Deburring Inconel Compressor Turbine Disc
The customer required controlled deburring of slots to keep within tolerances on a compressor turbine disc.
The customer required controlled deburring of slots to keep within tolerances on a compressor turbine disc.
The customer requested that their Aircraft Engine Compressor Disc made of Inconel be refurbished/repaired.
The customer requested deburring of the cut-out edges on an aluminum aircraft package that houses electronics.
Established inexpensive high volume approach to a one-step automatic process for deburring machined edges and imparting a cosmetic finish.
Established a one-step automatic process for deburring machined edges and imparting a cosmetic finish in a cellular environment.
Belair reduced the hand deburring of multiple geometric slots made with multiple sizes and forms while maintaining tight tolerances.
The customer’s goal was to establish a way to match a micro tech surface finish to achieve an ultra polish finish of less than Ra 6 µin.
The customer needed the surface reduced from 54 µin to a Ra of less than 10 µin. Bel Air automated this process and achieved a Ra of 8 µin.
Develop a faster more efficient, low-cost method of removing burrs from the gear teeth without a secondary machining operation.
Develop a faster more efficient, low-cost method of removing burrs from the gear teeth without a secondary machining operation.