GAS TURBINE BLADE COMPRISING WINGLETS TO COMPENSATE CENTRIFUGAL FORCES

A rotating blade for a gas turbine (5) is provided with: €¢ a root (17) configured to be coupled to a disc of the gas turbine (5) which rotates about an axis (A) of the gas turbine (5); a platform (20) coupled to the root (17); €¢ an airfoil (18) extending from the platform (20) and provided with a...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: BERETTA-MUELLER, Arrigo, GERSBACH, Frank, REITER, Jonas, NAIK, Shailendra
Format: Patent
Sprache:eng ; fre ; ger
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