Drone solar power generation device

Abstract

A solar power generation device for unmanned aerial vehicles (UAVs) is disclosed, designed for connection to a pre-installed UAV. The UAV has a connecting portion on its top surface. The device includes a power generation module. The power generation module comprises a first solar panel and a docking portion, the docking portion being located on the bottom surface of the first solar panel and connected to the connecting portion. The power generation module further includes a plurality of second solar panels, which are connected to the first solar panels via adapters and open / close relative to the first solar panels. Thus, the docking portion and the connecting portion are combined to mount the power generation module on the top surface of the UAV, generating electricity from the first solar panel. The second solar panels open / close to increase the light-receiving area during deployment, thereby achieving the structure of a solar power generation device for UAVs.

Claims

1. A solar power generation device for unmanned aerial vehicles (UAVs), for connection to a pre-set UAV, the top surface of which is provided with a connecting part, the solar power generation device for UAVs including at least one power generation module, wherein: The power generation module includes a first solar panel and a docking part. The docking part is located on the bottom surface of the first solar panel and is connected to the connecting part. Thus, after the docking part and the connecting part are combined, the power generation module is installed on the top surface of the drone and generates electricity through the first solar panel, thereby achieving the structure of a drone solar power generation device.

2. The drone solar power generation device as described in claim 1, wherein the power generation module is further provided with a plurality of second solar panels, each of the second solar panels being connected to the first solar panel via an adapter, so that the second solar panels can be opened and closed relative to the first solar panel, thereby increasing the light-receiving area when deployed.

3. The UAV solar power generation device as described in claim 2, wherein the adapter is a hinge.

4. The UAV solar power generation device as described in claim 2, wherein the adapter is a linkage element, and the linkage element is a four-bar linkage or a parallelogram linkage.

5. The UAV solar power generation device as described in claim 2, wherein the first solar panel and the second solar panel are monocrystalline silicon solar panels, polycrystalline silicon solar panels, or thin-film solar panels.

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