STATOR VANE ASSEMBLY HAVING MATE FACE SEAL WITH COOLING HOLES

A stator vane assembly (10) for a gas turbine engine includes a first endwall segment (12) and a second endwall segment (14) arranged circumferentially spaced from each other, whereby a mate face gap (20) is defined between a first mate face (22) of the first endwall segment (12) and a second mate f...

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Bibliographische Detailangaben
Hauptverfasser: AZAD, Gm Salam, LEE, Ching-Pang
Format: Patent
Sprache:eng ; fre
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