The
forging forming method for the high-temperature
alloy blade of the large gas
turbine is suitable for controlling
thermal deformation in the blade
machining process and comprises the steps that S1, a high-temperature
alloy blank is selected, and the blank is subjected to rough turning
machining according to the design requirement of the blade so that a bar with end fillets can be formed at the two ends; s2, the bar is subjected to
upset forging heating and formed at a time through an
upset forging die, and an upset-forged blank is formed; s3, according to design requirements, a lower tenon and a blade body of the upset blank are subjected to turn-milling
machining to the target size, a glass
lubricant is sprayed, and heating is conducted; s4, a
small head of the heated upset blank is flattened in a flattening cavity of a pre-
forging die, then the blank is turned over by 90 degrees, a blade body is flattened in the pre-
forging cavity, and a blank piece is formed; s5,
oxide skin on the surface of the blank is removed, a lubricating agent is sprayed, and it is guaranteed that the surface of the blank is smooth; s6, forming leaves; and S7, the blade is subjected to deburring, heat treatment and
sand blasting treatment and is detected, and the machining efficiency of the blade is improved.