Lightweight cast inner diameter vane shroud for variable stator vanes
An inner diameter vane shroud (14) for use in a gas turbine engine is comprised of lightweight cast forward and aft shroud components (20; 22). The forward and aft shroud components (20; 22) are made with an investment casting technique that creates a hollow cavity (30; 32) that runs in a circumfere...
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Format: | Patent |
Sprache: | eng ; fre ; ger |
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Zusammenfassung: | An inner diameter vane shroud (14) for use in a gas turbine engine is comprised of lightweight cast forward and aft shroud components (20; 22). The forward and aft shroud components (20; 22) are made with an investment casting technique that creates a hollow cavity (30; 32) that runs in a circumferential direction through each component. The forward and aft shroud components (20; 22) are matable to form sockets (24A) that receive inner diameter ends of variable stator vanes (28A). |
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