Peening coverage has essential effects on the service performance of parts. In this paper
aluminum alloy 2024–T351 was subjected to pneumatic shot peening with different coverage of 88.3%
100%
200% and 400% by adjusting feeding speed. The surface topography and microstructure
roughness
residual stress and microhardness were investigated using a scanning electron microscope
roughness tester
residual stress instrument and Vickers hardness tester. The surface roughness increases first and then decreases with the increase of peening coverage. The average surface roughness of peened sample with 100% coverage is 4.601 μm
which is the highest value. Moreover
the peened surface shows significant folds and microcracks owing to the high coverage of 400%. The increase of peening coverage leads to the enlargement of the maximum compressive residual stress and depth of the compressive residual stress layer. Similarly
the maximum hardness and hardened layer depth are enhanced with peening coverage. The maximum hardness corresponding to peening coverage of 88.3%
Experimental Research on Surface Integrity of Shot Peening K417G Superalloy
Effect of Shot Peening Coverage on Residual Stress and Surface Roughness of 9310 Aircraft Gear
Numerical Study on Surface Integrity of Shot-Peened Aluminum
Effect of Shot Peening on Surface Integrity and Fatigue Life of TC17 Alloy
Study on Effect of Different Shot Peening Intensities on Surface Integrity of FGH96 Powder Metallurgy Superalloy
Related Author
MA Fangwei
MIN Xianglu
HAN Wei
LIANG Qiaoyun
YUAN Peiyu
TAN Liang
WANG Changqing
Lü Liangliang
Related Institution
AECC Shenyang Liming Aero-Engine Co. Ltd.
Key Laboratory of High Performance Manufacturing for Aero Engine, Ministry of Industry and Information Technology, Northwestern Polytechnical University
AECC Harbin Dongan Engine Co., Ltd.
Central South University
School of Mechanical Engineering, Anhui University of Science and Technology