Unmanned aerial vehicle pod structure

Abstract

The invention discloses an unmanned aerial vehicle pod structure, and belongs to the technical field of unmanned aerial vehicles. Loads of the unmanned aerial vehicle and the electronic equipment can be decoupled in a physical structure, and the antennae are symmetrically arranged on the left side and the right side in the pod and can be independently hung on the belly. According to the structure, the safety distance between the knife-shaped antenna at the bottom of the pod and the ground is increased, and the independence and interchangeability of the pod are greatly improved.

Description

technical field [0001] The invention relates to the technical field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle pod structure. Background technique [0002] The pod refers to a streamlined nacelle that is installed with on-board equipment, electronic equipment or weapons, and hung on the belly or under the wings. The UAV electronic pod can decouple the UAV and electronic equipment loads in terms of physical structure, realize optional or optional equipment, and greatly improve the flexibility of UAV loads. [0003] Existing large-scale UAV pods need to be mounted on the aircraft through the mounting device hanger. This type of structure often has the characteristics of large mass and large vertical size. Large-scale UAV pods are mainly multi-metal structures, which cannot meet the special requirements for installing antennas in the cabin. The load of electronic equipment often needs to mount the pod on the belly of the aircraft in order to redu...

AI Technical Summary

Problems solved by technology

Or install the electronic equipment load in a streamlined radome that conforms to the belly of the aircraft. This method is difficult to install due to the processing error of the aircraft skin, the assembly gap is large, and it is difficult to maintain and debug.

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