The invention provides a fuselage section for an aircraft and the aircraft. In one aspect, a fuselage section for an aircraft is described, the fuselage section comprising: a pressure bulkhead comprising a dome-shaped structure and at least one coupling structure extending from an edge of the dome-shaped structure; and at least one circumferential structure arranged on the skin of the fuselage section, where the dome-shaped structure is secured to the circumferential structure via a distal portion of a coupling structure, where the distal portion is coupled to a foot portion of the circumferential structure, the coupling structure extending obliquely from the foot portion of the circumferential structure, such that the distance between the skin of the fuselage section and the coupling structure increases from the foot portion to the edge of the dome-shaped structure.
本发明提供了用于飞行器的机身区段和飞行器。在一个方面中,描述了一种用于飞行器的机身区段,该机身区段包括:压力隔板,该压力隔板包括圆顶形结构和至少一个联接结构,该至少一个联接结构从圆顶形结构的边缘延伸;以及至少一个周向结构,该至少一个周向结构布置在机身区段的蒙皮上,其中,圆顶形结构经由联接结构的远侧部分固定至周向结构,其中,所述远侧部分联接至周向结构的脚部分,联接结构从周向结构的脚部分倾斜地延伸,使得机身区段的蒙皮与联接结构之间的距离从脚部分到圆顶形结构的边缘增大。
Fuselage section for aircraft and aircraft
用于飞行器的机身区段和飞行器
2024-01-16
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
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