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温度相关18CrNiMo7-6合金钢表面变质层断裂韧性的划痕法研究

INVESTIGATION ON TEMPERATURE-DEPENDENT FRACTURE TOUGHNESS OF SURFACE MODIFICATION LAYER OF 18CRNIMO7-6 ALLOY STEEL VIA SCRATCH TEST

  • 摘要: 工程关键构件服役过程中常面临着复杂的热-力耦合工况, 其表面变质层的断裂韧性是决定构件服役性能与寿命安全的核心指标之一. 重载齿轮、风电轴承等核心传动构件在热-力耦合工况下, 表面微裂纹极易萌生扩展, 易引发突发性断裂, 造成重大经济损失与安全隐患. 传统断裂韧性标准测试方法对试样尺寸要求严苛, 不仅需要制备大尺寸标准试样和高精度预制裂纹, 且只能获取均质材料的宏观平均性能, 难以实现对微米级表面变质层的微损、高分辨率定量表征. 针对上述难题, 本文以含表面变质层18CrNiMo7-6合金钢为研究对象, 系统开展300 K~673 K环境温度下的常载荷划痕试验, 获取了不同温度下材料的切向力、划痕深度、划痕宽度及裂纹形貌等关键响应参数, 引入3种断裂力学模型反演材料表面变质层的断裂韧性参数, 并结合相应温度下的小冲杆试验(Small Punch Test, SPT)结果进行独立交叉验证. 研究结果表明, 在不同的温度环境下, 表面变质层不同深度材料的断裂韧性随深度的增加而增加. 在300 K与473K 温度下划痕试验反演结果与小冲杆试验结果规律一致, 最大相对误差低于20%, 但在673 K温度下的规律存在一定差异, 需要在后续进行深入研究. 研究成果可为18CrNiMo7-6钢构件在热-力耦合工况下的断裂抗力评估与服役寿命预测提供关键参数支撑, 对保障重载齿轮等关键零部件的结构完整性具有重要参考价值.

     

    Abstract: Key engineering components frequently operate under complex thermo-mechanical coupled conditions during service. The fracture toughness of the surface modification layer is a core indicator determining the service performance and structural integrity of these components. Core transmission components such as heavy-duty gears and wind turbine bearings are prone to surface microcrack initiation and propagation under thermo-mechanical coupled conditions, which can easily lead to sudden fracture failure and cause significant economic losses and safety hazards.Traditional standard testing methods for fracture toughness impose strict requirements on specimen dimensions, which not only require the preparation of large-size standard specimens and high-precision pre-cracks, but also can only obtain the macroscopic average properties of homogeneous materials, making it difficult to achieve micro-destructive, high-resolution quantitative characterization of micron-scale surface modification layers.To address these challenges, this study investigates surface modification layer of 18CrNiMo7-6 alloy steel by systematically conducting constant-load scratch tests at ambient temperatures ranging from 300 K to 673 K. And obtains key response parameters such as tangential force, scratch depth, scratch width and crack morphology of materials at different temperatures. Three fracture mechanics models are introduced to inversely determine the fracture toughness parameters of the material's gradient layer, which are then independently cross-validated using small punch test (SPT) results at corresponding temperatures. The research results show that under different ambient temperature conditions, the fracture toughness of materials at different depths of surface modified layer increases with the increase of depth.The inverse calculation results from scratch tests exhibit consistent trends with the results of small punch tests at 300 K and 473 K, with a maximum relative error of less than 20%. However, there are certain discrepancies in the variation trends at 673 K, which requires further in-depth investigation in subsequent studies.The research findings provide critical parameter support for the fracture resistance assessment and service life prediction of 18CrNiMo7-6 steel components under thermo-mechanical coupling conditions, offering significant reference value for ensuring the structural integrity of critical parts such as heavy-duty gears.

     

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