Journal of Aeronautical Materials (Aug 2024)

Effect of welding defects on fatigue behavior of Ni-base superalloy GH4065A

  • LI Linhan,
  • ZHANG Ji,
  • TIAN Chenggang,
  • YANG Shanjie,
  • SHEN Zhongmin,
  • ZHANG Wenyun,
  • ZHANG Beijiang

DOI
https://doi.org/10.11868/j.issn.1005-5053.2024.000038
Journal volume & issue
Vol. 44, no. 4
pp. 85 – 95

Abstract

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The spot-welding defects of highly alloyed Ni-base superalloy GH4065A were investigated by using SEM and EBSD analysis methods. Effects of the welding defects on fatigue life and fracture behavior were studied by comparing thin plate samples with a central hole that were non-welded,densely welded and sparsely welded respectively. The results show that the lack-of-fusion defect,solidification crack and liquation crack are the main welding defects responsible for significant reductions in low-cycle fatigue life as well as combined low and high cycle fatigue life. These welding defects result in a transition of the fatigue crack initiation site from the inner surface of the central hole in the non-welded sample to the welding spot in the welded sample,leading to 44%-83% reductions in low-cycle fatigue life at 700 ℃/700 MPa. For the combined low and high cycle fatigue conditions(with a stress amplitude of 700 MPa for the low cycle loading part and 100 MPa for the high cycle loading part),the welding defects not only alter the site at which fatigue cracks initiate,but also make the crack propagation mode more intergranular. This results in dramatic decreases of over 85% in the fatigue life of welded samples at both 600 ℃ and 700 ℃. Due to shorter distance between the welding spot and the central hole,densely-welded samples exhibit a slightly lower level of fatigue life under low-cycle loading conditions compared to sparsely welded samples. However,the fatigue life difference between them becomes negligible when subjected to combined low and high cycle loadings.

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