[특허]Aircraft fuselage and corresponding aircraft

Airbus

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특허 상세정보

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Aircraft fuselage and corresponding aircraft

특허상세정보
국가/구분	United States(US) Patent 등록
국제특허분류(IPC7판)	B64C-001/20 B64C-001/00
미국특허분류(USC)	244/118.1; 244/118.5; 244/118.6; 244/119
출원번호	US-0311548 (2005-12-20)
등록번호	US-7395989 (2008-07-08)
우선권정보	FR-04 13547(2004-12-20)
발명자 / 주소	Saint Jalmes,Bruno Rezag,Andr�� Zaneboni,Jason
출원인 / 주소	Airbus
대리인 / 주소	Oblon, Spivak, McClelland, Maier & Neustadt, P.C.
인용정보	피인용 횟수 : 9 인용 특허 : 14

초록
▼

An aircraft fuselage includes an outer skin and at least one main deck separating an interior space of the aircraft fuselage longitudinally into a first space and a second space. At least one portion of the first space is divided into at least three longitudinal zones, and the at least three longitudinal zones include at least one central zone and at least two lateral zones. The at least one central zone is divided into three sectors, and the three sectors include a front sector, a central sector, and a rear sector. The at least two lateral zones include a first and second lateral zone configuration, the front sector includes a first and second front sector configuration, the central sector includes a first and second central sector configuration, and the rear sector includes a first and second rear sector configuration.

