A dual-state propulsion aircraft includes an aircraft fuselage; and at least one dual-state propulsion system, including a fixed nacelle, a rotatable nacelle optionally including a front curved section and rear straight section, mechanical nacelle rotation stops, mechanical shaft rotation stops, a motor, and a thruster with pivotable blades; such that the at least one dual-state propulsion system is rotatable to a first system position configured for horizontal flight and to a second system position configured for vertical flight.
Dual-state rotatable propulsion system
2023-11-09
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
Variable-caliber rotatable nozzle and water jet propulsion system
European Patent Office | 2024
|FREE TILTING ROTATABLE AND REVERSIBLE GEAR BOX FOR OUTBOARD PROPULSION SYSTEM
European Patent Office | 2019
Aerial vehicle propulsion mechanism with coaxially aligned and independently rotatable propellers
European Patent Office | 2019
|AERIAL VEHICLE PROPULSION MECHANISM WITH COAXIALLY ALIGNED AND INDEPENDENTLY ROTATABLE PROPELLERS
European Patent Office | 2017
|