Aircraft rotor blade sleeve having a protuberance in its rear zone, and a rotor provided with such a sleeve

A sleeve connecting a blade to the hub of a rotor of a rotary wing aircraft. The sleeve has a leading edge and a trailing edge, together with a protuberance arranged on the trailing edge. The dimensions of the protuberance are linked to the dimensions of the sleeve. The presence of the protuberance...

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Bibliographische Detailangaben

Hauptverfasser:	Desvigne, Damien, Alfano, David
Format:	Patent
Sprache:	eng
Schlagworte:	AEROPLANES AIRCRAFT AVIATION COSMONAUTICS HELICOPTERS PERFORMING OPERATIONS TRANSPORTING
Online-Zugang:	Volltext bestellen
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