Shroudless blade for a high-speed turbine stage

Described is a blade for a high-speed turbine stage of an aircraft gas turbine, in particular of an aircraft engine, the blade including a radially inner blade root, and an airfoil extending radially outwardly from the blade root. It is provided that the blade be shroudless and that the airfoil have...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: Pernleitner, Martin, Klingels, Hermann, Frischbier, Joerg, Maar, Karl, Wittmer, Jens
Format: Patent
Sprache:eng
Schlagworte:
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