HYBRID GYRODYNE AIRCRAFT

A multi-rotor aircraft includes a fuselage, a propulsion engine coupled to the fuselage that generates thrust to propel the aircraft along a first vector during forward flight, and rotors coupled to the fuselage, each rotor comprising blades, each rotor coupled to a motor, and each motor configured...

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Bibliographische Detailangaben
Hauptverfasser: YONGE, Lawrence Winston, VANDER MEY, James E
Format: Patent
Sprache:eng ; fre ; ger
Schlagworte:
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