Electroplated wheels have excellent formability and shape holding capacity which make it more and more widely used in complex curved surface grinding. But the researches on the surface integrity influenced by wheel wear is insufficient. Therefore
the surface topography feature of cantilever plunge grinding were studied and the roughness changing with wheel wear were recorded when the rectangular specimens with high stiffness and a kind of motor stator vane with weak stiffness were grinded. The result show that the appropriate wear can make the roughness fell by 35%. But the wear has little influence on surface hardness and residual stress. The weak stiffness of aero-engine blade can increase the roughness. The appropriate wear not only can make the blade top edge roughness reduce by 64% but also can weaken the influence on roughness by stiffness and improve the uniformity of surface integrity. So the wear of electroplated wheels can be estimated by workpiece roughness. The conclusion can help select the wheels with appropriate wear for finish grinding. It contributes to decrease the roughness of workpiece and improve the uniformity of surface integrity.
Effect of Ultrasonic-Assisted Laser Shock Peening on Tensile Property of 7075–T6 Aluminum Alloy
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
Progress of Friction and Wear Properties of Continuous Fiber Reinforced High-Performance Thermoplastic Composites
Study on Effect of Different Shot Peening Intensities on Surface Integrity of FGH96 Powder Metallurgy Superalloy
Related Author
CHENG Zilong
MENG Xiankai
LIU Yang
WEI Shuai
SONG Fuyang
CHAI Dongsheng
WANG Huanchen
LIU Zhenyang
Related Institution
Institute of Advanced Manufacturing and Modern Equipment Technology, Jiangsu University
School of Mechanical Engineering, Jiangsu University
Key Laboratory of High Performance Manufacturing for Aero Engine, Ministry of Industry and Information Technology, Northwestern Polytechnical University