An aircraft has a fuselage, an engine disposed within the fuselage, a rotatable wing disposed above the fuselage and selectively rotatable about a wing rotation axis, and a plurality of interconnect driveshafts disposed within the rotatable wing, and at least one drive system component that is connected between the engine and the interconnect driveshaft is disposed along the wing rotation axis.
Fuselage Mounted Engine with Wing Stow
22.03.2018
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
AIRCRAFT WITH A FUSELAGE-MOUNTED ENGINE AND WING STOW
Europäisches Patentamt | 2018
|Stowable wing aircraft with dual, fuselage-mounted engines
Europäisches Patentamt | 2023
|STOWABLE WING AIRCRAFT WITH DUAL, FUSELAGE-MOUNTED ENGINES
Europäisches Patentamt | 2019
|STOWABLE WING AIRCRAFT WITH DUAL, FUSELAGE-MOUNTED ENGINES
Europäisches Patentamt | 2022
|