A shell arrangement for a fuselage of an aircraft includes a first shell portion extending in a curved manner in a shell peripheral direction and a second shell portion extending in a curved manner inthe shell peripheral direction, wherein, in an overlapping portion of the shell arrangement, a first end region of the first shell portion and a second end region of the second shell portion overlapeach other in the shell peripheral direction and a first outer face of the first shell portion and a second inner face of the second shell portion are adhesively bonded to each other by an adhesive layer, and wherein an edge of the first shell portion which terminates the first end region with respect to the shell peripheral direction extends in the overlapping portion in an undulating manner in ashell longitudinal direction which extends transversely relative to the shell peripheral direction.
本发明提供一种用于飞行器的机身的壳层组件,包括沿壳层圆周方向弯曲地延伸的第一壳层部件和沿所述壳层圆周方向弯曲地延伸的第二壳层部件,其中在所述壳层组件的重叠区段中,所述第一壳层部件的第一端部区域和所述第二壳层部件的第二端部区域以沿壳层圆周方向彼此重叠的方式布置,并且所述第一壳层部件的第一外表面和所述第二壳层部件的第二内表面是借助于粘合剂层互相粘合的,并且其中所述第一壳层部件的相对于所述壳层圆周方向终止所述第一端部区域的边缘在所述重叠区段中沿横向于所述壳层圆周方向延伸的壳层纵向方向波形地延伸。
Shell arrangement for fuselage of aircraft and fuselage for aircraft
用于飞行器的机身的壳层组件和用于飞行器的机身
2020-11-24
Patent
Electronic Resource
Chinese
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