1. 大连理工大学,大连,116024
2. 中国航空制造技术研究院,北京,100024
纸质出版:2025
移动端阅览
林鑫, 盖鹏涛, 周文龙, 等. 喷丸处理对高强韧β钛合金疲劳性能影响[J]. 航空制造技术, 2025,68(19).
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).
林鑫, 盖鹏涛, 周文龙, 等. 喷丸处理对高强韧β钛合金疲劳性能影响[J]. 航空制造技术, 2025,68(19). DOI: 10.16080/j.issn1671-833x.2025.19.128.
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.
本文以高强韧β钛合金为研究对象,研究了喷丸强度、弹丸介质(铸钢丸和陶瓷丸)及复合喷丸对靶材疲劳性能的影响。采用扫描电镜、X射线衍射仪等设备表征,分析了喷丸工艺对试样表面完整性及疲劳断裂的影响。试验表明,喷丸处理能有效改变靶材表面机加工轮廓,随着喷丸强度增加(最大至0.25 mmA),表面粗糙度升高,但没有出现脱层或微裂纹缺陷,表明靶材塑韧性好。然而,靶材表面对覆盖率较为敏感,复合喷丸处理(覆盖率400%)表面局部出现脱层和褶皱缺陷。喷丸在靶材表面引入深约280 μm的残余压应力层,随喷丸强度增加,残余应力值整体增加,但喷丸强度达到0.22 mmA 时,近表层(50 μm 厚)出现应力松弛。喷丸强化后疲劳性能提升显著,在铸钢丸条件下疲劳寿命较原始态可提高145.4倍,个别试样疲劳寿命达到10
7
次。相同喷丸强度下陶瓷喷丸疲劳性能提升更显著。单一弹丸介质喷丸处理后裂纹源均转移至次表层。复合喷丸平均疲劳寿命大幅降低,部分裂纹源出现在表面,归因于表面损伤和残余应力松弛。高强韧β 钛合金喷丸强化效果较好,对喷丸强度敏感性低、不易出现脱层或微裂纹缺陷,但对喷丸覆盖率较为敏感,不适用于复合喷丸或长时间喷丸处理。
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.
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