MAIN ROTOR ROTATIONAL SPEED CONTROL FOR ROTORCRAFT

An aircraft includes an airframe having an extending tail, a counter rotating, coaxial main rotor assembly disposed at the airframe including an upper rotor assembly and a lower rotor assembly and a translational thrust system positioned at the extending tail and providing translational thrust to th...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	Eadie William J, Weiner Steven D
Format:	Patent
Sprache:	eng
Schlagworte:	AEROPLANES AIRCRAFT AVIATION COSMONAUTICS HELICOPTERS PERFORMING OPERATIONS TRANSPORTING
Online-Zugang:	Volltext bestellen
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