The present invention relates generally to a vertical take-off and landing (VTOL) aircraft and a propulsion system for a vehicle vertical take-off and landing (VTOL), for example, helicopters, others VTOL aircrafts. The claimed VTOL aircraft provides a most effective control of the aircraft equipped with such a propulsion system, performed through the optimal distribution of the airflow generated by the rotor, while maintaining the simplicity, reliability and efficiency of the aircraft design.
VERTICAL TAKE-OFF AND LANDING (VTOL) AIRCRAFT AND A PROPULSION SYSTEM FOR A VEHICLE VERTICAL TAKE-OFF AND LANDING (VTOL)
2019-01-17
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |