高世民,全 芳,陈志同. GH4169材料磨削后数控抛光表面完整性试验研究*[J]. 航空制造技术, 2016, 59(23/24): 52-56. GAO Shimin, QUAN Fang, CHEN Zhitong. Research on Surface Integrity for GH4169 of CNC Polishing After Grinding. Aeronautical Manufacturing Technology, 2016, 59(23/24): 52-56.
GAO Shimin, QUAN Fang. Research on Surface Integrity for GH4169 of CNC Polishing After Grinding[J]. Aeronautical Manufacturing Technology, 2016, 59(23/24).
高世民,全 芳,陈志同. GH4169材料磨削后数控抛光表面完整性试验研究*[J]. 航空制造技术, 2016, 59(23/24): 52-56. GAO Shimin, QUAN Fang, CHEN Zhitong. Research on Surface Integrity for GH4169 of CNC Polishing After Grinding. Aeronautical Manufacturing Technology, 2016, 59(23/24): 52-56. DOI: 10.16080/j.issn1671-833x.2016.23/24.052.
GAO Shimin, QUAN Fang. Research on Surface Integrity for GH4169 of CNC Polishing After Grinding[J]. Aeronautical Manufacturing Technology, 2016, 59(23/24). DOI: 10.16080/j.issn1671-833x.2016.23/24.052.
Research on Surface Integrity for GH4169 of CNC Polishing After Grinding
the process of CNC polishing after CBN wheel grinding was conducted. Firstly
the influence of the pre-compression parameter on life of wool wheel and the roughness were studied. The influences of polishing depth on the surface topographic characters of surface integrity including surface roughness
surface micro-hardness
and surface residual stress
were studied to optimize the polishing depth. With the increasing of the polishing depth
the roughness Ra drops firstly and then gets stable
and the surface micro-hardness decreases. The normal residual stress in the feed direction shows a trend from rise to decline
while in the vertical feed direction
it stays unchanged basically and then decreases. The polishing depth after optimized is 2μm
and pre-compression parameter is about from 0.5mm to 1.0mm. It has a small roughness of 0.3μm
a macro-hardness of HV389.36 and the high compressive stresses after CBN grinding
which are -871.6MPa and -1084.0MPa for two principal stress directions.
CNC Polishing Surface Residual Stress Analysis for GH4169 After Grinding
Study on Material Removal Behavior and Surface Integrity of Robotic Belt Grinding for Titanium Alloy Hollow Components Fabricated by Additive Manufacturing
Experimental Research on Surface Integrity of Shot Peening K417G Superalloy
Study on Effect of Different Shot Peening Intensities on Surface Integrity of FGH96 Powder Metallurgy Superalloy
Effect of Surface Integrity of Milling TA15 Titanium Alloy on Fatigue Life
Related Author
CHAI Dongsheng
WANG Huanchen
LIU Zhenyang
XIAO Guijian
MA Fangwei
MIN Xianglu
HAN Wei
LIANG Qiaoyun
Related Institution
Key Laboratory of High Performance Manufacturing for Aero Engine, Ministry of Industry and Information Technology, Northwestern Polytechnical University