TY - JOUR
T1 - Research on wear resistance of (tib+la2o3)/imi834 with micro-laser shock peening
AU - Li, Yuhan
AU - Nie, Xiangfan
AU - Wang, Hai
N1 - Publisher Copyright:
© Published under licence by IOP Publishing Ltd.
PY - 2025
Y1 - 2025
N2 - Micro-Laser Shock Peening (Micro-LSP) is an advanced laser surface modification technology. The surface of (TiB+La2O3)/IMI834 samples was treated with micro-laser shock processing. Characterization and analysis of the samples before and after the treatment were conducted using a microhardness tester, scanning electron microscope (SEM), energy-dispersive spectrometer (EDS), and residual stress meter. The results indicated that the (TiB+La2O3)/IMI834 samples underwent substantial alterations in surface topography after Micro-LSP, characterized by an escalation in surface roughness from 0.738 μm to 1.956 μm, a peak residual compressive stress of 431.29 MPa, an augmentation in micro-hardness to 492 HV, and the formation of a hardened layer approximately 570 μm in thickness. Moreover, the wear rate of the samples decreased by 24.16% ∼ 32.12% after Micro-LSP.
AB - Micro-Laser Shock Peening (Micro-LSP) is an advanced laser surface modification technology. The surface of (TiB+La2O3)/IMI834 samples was treated with micro-laser shock processing. Characterization and analysis of the samples before and after the treatment were conducted using a microhardness tester, scanning electron microscope (SEM), energy-dispersive spectrometer (EDS), and residual stress meter. The results indicated that the (TiB+La2O3)/IMI834 samples underwent substantial alterations in surface topography after Micro-LSP, characterized by an escalation in surface roughness from 0.738 μm to 1.956 μm, a peak residual compressive stress of 431.29 MPa, an augmentation in micro-hardness to 492 HV, and the formation of a hardened layer approximately 570 μm in thickness. Moreover, the wear rate of the samples decreased by 24.16% ∼ 32.12% after Micro-LSP.
UR - https://www.scopus.com/pages/publications/105009699855
U2 - 10.1088/1742-6596/3026/1/012056
DO - 10.1088/1742-6596/3026/1/012056
M3 - 会议文章
AN - SCOPUS:105009699855
SN - 1742-6588
VL - 3026
JO - Journal of Physics: Conference Series
JF - Journal of Physics: Conference Series
IS - 1
M1 - 012056
T2 - 2025 International Conference on Aerospace Engineering and Materials Technology, AEMT 2025
Y2 - 28 February 2025 through 2 March 2025
ER -