发明公开
EP2318273A4 VTOL VEHICLE WITH COAXIALLY TILTED OR TILTABLE ROTORS 审中-公开
VTOL-FAHRZEUG MIT KOAXIAL GENEIGTEN ODER NEIGBAREN ROTOREN

VTOL VEHICLE WITH COAXIALLY TILTED OR TILTABLE ROTORS
摘要:
A VTOL vehicle includes a forward rotor, an aft rotor and a fuselage, the forward and aft rotor lying in a longitudinal axis of the vehicle, with the fuselage located axially between the forward and aft rotors. The vehicle has an in-flight configuration wherein the forward rotor is tilted downwardly at a negative tilt angle relative to the fuselage and the aft rotor is tilted upwardly at a positive tilt angle relative to the fuselage.
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