The present lift generating fuselage (1) for aircraft mainly comprises of: a novel aerofoil shaped fuselage (1A); or a novel aerofoil shaped fuselage body (2); and integral webs (3); or a novel aerofoil shaped fuselage body (2); integral webs (3) and overhead central wing (4).
LIFT GENERATING FUSELAGE FOR AIRCRAFT
21.06.2018
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
Novel heavy-load aircraft with stub-wing lift fuselage
Europäisches Patentamt | 2024
|Aircraft fuselage section, aircraft fuselage and aircraft
Europäisches Patentamt | 2023
|