发明授权
US09447689B2 Method of repairing a turbine nozzle segment in a turbine engine 有权
修复涡轮发动机中的涡轮喷嘴段的方法

Method of repairing a turbine nozzle segment in a turbine engine
摘要:
A method for repairing a turbine nozzle having at least one vane disposed between an inner and an outer band. Embodiments of the method can comprise separating the inner band from the outer band and securing a replacement part to the inner band. In one embodiment, the methods accommodate replacement parts that include vanes with a base feature that comprises a non-airfoil shape and that integrates cooling features useful for operation of the turbine nozzle.
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