The medium-temperature
radial forging method comprises the steps that pretreatment is conducted, specifically, a
niobium-
tungsten alloy extrusion bar blank is heated for 60-180 minutes at the temperature of 750-950 DEG C, rapid
forging and straightening are conducted, and a medium-temperature
radial forging bar blank is obtained and annealed for 60-120 minutes at the temperature of 1250-1450 DEG C; medium-temperature
radial forging is conducted, specifically, a two-
step method is adopted, in the first step, a bar blank is preheated to 80-100 DEG C and coated with Ta1350 high-temperature glass
powder, heat preservation is conducted for 90-180 minutes at the temperature of 1050-1150 DEG C, and the bar blank is forged into a bar with the
diameter of 70 + / -1 mm in the mode that the
diameter is reduced by 7-10 mm every time; and in the second step, the heating and
coating processes are repeated, the
diameter is reduced by 5-7 mm every time, and the bar with the required specification is manufactured. By optimizing the medium-temperature
forging and annealing process, the
fine grain structure is controlled, the high-temperature
mechanical property,
creep resistance and
oxidation resistance of the material are improved, and the material is suitable for
aerospace engines and other high-temperature and high-pressure scenes. Compared with a traditional method, the technology improves the yield, shortens the production period, reduces the labor intensity, is suitable for large-scale production, reduces surface air suction, oxidation and burning loss, and improves the production efficiency and the finished product quality.