TURBOMACHINE COMPONENT WITH NON-AXISYMMETRIC SURFACE

The present invention relates to a turbomachine component (1) or collection of components comprising at least a first and a second blade (3I, 3E) and a platform (2) from which the blades (3I, 3E) extend, characterized in that the platform (2) has a non-axisymmetric surface (S) bounded by a first and...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	BERNARDOSAMAGNE, Esteban, VOLLEBREGT, Matthieu, Jean Luc, LUKOWSKI, Benjamin
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	BLASTING ENGINE PLANTS IN GENERAL HEATING LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES WEAPONS
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