Bucket assembly for turbine system and corresponding turbine system

A bucket assembly (30) is disclosed. The bucket assembly includes an airfoil (32) having a generally aerodynamic contour and defining a tip (52), and a lower body portion (34) extending generally radially inward from the airfoil (32). The bucket assembly further includes a tip shroud (60) disposed o...

Ausführliche Beschreibung

Gespeichert in:

Bibliographische Detailangaben
Hauptverfasser:	LACY, BENJAMIN PAUL, GIGLIO, ANTHONY LOUIS
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	BLASTING ENGINE PLANTS IN GENERAL HEATING INDEXING SCHEME FOR ASPECTS RELATING TONON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES ORJET-PROPULSION PLANTS INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUSSUBCLASSES OF CLASSES F01-F04 LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES WEAPONS
Online-Zugang:	Volltext bestellen
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!

Beschreibung
Zusammenfassung:	A bucket assembly (30) is disclosed. The bucket assembly includes an airfoil (32) having a generally aerodynamic contour and defining a tip (52), and a lower body portion (34) extending generally radially inward from the airfoil (32). The bucket assembly further includes a tip shroud (60) disposed on the tip (52) of the airfoil (32) and comprising a main body (62) and a rail (64). The rail (64) includes an exterior surface (66). The exterior surface (66) defines one or more microchannels (80). The bucket assembly (30) further includes a cover layer (82) configured on the exterior surface (66). A corresponding turbine system (10) is also provided.