The invention relates to a movable cradle system for an aircraft element, such as an aircraft engine or the like, and to a method for implementing such a system, said system being characterized in that it comprises: a first movable module (10) and a second movable module (20), each movable module comprising: a frame (12, 22) equipped with at least three wheels; lifting means adapted to be able to move the aircraft element at least in a vertical direction; at least one connecting arm (16, 17) adapted to be able to secure the frame of the first module and the frame of the second module together and to allow data to be transmitted between the first module and the second module; and wherein: the movable modules are adapted to be able to be controlled in a mutually coordinated manner.
本发明涉及一种用于飞行器元件的可移动托架系统以及用于实现该系统的方法,该飞行器元件诸如为飞机发动机等,所述系统的特征在于该系统包括:第一可移动模块(10)和第二可移动模块(20),每个可移动模块包括:框架(12、22),其配备有至少三个轮;升降装置,其适于能够至少沿竖直方向移动所述飞行器元件;至少一个连接臂(16、17),其适于能够将所述第一模块的框架和所述第二模块的框架固定在一起,并且允许在第一模块第二模块之间传输数据;并且其中:所述可移动模块适于能够以相互协调的方式被控制。
Movable carriage system and method for implementing movable carriage system
可移动托架系统和用于实现可移动托架系统的方法
2022-09-13
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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