The invention relates to a method of eliminating deformation of a
wax mould for an ultrathin elongated working blade of a
turbine, and belongs to the technical field of manufacturing of blades of
aviation engines. The method overcomes disadvantages in the prior art, provides a scheme of carrying and installing the blade
wax mould by utilizing a
wax mould clamping fixture, and discloses a design scheme of the wax mould clamping fixture. In an actual development and production process of a
turbine working blade, because the wax mould clamping fixture is utilized to carry and install the blade wax mould, deformation of the blade wax mould is effectively controlled, and the deformation amount of the
turbine working blade manufactured by utilization of the blade wax mould is reduced from original about 1 mm to now about 0.3 mm. Because the deformation amount is reduced, blade correction becomes relatively easy, thus avoiding generation of correction cracks, increasing the yield of
precision casting of the turbine working blade by about 20%, largely reducing the
rejection rate of the blade and largely saving the production cost.