Abstract:Abstract:Nickel-based superalloy Inconel 718 possesses high strength and corrosion resistance, which is widely applied in aviation industry, especially the high temperature components of gas turbine engines. However, the final forming grinding process often forms a large residual tensile stress on the surface of the parts, which is detrimental to the fatigue strength and life of the parts. A combined grinding process based on the principle of the thermal gradient adjustment in grinding zone is studied, which c… Show more
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