Trailing edge adjustable weight system for helicopter main rotor blades

A system of adjustable balancing weights is provided for a helicopter main rotor blade (42). The trailing edge (52) of the rotor blade (42) is formed with a plurality of recesses (74) that each receive an aerodynamically shaped weight (92,92') to adjust and balance the weight of the rotor blade...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	HENTHORN, KEVIN, MCNULTY, MICHAEL J, LOFTUS, ROBERT T
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AEROPLANES AIRCRAFT AVIATION COSMONAUTICS HELICOPTERS PERFORMING OPERATIONS TRANSPORTING
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