谢志勇,解丽静,高飞农,王西彬,任雁,李宏伟. 基于纳米压痕技术的齿根渗碳层力学特征表征[J]. 航空制造技术, 2023, 66(23/24): 70-78. XIE Zhiyong, XIE Lijing, GAO Feinong, WANG Xibin, REN Yan, LI Hongwei. Characterization on Mechanical Properties of Carburized Layer at Gear Root Based on Nano-Indentation Technology[J]. Aeronautical Manufacturing Technology, 2023, 66(23/24): 70-78.
XIE Zhiyong, XIE Lijing, GAO Feinong, et al. Characterization on Mechanical Properties of Carburized Layer at Gear Root Based on Nano-Indentation Technology[J]. Aeronautical Manufacturing Technology, 2023, 66(23/24).
谢志勇,解丽静,高飞农,王西彬,任雁,李宏伟. 基于纳米压痕技术的齿根渗碳层力学特征表征[J]. 航空制造技术, 2023, 66(23/24): 70-78. XIE Zhiyong, XIE Lijing, GAO Feinong, WANG Xibin, REN Yan, LI Hongwei. Characterization on Mechanical Properties of Carburized Layer at Gear Root Based on Nano-Indentation Technology[J]. Aeronautical Manufacturing Technology, 2023, 66(23/24): 70-78. DOI: 10.16080/j.issn1671-833x.2023.23/24.070.
XIE Zhiyong, XIE Lijing, GAO Feinong, et al. Characterization on Mechanical Properties of Carburized Layer at Gear Root Based on Nano-Indentation Technology[J]. Aeronautical Manufacturing Technology, 2023, 66(23/24). DOI: 10.16080/j.issn1671-833x.2023.23/24.070.
Characterization on Mechanical Properties of Carburized Layer at Gear Root Based on Nano-Indentation Technology
The carburized layer at 18Cr2Ni4WA steel gear root has mechanical behavior different from the substrate. Its accurate characterization is important for the analysis on the crack initiation and fatigue properties of the gear root. The nano-indentation test is taken as the test measure for the characterization of the local mechanical behavior in the carburized layer. Nano-indentation tests are carried out within the carburized layer. The finite element simulations of nano-indentation tests with different sets of constitutive model parameters combination are performed. Based on the simulated and the experimental load-displacement curves
the combined prediction errors of curvature
residual depth and the ratio of plastic deformation work to total deformation work are calculated. In result
the constitutive model parameters are defined for the carburized layer. It is verified that the constitutive model derived by this method can reflect the mechanical behavior of the carburized layer.