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A drone with a back-mounted solar panel

A technology for solar panels and unmanned aerial vehicles, applied in the field of unmanned aerial vehicles, can solve the problems of inability to increase the load, limited endurance of unmanned aerial vehicles, etc., and achieve the effect of good structural stability.

Active Publication Date: 2020-12-11
合肥凯石投资咨询有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] The purpose of the present invention is to provide a UAV with a back-mounted solar panel, which solves the problem of limited endurance and inability to increase the load of traditional UAVs.

Method used

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  • A drone with a back-mounted solar panel
  • A drone with a back-mounted solar panel
  • A drone with a back-mounted solar panel

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Embodiment Construction

[0019] The application will be described in further detail below in conjunction with the accompanying drawings. It is necessary to point out that the following specific embodiments are only used to further illustrate the application, and cannot be interpreted as limiting the protection scope of the application. The above application content makes some non-essential improvements and adjustments to this application.

[0020] combine Figure 1 to Figure 6 As shown, an unmanned aerial vehicle with a back-mounted solar panel includes an unmanned aerial vehicle fuselage 1, and the back end of the unmanned aerial vehicle fuselage 1 is provided with a storage slot 2, and the storage slot 2 is along the direction of the fuselage. set, and the rear end of the storage tank 2 is an open structure, the storage tank 2 is provided with a rotating bracket 3, a part of the rotating bracket 3 is stored in the storage tank 2, and the other part extends at the tail end of the drone body 1, the st...

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Abstract

The invention discloses an unmanned aerial vehicle (UAV) with a back-mounted solar panel, including the UAV fuselage, The rear end of the fuselage of the unmanned aerial vehicle is provided with a receiving groove, and the rear end of the receiving groove is of an opening structure, A rotary bracket is arranged in the receiving groove, A part of the rotating bracket is housed in the receiving groove, The other extends to the tail end of the UAV fuselage, a driving mechanism is arranged on the bottom of the receiving groove near the tail end, the driving mechanism is used for connecting the rotating bracket and driving the rotating bracket to rotate in a first plane, the first plane is a vertical plane parallel to the fuselage direction, and the second plane is a vertical plane perpendicular to the fuselage direction, and the rotating bracket is rotated in a second plane; Solar panels are attached to the rotating bracket. The invention has the advantages that the problem of limited endurance ability of the unmanned aerial vehicle and inability to increase the load are solved by the solar sail board of the unmanned aerial vehicle with back load type; and the solar sail board of the unmanned aerial vehicle has the advantages that the solar sail board of the unmanned aerial vehicle with back load type is adopted. At the same time, the rotating bracket and the driving mechanism havegood structural stability, and will not affect the flight of the UAV during the rotating process.

Description

technical field [0001] The invention relates to the technical field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle with a back-mounted solar panel. Background technique [0002] Solar-powered drones use sunlight to generate electricity to propel the motors that keep the aircraft in flight. Its advantage is that it can fly in the air for a long time without refueling. In a sense, it can replace satellites to perform long-term space missions, such as remote sensing, communication, etc., and the cost can be greatly reduced. However, due to the low conversion rate of solar energy and low battery energy, solar-powered aircraft have to be designed with huge wings and thin fuselages. At present, solar-powered aircraft that can successfully stay in the air for a long time are basically unable to increase the load, and have little use value. Contents of the invention [0003] The purpose of the present invention is to provide a UAV with a back-mounted so...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64D27/02
CPCB64D27/02B64D2211/00
Inventor 万可
Owner 合肥凯石投资咨询有限公司
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