Integrated stabilizing mechanism for landing supporting legs of objective table of object-carrying unmanned aerial vehicle

Abstract

The invention discloses an integrated stabilizing mechanism for landing supporting legs of an objective table of an object-carrying unmanned aerial vehicle. The integrated stabilizing mechanism includes a landing gear, the undercarriage comprises a wind power balance body, supporting legs and wind power adjusting bodies. The upper ends of the supporting legs are fixed through the lower end of thewind power balance body. The number of the supporting legs is four. The number of the wind power adjusting main bodies is four. The wind power adjusting bodies are fixedly installed through supportinglegs. The wind power balance body comprises stop blocks, a supporting column, heavy blocks, a connecting rod, a wind shield, a fixing base and a rotating frame. A pair of stop blocks is arranged, aninserting rod is fixedly connected to the center of the rear end of each stop block, the inserting rods are inserted into the inner wall of the rotating frame in a sliding mode, the lower end of the supporting column is fixedly connected to the upper end of the fixing base, the upper end of the supporting column is fixedly connected through a target unmanned aerial vehicle, and the heavy blocks are fixedly connected through the front ends of the inserting rods. The landing stability can be improved, and the use requirement can be better met.

Description

technical field [0001] The invention relates to the technical field of landing gear equipment, in particular to an integrated stabilization mechanism for landing and landing legs of a load-carrying unmanned aerial vehicle. Background technique [0002] Common landing gear for UAVs is usually a bracket with a simple structure, which has the advantages of simple structure and low mass. However, when it is used to transport large pieces of goods, the goods will flutter with the wind after being affected by the wind. Dragging the cargo in the opposite direction will cause the cargo and landing plus an inclined landing, which will easily make the UAV easy to dump after landing. Therefore, a device that can alleviate the above problems is urgently needed. Contents of the invention [0003] The purpose of the present invention is to provide an integrated stabilization mechanism for the lifting and landing legs of the loading UAV stage, so as to solve the problems raised in the ab...

AI Technical Summary

Problems solved by technology

[0002] Common landing gear for UAVs is usually a bracket with a simple structure, which has the advantages of simple structure and low mass. However, when it is used to transport large pieces of goods, the goods will flutter with the wind after being affected by the wind. Dragging the cargo in the opposite direction will cause the cargo and landing plus inclined landing, which will easily make the UAV easy to dump after landing, so a device that can alleviate the above problems is urgently needed

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