LIN Xin, GAI Pengtao, ZHOU Wenlong, et al. Effect of Shot Peening on Fatigue Properties of High-Strength and High-Toughness β-Titanium Alloy[J]. Aeronautical Manufacturing Technology, 2025, 68(19).
DOI:
LIN Xin, GAI Pengtao, ZHOU Wenlong, et al. Effect of Shot Peening on Fatigue Properties of High-Strength and High-Toughness β-Titanium Alloy[J]. Aeronautical Manufacturing Technology, 2025, 68(19). DOI: 10.16080/j.issn1671-833x.2025.19.128.
Effect of Shot Peening on Fatigue Properties of High-Strength and High-Toughness β-Titanium Alloy
This study investigates the effects of shot peening intensity
shot medium (cast steel shot and ceramic shot)
and composite shot peening on the fatigue properties of high-strength and high-toughness β-titanium alloy. Characterization techniques
including scanning electron microscopy (SEM) and X-ray diffractometry (XRD)
were employed to analyze the influence of shot peening processes on the surface integrity and fatigue fracture behavior of target materials. Experimental results show that shot peening effectively modifies the machined surface profile of target materials. With the increase of shot peening intensity (up to 0.25 mmA)
surface roughness increases
yet no delamination or micro-crack defects are observed
indicating excellent plasticity toughness of the target materials. However
the surface of target materials is sensitive to coverage: Local delamination and wrinkling defects occur on the surface after composite shot peening with 400% coverage. Shot peening introduces a residual compressive stress layer approximately 280 μm in depth on the surface of target materials. The residual stress value generally increases with shot peening intensity
but stress relaxation occurs in the near-surface layer (50 μm thickness) when the intensity reaches 0.22 mmA. Shot peening significantly enhances fatigue performance: Under cast steel shot peening conditions
the fatigue life increases by 145.4 times compared to the as-received state
with individual specimens reaching 1×107 cycles. Ceramic shot peening demonstrates more pronounced fatigue improvement at the same intensity. For peening with a single-shot medium
crack initiation sites shift to the subsurface layer
whereas composite shot peening reduces the average fatigue life significantly
with some crack sources appearing on the surface
attributed to surface damage and residual stress relaxation. In conclusion
high-strength and high-toughness β-titanium alloy exhibits favorable shot peening performance
low sensitivity to shot peening intensity (resistant to delamination or microcrack)
but high sensitivity to shot peening coverage
making it unsuitable for composite or extended shot peening treatments.
Key Laboratory of High Performance Manufacturing for Aero Engine, Ministry of Industry and Information Technology of Northwestern Polytechnical University
Beijing Key Laboratory of Precision and Ultra-Precision Manufacturing Equipment and Control, Tsinghua University