The application relates to the technical field of
precision casting and discloses a
casting process for a multiple-
assembly high-temperature
alloy turbine guide vane for an aero-engine, which comprises the following steps: S1, preparing a vane mold according to the structure of the multiple-
assembly high-temperature
alloy turbine guide vane; S2, pressing a multiple-
assembly high-temperature
alloy turbine guide vane
wax mold: using the vane mold in step S1 and selecting
wax material, a vane
wax mold 8 is pressed by adopting an injection molding mode; S3, bonding a mold group: bonding two vane wax molds 8 prepared in step S2 and a pouring
system together to form a mold group; S4, preparing an
oxide ceramic mold shell, after the mold shell is air-dried, a dewaxing treatment is carried out; S5, pre-burning the
oxide ceramic mold shell; and S6, pouring alloy liquid. The multiple-assembly turbine guide vane
casting produced through the improvement of the vane wax mold preparation bonding scheme, the
oxide ceramic mold preparation process and the pouring process meets the index requirements in terms of grain size,
metallurgy and size control, and the production is stable.