| 摘要 |
<p>A turbine shroud cooling assembly (100,200,300,400,500) for a gas turbine system (10) includes an outer shroud component (106) disposed within a turbine section (16) of the gas turbine system and proximate a turbine section casing (24), wherein the outer shroud component (106) includes at least one airway (105) for ingesting an airstream. Also included is an inner shroud component (102) disposed radially inward of, and fixedly connected to, the outer shroud component, wherein the inner shroud component includes a plurality of microchannels (110) extending in at least one of a circumferential direction and an axial direction for cooling the inner shroud component with the airstream from the at least one airway.</p> |
