An aircraft 100 comprising a fuselage 150, and a forward-swept wing 160 in shoulder-wing configuration with a center wing section 210 that is formed in an upper portion 157 of the fuselage 150 and that interconnects a portside wing section 161 and a starboard side wing section 164 of the forward-swept wing 160, wherein the portside wing section 161 comprises a portside longitudinal front spar 181 and a portside longitudinal rear spar 182, wherein the starboard side wing section 161 comprises a starboard side longitudinal front spar 181 and a starboard side longitudinal rear spar 182, and wherein the center wing section 210 comprises a center wing spar 190 that is attached to the portside longitudinal front spar 181, the portside longitudinal rear spar 182, the starboard side longitudinal front spar 181, and the starboard side longitudinal rear spar 182.
AN AIRCRAFT WITH A FORWARD-SWEPT WING IN SHOULDER-WING CONFIGURATION
FLUGZEUG MIT EINEM NACH VORNE GEPFEILTEN FLÜGEL IN SCHULTER-FLÜGELKONFIGURATION
AÉRONEF AYANT UNE AILE EN FLÈCHE AVANT EN CONFIGURATION D'AILE D'ÉPAULE
2024-06-05
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
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