The invention discloses a high-temperature
alloy turbine blade
directional solidification method based on multistage dynamic
gas protection control. The high-temperature
alloy turbine blade
directional solidification method comprises the following steps that a high-temperature
alloy mother alloy material is put into a
crucible; filling
inert gas to a preset pressure, heating the
crucible, heating to a preset temperature, and keeping the temperature to ensure that the alloy liquid is liquefied; continuously filling
inert gas to preset pressure and then refining, wherein a vibration generator generates a
magnetic field in the refining process to carry out
electromagnetic vibration on the alloy liquid; continuously filling
inert gas to preset pressure, and then transferring the
crucible;
inert gas is continuously filled to preset pressure, then the crucible is tilted, pouring is conducted, and in the pouring process, a gas purging device sprays the
inert gas to conduct purging protection on the alloy liquid; and continuously filling
inert gas to preset pressure, and pulling the shell to finish the
directional solidification process. The method can reduce the gas content in the melt, prevent the melt from being oxidized, promote the removal of a
surface oxidation film, reduce pores and oxidation film inclusion, and improve the purity, mechanical properties and yield of the
casting.