| 摘要 |
<p>A cooling assembly for a bucket of a turbine system includes a shroud assembly (50) operably coupled to an outer casing (24) of a turbine section (16). Also included is an airfoil (26) having at least one cavity (34), wherein the at least one cavity (34) is configured to receive a cooling flow (58) from a cooling source through at least one channel (60) disposed within the shroud assembly (50). A corresponding method of cooling a bucket is also provided.</p> |
