Invention Grant
US09458731B2 Turbine shroud cooling system 有权
涡轮罩冷却系统

Turbine shroud cooling system
Abstract:
The present application provides a turbine shroud cooling system for a gas turbine engine. The turbine shroud cooling system may include a number of variable area cooling shrouds with tuning pins and a number of fixed area cooling shrouds with anti-rotation pins. The variable area cooling shrouds may include modulated cooling shrouds. The fixed area shrouds may include non-modulated shrouds.
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