An aerial vehicle pertinent to the present application has a rotor system that operates in both a vertical-take-off-landing (VTOL) and a cruise mode. There are boom structures which support rotors and the tail. Tiltable rotors are located at the front ends of the booms. The rear rotors are placed under an upward rise in the booms, which allows for reduced in-flight drag and eliminates the need for collapsible rotors when said rotors are not actively operational.
STRUCTURAL FEATURES OF VERTICAL TAKE-OFF AND LANDING (VTOL) AERIAL VEHICLE
30.11.2023
Patent
Elektronische Ressource
Englisch
VTOL (vertical take-off and landing) UAV (unmanned aerial vehicle)
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