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    • 4. 发明授权
    • Aircraft fuselage and corresponding aircraft
    • 飞机机身和相应的飞机
    • US07395989B2
    • 2008-07-08
    • US11311548
    • 2005-12-20
    • Bruno Saint-JalmesAndré RezagJason Zaneboni
    • Bruno Saint-JalmesAndré RezagJason Zaneboni
    • B64C1/20
    • B64D11/00B64C2001/0036
    • 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.
    • 飞机机身包括外皮和至少一个主甲板,其将飞机机身的内部空间纵向分成第一空间和第二空间。 第一空间的至少一部分被分成至少三个纵向区域,并且至少三个纵向区域包括至少一个中心区域和至少两个侧向区域。 至少一个中央区域分为三个部分,三个部分包括前部扇区,中央扇区和后部扇区。 所述至少两个横向区域包括第一和第二横向区域构造,所述前部区段包括第一和第二前部扇形结构,所述中央扇区包括第一和第二中央扇形结构,并且所述后部扇区包括第一和第二后部扇区 组态。