COOLING ASSEMBLY FOR BUCKET OF TURBINE SYSTEM AND COOLING METHOD

PROBLEM TO BE SOLVED: To provide a cooling assembly for a bucket of a turbine system and a cooling method.SOLUTION: A cooling assembly for a bucket of a turbine system includes a shroud assembly operably coupled to an outer casing of a turbine section. The cooling assembly also includes an airfoil h...

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Bibliographische Detailangaben
1. Verfasser:	WASSYNGER STEPHEN PAUL
Format:	Patent
Sprache:	eng
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ENGINE PLANTS IN GENERAL GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES WEAPONS
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Beschreibung
Zusammenfassung:	PROBLEM TO BE SOLVED: To provide a cooling assembly for a bucket of a turbine system and a cooling method.SOLUTION: A cooling assembly for a bucket of a turbine system includes a shroud assembly operably coupled to an outer casing of a turbine section. The cooling assembly also includes an airfoil having at least one cavity, wherein the at least one cavity is configured to receive a cooling flow from a cooling source through at least one channel disposed within the shroud assembly.