Vertical tail flipping device

Abstract

This utility model belongs to the field of aircraft component assembly technology and discloses a vertical tail tilting device, including a support base, a mounting bracket, a connecting component, and a tilting structure. The tilting structure includes a position adjustment component, a tilting auxiliary component, and a drive component. The position adjustment component can move along the length direction of the support base under the action of the drive component, and the second mounting part is tilted relative to the support base by means of mechanical transmission, thus completing the vertical tail tilting process. The tilting process is achieved through the combined mechanical transmission effects of the drive component, the position adjustment component, the tilting auxiliary component, the second mounting part, and the support base. It can achieve the tilting operation of the vertical tail without relying on large hoisting equipment or a large amount of manual labor, which significantly reduces the labor cost required for the tilting process and improves the operational safety of the entire tilting process. Furthermore, the mounting bracket can constrain the vertical tail in different directions under the action of the connecting component, and the connection stability and connection strength between the vertical tail and the vertical tail tilting device are high.

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