The invention relates to the technical field of aircraft maintenance ladder assemblies, in particular to an adjusting system for an aircraft ladder assembly, a base assembly and a lifting assembly, the lifting assembly is located above the base assembly, the base assembly comprises two base bodies, and the lifting assembly comprises two lifting plates; the two base bodies and the two lifting plates are connected in a crossed mode, and rotating shafts are arranged between the base bodies and the lifting plates and used for rotation between the base bodies and the lifting plates. The base assembly, the lifting assembly and the like are arranged, base bodies and lifting plates in the base assembly and the lifting assembly are rotationally connected, and when the undercarriages are overhauled, due to the fact that the undercarriages are different in size, in order to avoid pulleys of the undercarriages, the functions of hydraulic rods in a management system can be utilized, and the undercarriages can be overhauled conveniently. And the base main body and the lifting plate are rotated to an available angle in a crossed manner, and then are pushed to the overhauling position of the undercarriage for overhauling, so that the overall universality of the ladder assembly is realized.
本发明涉及飞机维修梯架技术领域,具体的说是一种用于飞机梯架的调节系统,基座组件和升降组件,所述升降组件位于基座组件的上方,所述基座组件包括两基座主体,所述升降组件包括两升降板;两组所述基座主体和升降板之间交叉连接,所述基座主体和升降板之间设置有转动轴,供基座主体和升降板之间转动;通过设置有基座组件以及升降组件等,其中基座组件和升降组件中的基座主体和升降板之间为转动连接,在对起落架进行检修时,由于起落架的大小各异,且为了避开起落架的滑轮,可以利用管理系统中的液压杆功能,将基座主体和升降板进行交叉转动至可用角度,再推入到起落架的检修位置处进行检修,实现梯架整体的普适性。
Adjusting system for aircraft ladder assembly
一种用于飞机梯架的调节系统
2023-10-13
Patent
Electronic Resource
Chinese
IPC: | B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen |
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