Adjustment Of Turbine Engine Part

Abstract: The invention relates to a method for adjusting a turbine engine part to be placed in a gas stream of the turbine engine, the part having previously undergone a material addition operation in order to fill in a defect in at least one area of the surface thereof, resulting in an extra thickness in at least one area of the surface thereof, characterised in that the method comprises steps of: - ordering (E1) the formation of a three-dimensional image of the part; - identifying (E2) the at least one area of the surface of the part that includes the extra thickness, and identifying the extra thickness, in the three-dimensional image of the part; - determining (E3) a trajectory of an adjustment tool, as a function of the geometry of the extra thickness identified; and - ordering (E4) the adjustment of the part according to the trajectory determined.

Patent Information

Applicants

Inventors

Specification

Documents

Application Documents