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US08668442B2 Turbine nozzles and methods of manufacturing the same 失效
涡轮喷嘴及其制造方法

Turbine nozzles and methods of manufacturing the same
Abstract:
A turbine nozzle is provided and includes a first ring having a first microstructure, a vane extending from the first ring, a first porous zone between the first ring and the vane that is more porous than the first microstructure to attenuate thermo-mechanical fatigue cracking between the vane and the first ring. Methods of manufacturing the turbine nozzle are also provided.
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