A bladeless unmanned aerial vehicle includes a body and two or more thruster assemblies coupled to the body. The thruster assemblies each includes a ducted fan compressor and a discharge frame. The discharge frames may be bladeless fans or may be nozzles. The discharge frames may be positioned substantially vertically, tilted at an angle about an axis extending radially from the center of the body, and/or angled in a vertical plane aligned with an axis extending radially from the center of the body.
BLADELESS UNMANNED AERIAL VEHICLE
02.05.2019
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |