Patent ID: 6896036

Claim:
A method of making a turbine blade having cooling channels therein, said method comprising the steps of: (a) producing an elongated ceramic core having a base portion at a base of a turbine blade to be made and a free end opposite said base portion, embedding at least one pin at said free end of said core so that said pin projects from said free end, said pin being composed of the nickel-based alloy NiCr82 and being formed with a circumferential groove, said pin being so embedded in the core that the circumferential groove is located in a region of a crown bottom of a turbine blade to be formed; (b) covering said ceramic core with a wax layer; (c) forming a ceramic shell on said wax layer by repeated immersion of the ceramic core with the wax layer thereon in a binder and coating with a ceramic material whereby said pin has opposite extremities embedded in said core and in said shell; (d) removing the wax from between said core and said ceramic shell to leave a space therebetween; (e) firing said ceramic shell; (f) casting a molten metal into said space and hardening the metal, thereby forming a turbine blade blank, said pin being incorporated in said turbine blade blank with metal of the blade blank filling said groove to provide a form-fitting engagement of said blade with said pin; (g) removing the core and the shell from the blade blank whereby said extremities of said pin project therefrom; and (h) machining the blade blank to form the turbine blade, thereby machining away the extremity of said pin which extended into said shell.