degrees C was also performed using the same test setup. A compliance-based method is proposed to experimentally evaluate the crack opening stress and thereby estimate the effective stress intensity factor range Delta K-eff for both isothermal and nonisothermal conditions. For in phase thermomechanical fatigue, the crack growth rate is increased if a hold time is applied at the maximum temperature. By using the compliance-based crack opening evaluation, this increase in crack growth rate was explained by an increase in the effective stress intensity factor range which accelerated the cycle dependent crack growth. No significant difference in crack growth rate vs Delta K-eff was observed between in phase thermomechanical fatigue tests and isothermal tests at the maximum temperature. For out of phase thermomechanical fatigue, the crack growth rate was insensitive to the maximum temperature and also to the length of hold time at maximum temperature. The crack growth rate vs Delta K-eff during out of phase thermomechanical fatigue was significantly higher than during isothermal fatigue at the minimum temperature, even though the advancement of the crack presumably occurs at the same temperature. Dissolution of gamma' precipitates and recrystallization at the crack tip during out of phase thermomechanical fatigue is suggested as a likely explanation for this difference in crack growth rate.

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