A structural support assembly for a high-wing aircraft may include a plurality of columns extending through a passenger compartment of the aircraft having a pair of wings mounted proximate a top of a fuselage. A column upper end of at least one of the columns may be coupled to a center wing box structure adjacent to a rear spar thereof. A column lower end of at least one of the columns may be coupled to a floor substructure.
High-wing-aircraft fuselage support structure
2015-11-17
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
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