Turbine rotor blade and method of assembling the same

A rotor blade assembly includes a shank, an airfoil that is formed integrally with the shank, and a removable platform coupled between said shank and said airfoil via a friction fit. A method of assembling a gas turbine engine rotor blade assembly that includes a removable platform, and a gas turbin...

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Bibliographische Detailangaben

Hauptverfasser:	Keith, Sean Robert, Danowski, Michael Joseph, Leeke, Jr, Leslie Eugene
Format:	Patent
Sprache:	eng
Online-Zugang:	Volltext bestellen
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