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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 a drone with a back-mounted solar panel, which includes a drone body. A storage slot is provided at the rear end of the back of the drone body, and the rear end of the storage slot is an open structure. A rotating bracket is provided in the storage slot. Part of the rotating bracket is stored in the storage slot, and the other part extends to the tail end of the drone fuselage. A driving mechanism is provided on the bottom of the storage slot near the tail end. The driving mechanism is used for Connect the rotating bracket and drive the rotating bracket to rotate in the first plane and the second plane. The first plane is a vertical plane parallel to the direction of the fuselage, and the second plane is a vertical plane perpendicular to the direction of the fuselage; on the rotating bracket There are solar panels attached. The advantage of the present invention is that the back-loaded UAV solar panel solves the problem that the UAV has limited endurance and cannot increase the load; at the same time, the rotating bracket and driving mechanism used have good structural stability and can , will not affect the flight of the drone.

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
CPCB64D27/02B64D27/353
Inventor 万可
Owner 合肥凯石投资咨询有限公司
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