An aircraft defining a vertical direction, a longitudinal direction, and a transverse direction is provided. The aircraft includes: a fuselage; a propulsion system comprising a power source and a plurality of vertical thrust electric fans driven by the power source; and a wing extending from the fuselage in the transverse direction. The wing includes a support structure that comprises a plurality of first support members and a plurality of second support members. The plurality of first support members extending at least partially between the plurality of second support members. The plurality of vertical thrust electric fans arranged between the plurality of first support members and the plurality of second support members.
AERONAUTICAL PROPULSION SYSTEM HAVING ELECTRIC FANS
2025-01-16
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
HYBRID-ELECTRIC PROPULSION SYSTEM FOR AERONAUTICAL APPLICATIONS
European Patent Office | 2025
|Turbogenerator for hybrid electric aeronautical propulsion
European Patent Office | 2023
|TURBOGENERATOR FOR HYBRID ELECTRIC AERONAUTICAL PROPULSION
European Patent Office | 2022
|