TURBINE BLADE HAVING AN IMPROVED STRUCTURE

An aviation turbine blade (10) includes at least a first lower surface cavity (C2) and a first upper surface cavity (C3), each adjacent to a first through-cavity (C1) and a second through-cavity (C4), the first upper surface cavity (C3) being adjacent to the upper surface wall (24), the first lower...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	ROLLINGER, Adrien Bernard Vincent, PAQUIN, Sylvain, CARIOU, Romain Pierre, FLAMME, Thomas Michel
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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