This invention discloses an adaptive balancing lifting device for aircraft door
assembly and disassembly, belonging to the field of lifting device technology. It includes a lifting frame, lifting components, and a clamping
assembly. The clamping
assembly is equipped with a flexible component containing magnetofluid and a corresponding excitation component, which can adapt to the curved surface of the door and actively harden to provide reliable clamping. The lifting device also integrates a multi-degree-of-freedom angle adjustment component and a vision-feedback-based active balancing
system. Before handling, the clamping angle can be adjusted to align the door using the longitudinal and lateral adjustment components. During handling, a vision camera detects the door's attitude in real time, and the
control system drives independent lifting components on both sides for dynamic leveling. Micro-vibrations are absorbed by adjusting the magnetofluid state, achieving adaptive flexible gripping, precise attitude adjustment, and stable anti-sway handling of irregular
doors, significantly improving the safety, accuracy, and efficiency of assembly and disassembly operations.