Rapidly assembled and disassembled drone undercarriage structure

Abstract

The invention discloses a rapidly assembled and disassembled drone undercarriage structure. The rapidly assembled and disassembled drone undercarriage structure is composed of a main undercarriage, afront undercarriage, a first quick release pin and a second quick release pin; a drone body connector is fixedly connected with a drone body, and a main undercarriage connector is fixed at the upper end of the main undercarriage; a front undercarriage-drone body support column is connected with the drone body, one end of a front undercarriage support rod is connected with the front undercarriage,and the other end of the front undercarriage support rod is embedded inside the front carriage-drone body support column and connected through a quick release pin. When a drone is expanded, a main undercarriage connector is inserted into the lug of the drone connector and connected with the drone body connector through a quick release pin; after the front undercarriage support rod is inserted intothe front undercarriage-drone body support column. When the drone is withdrawn, the first quick release pin and the second quick release pin are pulled up to achieve separation of the front undercarriage and the main undercarriage from the drone body. The rapidly assembled and disassembled drone undercarriage structure is convenient to assemble and disassemble, and by designing modular parts, achieves simple operation and greatly reduces the time for flight preparation and withdrawal.

Description

technical field [0001] The invention relates to the technical field of unmanned aerial vehicles, in particular to a quick disassembly and assembly landing gear structure of an unmanned aerial vehicle. Background technique [0002] UAVs have the advantages of small size, low cost, strong environmental adaptability, flexible use, and high operating efficiency. Especially when performing boring and long-term tasks, UAVs have incomparable advantages over manned machines. In addition to being used in the military field, UAV systems are also used in civilian fields such as forest protection, power line inspection, environmental monitoring, communication relay, and logistics. [0003] Among the many take-off and landing methods of UAVs, the wheeled take-off and landing form has the characteristics of high safety, convenient use, and low maintenance costs, so it is widely used in most UAV systems. However, for some small UAV flight platforms, the landing gear is mostly fixed, and ...

AI Technical Summary

Problems solved by technology

The landing gear system adopts the fixed connection method, the disassembly process is complicated and the disassembly time is long

At the same time, during the deployment process, the landing gear system with bolt connection is used, the installation process is more cumbersome and the installation time is long

Greatly affects the deployment time of the entire system, and the maintenance preparation period is longer

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