SYSTEM AND METHOD FOR IMPROVED ROTOR TIP PERFORMANCE

The present invention discloses systems (10) and methods for the performance enhancement of rotary wing aircraft through reduced torque, noise and vibration. In one embodiment, a system includes a sail (12) having an aerodynamic shape positioned proximate to a tip (14) of the rotor blade (16). An ac...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	MCVEIGH, MICHAEL, A, BUSSOM, RICHARD, C, ZIENTEK, THOMAS, A, NARDUCCI, ROBERT, P
Format:	Patent
Sprache:	eng ; fre
Schlagworte:	AEROPLANES AIRCRAFT AVIATION COSMONAUTICS HELICOPTERS PERFORMING OPERATIONS TRANSPORTING
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