High-wing-aircraft fuselage support structure
AssigneeThe Boeing Company
InventorsStephen T. Brown, Sergey Barmichev
Life of this patent
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Abstract
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.
Claims20
A structural support assembly for a fuselage of a high-wing aircraft, comprising:
- a plurality of columns extending through a passenger compartment of an aircraft having a pair of wings mounted proximate a top of a fuselage;
- a column upper end of at least one of the columns being coupled to a center wing box structure proximate a rear spar thereof;
- and
- a column lower end of at least one of the columns being coupled to a floor substructure of the fuselage.
A structural support assembly for a fuselage of a high-wing aircraft, comprising:
- a pair of columns extending substantially vertically through a passenger compartment of an aircraft having a pair of wings mounted proximate a top of a fuselage;
- a column upper end of at least one of the columns being coupled to a center wing box structure adjacent to a rear spar thereof and proximate a vertical center of gravity of the wings;
- a column lower end of at least one of the columns being coupled to a wheel well forward bulkhead;
- and
- at least one of the columns being positioned adjacent to a passenger seat.
A method of supporting a wing of a high-wing aircraft, comprising:
- providing a fuselage having a wing mounted proximate a top of the fuselage and a main landing gear mounted to the fuselage;
- and
- extending a plurality of columns substantially vertically through an aircraft passenger compartment;
- coupling a column upper end of the plurality of columns to a center wing box structure proximate a rear spar thereof;
- coupling a column lower end of the plurality of columns to a floor substructure of the fuselage;
- and
- transmitting a wing downward load through the plurality of columns and the floor substructure and into the main landing gear.
Dependencies are inferred from the claim text.