An airplane includes a wing mounted mid-level on a tubular fuselage. The wing includes carry-through that passes transversely through the fuselage and divides a cabin deck into fore and aft sections. At least one longitudinal passageway in the carry-through structure allows passenger/crew walk-throu
An airplane includes a wing mounted mid-level on a tubular fuselage. The wing includes carry-through that passes transversely through the fuselage and divides a cabin deck into fore and aft sections. At least one longitudinal passageway in the carry-through structure allows passenger/crew walk-through between the fore and aft sections of the deck.
대표청구항▼
1. An airplane, comprising: a fuselage including an upper deck having a floor, a mid level deck having a floor, and a lower level deck, wherein the mid level deck is located between the upper deck and the lower level deck;a wing mounted on the fuselage at the level of the mid level deck, the wing in
1. An airplane, comprising: a fuselage including an upper deck having a floor, a mid level deck having a floor, and a lower level deck, wherein the mid level deck is located between the upper deck and the lower level deck;a wing mounted on the fuselage at the level of the mid level deck, the wing including first and second wing panels respectively on opposite sides of the fuselage and a carry-through wing structure within the fuselage connecting the wing panels, the carry-through wing structure passing transversely through the fuselage and including an upper spar and a lower spar extending continuously across the fuselage and an upper spar extension connected to the upper spar and a lower spar extension connected to the lower spar, at least one substantially full passenger height passageway along the first deck through the carry-through wing structure, wherein the carry-through wing structure is positioned below the floor of the upper deck; andat least one engine mounted beneath each of the wing panels. 2. The airplane of claim 1, wherein: the passageway is pressurized,the carry-through structure further includes longitudinally extending ribs connecting the one or more spars, andthe passageway extends through the spars and between the ribs. 3. The airplane of claim 1, wherein: the upper deck is adapted to have seats for carrying passengers,the mid level deck has fore and aft sections adapted to have seats for carrying passengers, andthe carry-through structure includes a crew or passenger support facility. 4. The airplane of claim 3, wherein the support facility includes at least one of: a galley,a galley cart stowage facility,a lavatory,a crew rest facility,a passenger rest facility,a medical facility,a lounge,a bar,a play area, anda storage facility. 5. The airplane of claim 1, wherein the carry-through structure includes fuel storage. 6. The airplane of claim 1, further comprising: main landing gear mounted on the fuselage and having a majority portion thereof retractable entirely within the fuselage beneath the first deck, andwherein the main landing gear is mounted on the fuselage for swinging movement from a inboard retracted position to a deployed outboard position. 7. The airplane of claim 1, wherein the fuselage includes: a wheel well adapted for housing main landing gear, andthe lower level deck is a cargo deck beneath the mid level deck and capable of accommodating at least one of bulk cargo and a unit load device comprising at least one of an LD-3 container, an LD-1 container, an LD-2 container, an LD-3-46 container and an LD-3-45 container, the cargo deck including first and second cargo sections respectively fore and aft of the wheel well. 8. An airplane, comprising: a generally tubular fuselage including at least a first longitudinally extending payload carrying deck and a second longitudinally extending payload carrying deck stacked above the first deck; anda wing mounted on the fuselage, the wing passing transversely through the first deck and dividing the first deck into fore and aft sections, the wing including carry-through structure extending continuously transversely through the fuselage, the carry-through structure including an upper structural panel, a lower structural panel, at least one spar connected to both the upper structural panel and the lower structural panel, and a longitudinal passageway through the at least one spar and between the upper and lower structural panels allowing walk-through between the fore and aft sections of the first deck, the carry-through structure includes a first set of structural members connected between the upper and lower structural panels and extending transversely through the first deck, and a second set of structural members connected between the upper and lower structural panels and extending longitudinally through the first deck, wherein the structural members in the first set thereof include aligned openings defining the longitudinal passageway in the carry-through structure. 9. The airplane of claim 8, wherein the first deck and the passageway may be pressurized. 10. The airplane of claim 8, wherein: the fore and aft sections of the first deck each include passenger seating and at least one aisle, andthe passageway forms a substantially full passenger height corridor in the wing carry-through structure connecting the aisles in the fore and aft sections of the first deck. 11. The airplane of claim 8, wherein the cross section of the fuselage is a double lobe configuration. 12. The airplane of claim 8, wherein the fuselage includes: a double lobe frame forming a longitudinally extending outer recess in the fuselage,a composite skin covering the frame, including the recess. 13. The airplane of claim 8, further comprising: at least one utility disposed within a recess and extending longitudinally along the fuselage. 14. The airplane of claim 8, wherein: the first set of structural members are spars,the second set of structural members are ribs, andthe spars extend vertically beyond the upper and lower structural panels. 15. The airplane of claim 8, wherein a majority portion of the carry through structure is formed of composite materials. 16. A mid-wing, multi-deck airplane, comprising: a generally tubular fuselage including at least a lower cargo deck, a longitudinally extending mid-level passenger deck above the cargo deck, and a longitudinally extending upper passenger deck above the mid-level deck;a mid-level wing attached to the fuselage and passing through the mid-level deck, the wing including first and second wing panels respectively on opposite sides of the fuselage and a spar of a carry-though structure connecting the wing panels, the carry-through structure extending continuously transversely through the fuselage and dividing the mid-level deck into fore and aft sections, the carry-through structure including at least one longitudinally extending passageway through the spar forming a substantially full height walk-though aisle allowing a person to walk between the fore and aft sections;upper and lower structural panels vertically spaced from each other and extending transversely across the fuselage;a plurality of transversely extending spars connected between the upper and lower panels and extending transversely through the mid-level deck, the plurality of transversely extending spars extend vertically beyond the upper and lower structural panel;a plurality of rib members connected between the upper and lower structural panels and extending longitudinally through the mid-level deck;a least one engine mounted on each of the wing panels beneath the wing; andmain landing gear mounted on the fuselage and having a majority portion thereof retractable entirely within the fuselage beneath the mid-level passenger deck. 17. The airplane of claim 16, wherein: the passenger decks and the passageway may be pressured, andthe carry through structure includes at least one of: a galley,a galley cart stowage facility,a lavatory,a crew rest facility,a passenger rest facility,a medical facility,a lounge,a bar,a play area anda storage facility. 18. The airplane of claim 16, further comprising: first and second fuel tanks respectively within the first and second wing panels, each of the fuel tanks including an inboard portion extending into the carry-through structure. 19. The airplane of claim 16, wherein each of the engines is a large diameter high efficiency engine. 20. The airplane of claim 16 further comprising a spar extension connected to the spar of the carry-through structure.
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이 특허에 인용된 특허 (10)
Saint Jalmes,Bruno; Rezag,Andr��; Zaneboni,Jason, Aircraft fuselage and corresponding aircraft.
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