Disclosed herein is a vertical take-off and landing (VTOL) aircraft. The vertical take-off and landing aircraft includes a single wing, a plurality of engines, a first set of propellers on a first side of the single wing, a second set of propellers on a second side of the single wing, a first power transfer unit, a second power transfer unit, landing gears connected to the single wing, and a fuselage with a capacity of 100 passengers connected to the single wing. The plurality of engines includes a first engine mounted to the first side of the single wing and a second engine mounted to the second side of the single wing.
VTOL aircraft with tiltable propellers
2019-09-17
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
ELECTRIC VTOL AIRCRAFT WITH TILTING PROPELLERS AND LIFTING PROPELLERS
European Patent Office | 2024
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