Blade for a gas turbine

A blade, for a gas turbine, includes a blade airfoil, having a shroud segment arranged on its upper end. The shroud segment together with shroud segments of other blades of a blade row forming an annular shroud which delimits hot gas passage of the gas turbine, and said shroud segment, on sides on w...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: Riazantsev Sergei, Zambetti Chiara, Saxer-Felici Hélène
Format: Patent
Sprache:eng
Schlagworte:
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