ROTOR FOR HELICOPTER WITH IMPROVED DAMPING

The present invention relates to a rotor (1, 1', 1'', 1''', 1''', 1''') for helicopter comprising a shaft (2) adapted to be put into rotation by at least one engine element, a hub (3) splined to the shaft (2), at least four blades (4) radia...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	FRISON, Leonardo Antonio, MASARATI, Pierangelo
Format:	Patent
Sprache:	eng ; fre
Schlagworte:	AEROPLANES AIRCRAFT AVIATION COSMONAUTICS HELICOPTERS PERFORMING OPERATIONS TRANSPORTING
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