A VTOL aircraft having thrust and directional control comprises a fan for providing a centrifugal flow of air. At least one duct allows for and directs air flow. At least one nozzle allows for exhaust release. Each of the at least one nozzle has a first end attached to one of each of the at least one duct. Each of the at least one nozzle has a turn measuring 90 and faces downward from the second end of each of the at least one duct. Each of the at least one nozzle has a second end at which is a vane for redirecting airflow. The VTOL aircraft also has an attachment for landing.
VTOL AIRCRAFT HAVING DUCTED THRUST FROM A CENTRAL FAN
SENKRECHTSTART- UND -LANDEFLUGZEUG MIT KANALISIERTEM SCHUB AUS EINEM ZENTRALEN LÜFTER
AÉRONEF VTOL AYANT UNE POUSSÉE CANALISÉE À PARTIR D'UN VENTILATEUR CENTRAL
2021-01-13
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |