A method is provided for repairing a turbine component with a distressed portion. The method includes machining the turbine component into a first intermediate turbine article such that the distressed portion is removed; and rebuilding the first intermediate turbine article into the turbine component with an additive manufacturing process.
申请公布号
EP2495397(A2)
申请公布日期
2012.09.05
申请号
EP20120157966
申请日期
2012.03.02
申请人
HONEYWELL INTERNATIONAL INC.
发明人
MITTENDORF, DON;RYAN, DANIEL;GODFREY, DONALD G.;MORRIS, MARK C.;KINGTON, HARRY
