The present invention provides a modular fuselage assemblies for aircraft, an aircraft including modular fuselage assemblies, and methods of assembling modular fuselage assemblies. The modular fuselage assembly includes a plurality of fuselage lobes that may extend along a longitudinal axis of the modular fuselage assembly. Each fuselage lobe includes a plurality of frame members and a lobe skin that is operatively attached to the plurality of frame members and defines an external surface of the fuselage lobe. The modular fuselage assembly also includes a plurality of longerons extending alonga longitudinal axis of the modular fuselage assembly. At least two fuselage lobes are operatively attached to each longeron and the plurality of fuselage lobes and the plurality of longerons at leastpartially bound a cargo hold defined within the modular fuselage assembly. The methods include methods of assembling the modular fuselage assemblies.
本发明的名称为模块化机身组件、包括其的飞机及其装配方法。用于飞机的模块化机身组件、包括模块化机身组件的飞机以及装配模块化机身组件的方法。模块化机身组件包括可沿模块化机身组件的纵轴延伸的多个机身凸角。每个机身凸角包括多个框架构件和凸角蒙皮,该凸角蒙皮可操作地连接至多个框架构件并且限定机身凸角的外表面。模块化机身组件还包括沿模块化机身组件的纵轴延伸的多个纵梁。至少两个机身凸角可操作地连接至每个纵梁,并且多个机身凸角和多个纵梁至少部分地界定在模块化机身组件内限定的货舱。方法包括装配模块化机身组件的方法。
MODULAR FUSELAGE ASSEMBLIES FOR AIRCRAFT, AIRCRAFT INCLUDING MODULAR FUSELAGE ASSEMBLIES, AND METHODS OF ASSEMBLING MODULAR FUSELAGE ASSEMBLIES
模块化机身组件、包括其的飞机及其装配方法
2021-01-19
Patent
Elektronische Ressource
Chinesisch
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