TY - JOUR
T1 - Formation Mechanism of Surface Metamorphic Layer on Turning End Face of GH4169 Superalloy
AU - Yao, Changfeng
AU - Shen, Xuehong
AU - Zhang, Dinghua
N1 - Publisher Copyright:
© 2017, Editorial Board of Journal of Aeronautical Materials. All right reserved.
PY - 2017/12/1
Y1 - 2017/12/1
N2 - Turning experiments and Deform-3D finite element methods were used to study the formation mechanism of surface metamorphic layer on turning GH4169 processed. The investigations were carried out by analyzing the changing of cutting force, the temperature and strain field, the residual stress, micro-hardness, microstructure, as well as the distribution of the above all along the direction of the depth under various process parameters. The results show that the surface metamorphic layer is formed due to the thermal-mechanical coupled effects on the microstructure of the material in the machining process. The cutting force, heat and strain of surface material are increased with the increase of machining intensity. Besides the higher strength of machining, the greater changes of plastic deformation, metallographic and grain deformation are acquired. In the range of processing parameters, the temperature layer is 130-200 μm, the strain layer is 100-220 μm, the residual stress layer is 80-110 μm, the depth of hardening layer is 50-80 μm, and the depth of surface metamorphic layer is 2.5-5μm.
AB - Turning experiments and Deform-3D finite element methods were used to study the formation mechanism of surface metamorphic layer on turning GH4169 processed. The investigations were carried out by analyzing the changing of cutting force, the temperature and strain field, the residual stress, micro-hardness, microstructure, as well as the distribution of the above all along the direction of the depth under various process parameters. The results show that the surface metamorphic layer is formed due to the thermal-mechanical coupled effects on the microstructure of the material in the machining process. The cutting force, heat and strain of surface material are increased with the increase of machining intensity. Besides the higher strength of machining, the greater changes of plastic deformation, metallographic and grain deformation are acquired. In the range of processing parameters, the temperature layer is 130-200 μm, the strain layer is 100-220 μm, the residual stress layer is 80-110 μm, the depth of hardening layer is 50-80 μm, and the depth of surface metamorphic layer is 2.5-5μm.
KW - Cutting force
KW - Micro-hardness
KW - Microstructure
KW - Residual stress
KW - Temperature-strain distribution
UR - http://www.scopus.com/inward/record.url?scp=85048660538&partnerID=8YFLogxK
U2 - 10.11868/j.issn.1005-5053.2017.000112
DO - 10.11868/j.issn.1005-5053.2017.000112
M3 - 文章
AN - SCOPUS:85048660538
SN - 1005-5053
VL - 37
SP - 50
EP - 58
JO - Hangkong Cailiao Xuebao/Journal of Aeronautical Materials
JF - Hangkong Cailiao Xuebao/Journal of Aeronautical Materials
IS - 6
ER -