대표
청구항
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The invention claimed is: 1. An aircraft fuselage, comprising: an outer skin; and a single continuous main deck separating an interior space of the aircraft fuselage longitudinally into a first space above said single continuous main deck and a second space below said single continuous main deck, wherein at least one portion of the first space is divided into at least three longitudinal zones by a plurality of substantially vertical walls, said at least three longitudinal zones including at least one central zone and at least two lateral zones, wherein the at least one central zone is divided into three sectors, said three sectors including a front sector, a central sector, and a rear sector, wherein the at least two lateral zones include a first plurality of seats attached, either directly or indirectly, to the at least one main deck in a first lateral zone configuration, and are free of said plurality of seats in a second lateral zone configuration, wherein said front sector and said rear sector of the at least one central zone is configured to hold only freight, wherein freight does not include passengers, and wherein said central sector of the at least one central zone includes a second plurality of seats attached, either directly or indirectly, to the at least one main deck in a first central sector configuration, and is free of said second plurality of seats in a second central sector configuration. 2. An aircraft fuselage according to claim 1, wherein said central sector is in said first central sector configuration. 3. An aircraft fuselage according to claim 1, wherein aisles are provided in the at least one central zone that connect to the at least two lateral zones. 4. An aircraft fuselage according to claim 1, further comprising at least one plateau on which several seats configured to hold passengers are attached, the plateau including attachment equipment configured to attach the plateau to the main deck. 5. An aircraft fuselage according to claim 1, wherein said outer skin is lined with an inner skin. 6. An aircraft fuselage according to claim 5, further comprising longitudinal ribs configured to connect the upper portion of the inner skin to the lower portion thereof. 7. An aircraft fuselage according to claim 6, wherein the longitudinal ribs comprise connecting rods. 8. An aircraft fuselage according to claim 1, wherein the first space above the at least one main deck is an occupancy space configured to accommodate passengers, freight, or any combination thereof, and the second space below the main deck is a hold configured to accommodate at least containers under the designation LD-1, LD-3, and LD-8. 9. An aircraft fuselage according to claim 1, wherein the first space above the at least one main deck is a first occupancy space configured to accommodate passengers, freight, or any combination thereof, and the second space below the main deck is a second occupancy space configured to accommodate passengers, freight, or any combination thereof. 10. An aircraft, comprising a fuselage according to claim 1. 11. An aircraft fuselage according to claim 1, further comprising at least one access aisle traversing at least one of the at least two lateral zones, wherein the at least one access aisle extends substantially crosswise in relation to a longitudinal axis of said fuselage, and wherein the at least one access aisle is at least large enough to accommodate the passage of a pallet including freight. 12. An aircraft fuselage according to claim 11, further comprising at least one door located on a lateral wall of said fuselage that connects to the at least one access aisle. 13. An aircraft fuselage according to claim 1, wherein said at least two lateral zones are in said first lateral configuration and said central sector is in said first central sector configuration. 14. An aircraft fuselage according to claim 1, wherein said at least two lateral zones are in said second lateral configuration and said central sector is in said second central sector configuration. 15. An aircraft fuselage according to claim 1, wherein said at least two lateral zones are in said first lateral configuration and said central sector is in said second central sector configuration. 16. An aircraft fuselage according to claim 1, wherein said at least two lateral zones are further divided to include at least one first lateral zone in said first lateral zone configuration and at least one second lateral zone in said second lateral zone configuration. 17. An aircraft fuselage according to claim 1, wherein the second space below the main deck includes three longitudinal zones, each being configured to accommodate at least containers under the designation LD-1, LD-3, and LD-8. 18. An aircraft fuselage according to claim 1, wherein at least one of said three sectors of said at least one central zone is configured to accommodate at least containers under the designation LD-1, LD-3, and LD-8. 19. An aircraft fuselage according to claim 18, wherein said front and rear sectors are configured to accommodate at least containers under the designation LD-1, LD-3, and LD-8. 20. An aircraft fuselage according to claim 19, wherein said at least two lateral zones are in said first lateral configuration and said central sector is in said first central sector configuration. 21. An aircraft fuselage, comprising: an outer skin; and a single continuous main deck separating an interior space of the aircraft fuselage longitudinally into a first space above said single continuous main deck and a second space below said single continuous main deck, wherein at least one portion of the first space is divided into at least three longitudinal zones by a plurality of walls, said at least three longitudinal zones including at least one central zone and at least two lateral zones, wherein the at least one central zone is divided into three sectors, said three sectors including a front sector, a central sector, and a rear sector, wherein the at least two lateral zones and the central zone include a plurality of seats attached, either directly or indirectly, to the at least one main deck, wherein the front sector and the rear sector include a plurality of pallets attached, either directly or indirectly, to the single continuous main deck, and wherein said plurality of pallets are configured to secure only freight, wherein freight does not include seats configured to hold passengers. 22. An aircraft fuselage according to claim 21, wherein the plurality of pallets are configured to accommodate at least containers under the designation LD-1, LD-3, and LD-8. 23. An aircraft fuselage according to claim 1, wherein said single continuous main deck extends below each of said at least three longitudinal zones. 24. An aircraft fuselage according to claim 5, wherein said plurality of walls that divide said first space into said at least three longitudinal zones cover a plurality of ribs that extend from an upper portion of said inner skin located in said first space to a lower portion of said inner skin in said second space. 25. An aircraft fuselage according to claim 1, wherein said fuselage is a single tubular fuselage that includes an oval cross-section, and wherein said single continuous main deck extends from a first lateral side wall of said fuselage to a second lateral sidewall of said fuselage located on an opposite side of said fuselage. 26. An aircraft fuselage according to claim 21, wherein said single continuous main deck extends below each of said at least three longitudinal zones. 27. An aircraft fuselage according to claim 21, wherein said outer skin is lined with an inner skin, and wherein said plurality of walls that divide said first space into said at least three longitudinal zones cover a plurality of ribs that extend from an upper portion of said inner skin located in said first space to a lower portion of said inner skin in said second space.

이 특허에 인용된 특허 (14)

이 특허를 인용한 특허 피인용횟수: 9

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특허 상세정보

Aircraft fuselage and corresponding aircraft

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이 특허에 인용된 특허 (14)

이 특허를 인용한 특허 피인용횟수: 9

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Aircraft fuselage and corresponding aircraft

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이 특허에 인용된 특허 (14)

이 특허를 인용한 특허 피인용횟수: 9

IPC 상위 출원인

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IPC 상세정보(version : 201201)

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