DAMPED TURBINE BLADE ASSEMBLY

A damped turbine blade assembly for a gas turbine engine is disclosed. The damped turbine blade assembly includes a damper positioned within a first small slot of a first turbine blade and a second large slot of the second turbine blade. A portion of the damper can slidably mate with the second larg...

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Bibliographische Detailangaben
Hauptverfasser: LAMICQ, Olivier Jacques, DUONG, Loc Quang
Format: Patent
Sprache:eng ; fre ; ger
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