The task equipment hoisting structure comprises a front beam assembly, a rear beam assembly, a middle beam assembly, an oblique beam, a front skin assembly, a first middle skin assembly, a second middle skin assembly, a rear skin assembly and a limiting connector assembly. Wherein the front beam assembly and the rear beam assembly are connected through an oblique beam, and the middle beam assembly is arranged below the oblique beam to jointly form a hoisting beam assembly; the first middle skin assembly and the second middle skin assembly are fixed to the two sides of the hoisting beam assembly, the front skin assembly and the rear skin assembly are fixed to the two ends of the hoisting beam assembly and jointly define a ship-shaped skin area, one ends of the limiting connector assemblies are fixedly connected with the front beam assembly and the rear beam assembly respectively, and the other ends of the limiting connector assemblies are fixedly connected with the hoisting beam assembly. The other ends of the pair of limiting connector assemblies extend out of the skin area. And different task modes can be rapidly switched by rapidly replacing different middle beam assemblies and limiting connector assemblies.
本发明公开了一种任务设备吊装结构,包括前梁组件、后梁组件、中梁组件、斜梁、前部蒙皮组件、中部第一蒙皮组件、中部第二蒙皮组件、后部蒙皮组件、限位接头组件;其中,前梁组件与后梁组件之间通过斜梁连接,中梁组件布置在斜梁下方,共同构成吊装梁组件;中部第一蒙皮组件以及中部第二蒙皮组件固定于吊装梁组件两侧,前部蒙皮组件以及后部蒙皮组件固定于吊装梁组件两端,共同围成船型的蒙皮区域,限位接头组件布置一对,一对限位接头组件的一端分别与前梁组件、后梁组件固定连接,一对限位接头组件的另一端伸出至所述蒙皮区域的外部;通过快速更换不同的中梁组件和限位接头组件实现不同任务模式的快速切换。
Task equipment hoisting structure
一种任务设备吊装结构
26.04.2024
Patent
Elektronische Ressource
Chinesisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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