Abstract：The surface quality of turbine blade in aviation gas turbine engine directly affects the overall performance of the engine. In view of the low geometric accuracy and unstable quality in the surface treatment of turbine blade at home and abroad, the magnetic abrasive technology with magnetic needle is introduced, and different types of magnetic needle, rotating speed of magnetic pole and grinding time are taken as variable factors. The surface roughness and residual stress of the blade are taken as the indexes, and the law between the change factors and the index parameters is analyzed through experiments. The results show that the residual stress on the surface of turbine blade changes from original tensile stress to compressive stress, and the compressive stress increases with the increase of magnetic needle length and magnetic pole speed. The surface roughness of turbine blade and the burr height around the gas film hole are improved obviously by magnetic needle grinding. The research results can provide a reference for improving the surface quality of turbine blade by magnetic needle grinding process.
朱慧宁，马小刚，程海东，陈燕，韩冰. 磁针磁力研磨工艺对发动机涡轮叶片表面质量的试验研究[J]. 航空制造技术, 2021, 64(18): 62-68.
ZHU Huining, MA Xiaogang, CHENG Haidong, CHEN Yan, HAN Bing. Experimental Study on Surface Quality of Engine Turbine Blade by Magnetic Needle Magnetic Abrasive Technology. Aeronautical Manufacturing Technology, 2021, 64(18): 62-68.
2021, 
