Invention Grant
US06976653B2 VTOL micro-aircraft 失效
VTOL微型飞机

VTOL micro-aircraft
Abstract:
VTOL micro-aircraft comprising a first and a second ducted rotor mutually aligned and distanced according to a common axis and whose propellers are driven in rotation in mutually opposite directions. Between the two ducted rotors are positioned a fuselage and a wing system formed by wing profiles forming an X or an H configuration and provided with control flaps.
Public/Granted literature
Information query
Patent Agency Ranking
0/0