目的 揭示激光冲击-机械喷丸复合强化工艺对齿轮钢表面微观组织的影响机制。方法 采用X射线衍射线形分析(XRDLPA)方法,对比研究不同强化工艺(渗碳磨削、常规喷丸、激光冲击+常规喷丸、激光冲击+常规喷丸+微粒喷丸)对齿轮钢微观组织(位错密度、位错特性、晶块尺寸、微观应变、相含量)的影响,并通过透射电子显微(TEM)技术及三点弯曲疲劳试验分别验证XRDLPA方法的可行性,以及激光冲击-机械喷丸复合强化工艺对齿轮钢疲劳性能的提升效果。结果 通过复合强化工艺,将齿轮钢表面的位错密度由2.73×1016 m-2增至3.09×1016 m-2,马氏体中位错类型表现为螺型-刃型混合位错,螺型位错发生交滑移,其含量降低,刃型位错含量增加。通过复合强化工艺,促进了齿轮钢表面位错偶极子和位错胞的形成,位错排列参数M由7.3降至5.8;促进了晶块尺寸的均匀分布,平均晶块尺寸由57.1 nm细化至36.7 nm;基于位错增殖分割机制,齿轮钢表面形成了纳米化组织。基于原子滑移程度的不同,(200)晶面晶块尺寸最小,微观应变最大,(222)晶面晶块尺寸最大,微观应变最小。通过复合强化工艺促进了马氏体相变,齿轮钢中马氏体相含量由63.4%增至84%。采用激光冲击-机械喷丸处理后,齿轮钢弯曲疲劳寿命较渗碳磨削态试样提升了33.6倍(540 MPa,应力幅)。结论 基于XRDLPA方法,对激光冲击-机械喷丸复合强化齿轮钢表面微观组织特性进行定量分析是可行的。通过激光冲击-机械喷丸复合强化工艺诱导塑性应变,可促进位错增殖、晶块细化、马氏体相变,多尺度改善了齿轮钢表面微观组织结构,进而有效提升了齿轮钢弯曲疲劳寿命。
Abstract
Heavy-duty gears are subject to alternating loads, high torque as well as harsh service conditions, and bending fatigue is the main failure mode, seriously affecting the comprehensive performance of gears. Conventional shot peening (CSP) is a common method for gear surface strengthening. It introduces high magnitude compressive residual stress, but the induced surface roughness is relatively large, which restricts the manufacturing of high-performance gears. Laser shock peening (LSP) can introduce a deeper compressive stress layer, but the compressive stress level is lower than that of CSP. Fine particle peening (FPP) can improve the surface roughness and enlarge the compressive stress level on the exterior surface of gears, but the compressive stress layer is shallow. Therefore, the existing strengthening methods cannot meet the current technical performance requirements of heavy-duty gears. To address this issue, laser shock-mechanical shot peening compound strengthening method is proposed in this work and the induced microstructural features affecting the bending life of gears are experimentally investigated.
Carburized and ground gear steels made of 20CrMnTi are used in this work, and the dimension of each sample is 30 mm× 50 mm×5 mm. Three kinds of strengthening methods, in terms of CSP (media diameter of 0.8 mm, intensity of 0.52 mmA, coverage of 100%), FPP (media diameter of 0.05 mm, intensity of 0.14 mmN, coverage of 100%), and LSP (pulse energy of 4 J, spot diameter of 2 mm, overlap of 50%, pulse width of 20 ns), are combined to form a laser shock-mechanical shot peening compound strengthening process. Since LSP has strict requirements on the surface roughness of workpieces, this process is arranged before CSP. FPP is often used as the final strengthening process to improve the roughness of workpieces, so it is arranged after LSP and CSP. Considering the processing efficiency, CSP, FPP, and LSP are used for treating gear steels only once. This work aims to reveal the microstructure evolution of gear steels treated by laser shock-mechanical shot peening compound strengthening process. X-ray diffraction line profile analysis (XRDLPA) method is applied to comparatively study the effect of different strengthening processes (carburizing and grinding, conventional shot peening, laser shock peening + conventional shot peening, laser shock peening + conventional shot peening + fine particle peening) on the microstructure (dislocation density, crystallite size, micro-strain and phase fraction) of the gear steels. A three-point bending fatigue test is designed to reveal the effect of the compound strengthening method on the fatigue life of gear steels.
The results show that it is feasible to conduct a quantitative investigation on the microstructural characteristics of gear steels subject to laser shock-mechanical shot peening compound treatment with XRDLPA method. Laser shock-mechanical shot peening compound strengthening process can promote dislocation multiplication, crystallite refinement and phase transformation, thereby improving the surface microstructure of gear steels on multiple scales. The compound method can effectively enhance the bending fatigue life of gear steels. Specifically, with the application of the compound treatment, the dislocation density for martensite increases from 2.73×1016 to 3.09×1016 m-2 in the form of screw-edge-mixed type. The fraction of screw dislocation decreases due to the occurrence of cross-slip, whereas the fraction of edge dislocation increases. The formation of dislocation dipoles or dislocation cells in the surface layer can be further promoted by the compound strengthening process, and the dislocation arrangement parameter M decreases from 7.3 to 5.8. With the adoption of the compound treatment, the average crystallite size on the surface of gear steels decreases from 57.1 to 36.7 nm, and the uniformity distribution of the crystallite size is improved. Because of dislocation multiplication and division mechanism, nanostructured layers are generated on the surface of gear steels. Due to the different degrees of atomic slip, the (200) crystallographic plane exhibits the smallest crystallite size and highest micro-strain, whereas the (222) plane shows the smallest micro-strain and the largest crystallite size. With the employment of the compound treatment, the martensite fraction of gear steels increases from 63.4% to 84% resulting from martensite transformation. With the use of the compound treatment, the bending fatigue life of gear steels increases by 33.6 times (under the stress amplitude of 540 MPa).
关键词
激光冲击 /
机械喷丸 /
齿轮钢 /
复合强化 /
XRD线形分析 /
微观组织
Key words
laser shock peening /
mechanical shot peening /
gear steel /
compound strengthening /
XRD line profile analysis /
microstructure
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基金
国家自然科学基金(52405609, 52305081); 湖南省自然科学基金(2023JJ40049); 湖南省重点研发计划(2025JK2012)