VANE RING WITH FEED HOLE BLOCKAGE PREVENTER AND ASSOCIATED METHOD

A vane ring (70) for a gas turbine engine component includes a multiple of vanes (74) that extend between an inner vane platform (78) and an outer vane platform (82), each of the multiple of vanes (74) contains an airfoil cooling circuit (102) that receives cooling airflow (C) through a feed passage...

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Bibliographische Detailangaben
Hauptverfasser: COSHER, Christopher, BARGER, David, LUNDGREEN, Ryan, MCMAHON, Shawn M, TRINDADE, Ricardo, MADONNA, Nicholas J, HASSAN, Mohamed, PRENTER, Robin, PERRON, Christopher, ANIELLO, Justin M, GAUTSCHI, Steven Bruce, BARTLING, Brett Alan
Format: Patent
Sprache:eng ; fre ; ger
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Zusammenfassung:A vane ring (70) for a gas turbine engine component includes a multiple of vanes (74) that extend between an inner vane platform (78) and an outer vane platform (82), each of the multiple of vanes (74) contains an airfoil cooling circuit (102) that receives cooling airflow (C) through a feed passage (100) located in the outer vane platform (82) and an extension (110) from the outer vane platform (82), the extension (110) comprises a metering passage (112) in communication with the feed passage (100).