Turbine bucket for use in gas turbine engines and methods for fabricating the same

A turbine bucket (32) for use with a turbine engine is provided. The turbine bucket includes an airfoil (66) extending between a root end (88) and a tip end (90). The airfoil includes an outer wall (106) defining a cavity (112) extending from the root end to the tip end, the outer wall comprising a...

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1. Verfasser: Garcia-Crespo, Andres
Format: Patent
Sprache:eng ; fre ; ger
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Zusammenfassung:A turbine bucket (32) for use with a turbine engine is provided. The turbine bucket includes an airfoil (66) extending between a root end (88) and a tip end (90). The airfoil includes an outer wall (106) defining a cavity (112) extending from the root end to the tip end, the outer wall comprising a first ceramic matrix composite (CMC) substrate (107) extending a first distance from the root end to the tip end, and an inner wall (104) positioned within the cavity, the inner wall comprising a second CMC substrate (124) extending a second distance from the root end towards the tip end that is different than the first distance.