TURBOENGINE BLADING MEMBER

A turboengine blading member (1) is disclosed. The blading member comprises at least one airfoil (2) and at least one platform (31) provided at at least one of a base and a tip of the airfoil (2). The airfoil (2) comprising a profile body (23), a leading edge (21) provided at a first side of the pro...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: HERBERT BRANDL, THOMAS ZIERER, JOERG KRUECKELS
Format: Patent
Sprache:chi ; eng
Schlagworte:
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