The invention relates to an aircraft fuselage section 10 for an aircraft 40, comprising: a plurality of annular ribs 12 which are arranged one behind the other in the longitudinal direction X of the aircraft; two floor longitudinal supports (14a, 14b), which are arranged opposite one another in the transverse direction Y of the aircraft on the annular rib (12) and which laterally delimit the cabin floor (16); and a plurality of floor elements 18, which can be mechanically coupled to one another, are arranged between the two lateral floor longitudinal supports 14a, 14b and at least partially form a nacelle floor 16.
本发明涉及一种用于飞机40的飞机机身区段10,其具有:多个环形肋材12,所述环形肋材沿飞机纵向方向X相继设置;两个地板纵向承载件14a、14b,所述地板纵向承载件沿飞机横向方向Y彼此相对置地设置在环形肋材12处,并且所述地板纵向承载件对机舱底部16侧向地限界;和多个底部元件18,所述底部元件能够机械地彼此耦联,所述底部元件设置在两个侧向的地板纵向承载件14a、14b之间并且至少部分地形成机舱底部16。
Aircraft fuselage section for aircraft and aircraft with same
用于飞机的飞机机身区段和具有其的飞机
2024-01-09
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |
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