Modular quickly-spliced unmanned aerial vehicle

Abstract

The invention relates to a modular quickly-spliced unmanned aerial vehicle. The unmanned aerial vehicle comprises a left wing module, a hatch module, a vertical module, a body module, a parachute cabin module and a right wing module which are connected with one another through uniformly distributed latch devices, wherein each latch device consists of a latch seat and a locking column; and the latch devices are fixedly arranged on interconnected module materials respectively, and one latch device is a locking latch device. The main constituent parts of the unmanned aerial vehicle are subjectedto modular manufacturing, so that smallest volume can be realized for packaging, vehicle-mounted space is increased, and transportation is facilitated; meanwhile, the modular parts are subjected to standardized manufacturing, so that easily damaged parts can be quickly supplemented, installed and used, can be quickly assembled and disassembled and accurately matched when a task is executed, and can be applied to the task immediately, and work efficiency is improved. The unmanned aerial vehicle has a simple integral structure and a scientific and reasonable design, perfectly solves a large number of problems of the conventional unmanned aerial vehicle, and lays a foundation for the development and utilization of the unmanned aerial vehicle.

Description

technical field [0001] The invention belongs to the field of aviation and relates to an unmanned aerial vehicle, in particular to a modular fast splicing unmanned aerial vehicle. Background technique [0002] my country's small UAV industry started relatively late. In terms of shape, size and equipment, the design process generally refers to the design of foreign UAVs in active service. The fuselage and wing parts are still connected in a fixed way. There are major deficiencies in production and other aspects, which are specifically reflected in: 1. It cannot be quickly assembled and disassembled when performing tasks, and it cannot be put into the task again immediately; 2. The drone is large in size, which makes it difficult to mount, install, and transport; 3. When a part of the UAV is damaged, it cannot be replaced in time and quickly, and it cannot be effectively paired during maintenance, so it can only be repaired. [0003] In recent years, new technologies and new mat...

AI Technical Summary

Problems solved by technology

[0002] my country's small UAV industry started relatively late. In terms of shape, size and equipment, the design process generally refers to the design of foreign UAVs in active service. The fuselage and wing parts are still connected in a fixed way. There are major deficiencies in production and other aspects, which are specifically reflected in: 1. It cannot be quickly assembled and disassembled when performing tasks, and it cannot be put into the task again immediately; 2. The drone is large in size, which makes it difficult to mount, install, and transport; 3. When a part of the UAV is damaged, it cannot be replaced in time and quickly, and it cannot be effectively paired during maintenance, so it can only be repaired

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