CN210882586U

CN210882586U - Solar unmanned aerial vehicle wing

Info

Publication number: CN210882586U
Application number: CN201922059969.7U
Authority: CN
Inventors: 王强; 毛晓杰; 胡能浩
Original assignee: Chengdu Aeronautic Polytechnic
Current assignee: Chengdu Aeronautic Polytechnic
Priority date: 2019-11-26
Filing date: 2019-11-26
Publication date: 2020-06-30
Anticipated expiration: 2029-11-26

Abstract

The utility model belongs to the technical field of unmanned aerial vehicles, in particular to a solar unmanned aerial vehicle wing, which comprises a wing, wherein the surface of the wing is fixedly connected with a bottom metal, a solar energy conduction device is arranged on the bottom metal, a solar energy absorption plate is fixedly connected with the surface of the bottom metal, and a solar energy conversion device is arranged on the bottom metal; the utility model discloses, through setting up solar energy absorption board, can realize the absorption to solar energy, through setting up solar energy conduction device, can improve conduction efficiency, reinforcing energy utilization ratio, the device adopts solar energy absorption board, bottom metal, solar energy conversion device and electric wire, can the variable energy increase on the original basis of unmanned aerial vehicle, promote unmanned aerial vehicle's air continuation ability, alleviate the proportion of the shared unmanned aerial vehicle weight of the energy, make unmanned aerial vehicle increase more functions, whole device is rational in infrastructure, high durability and convenient use, therefore, the clothes hanger is strong in practicability.

Description

Solar unmanned aerial vehicle wing

Technical Field

The utility model belongs to the technical field of unmanned aerial vehicle, concretely relates to solar energy unmanned aerial vehicle wing.

Background

At present unmanned aerial vehicle all is not from taking energy regenerating unit, uses unmanned aerial vehicle must carry out the energy supply, and this duration that has reduced unmanned aerial vehicle, this has weakened unmanned aerial vehicle's function, will use to unmanned aerial vehicle and just need the additional energy, and the energy is then more and more expensive, and unmanned aerial vehicle's use cost is just higher and higher, very big increase use cost, reduced the availability factor.

SUMMERY OF THE UTILITY MODEL

To solve the problems set forth in the background art described above. The utility model provides a solar energy unmanned aerial vehicle wing has the energy and can regenerate and improve duration's characteristics.

In order to achieve the above object, the utility model provides a following technical scheme: solar energy unmanned aerial vehicle wing, including the wing, the fixed surface of wing is connected with the bottom metal, be provided with solar energy conduction device on the bottom metal, the fixed surface of bottom metal is connected with the solar energy absorption board, be provided with solar energy conversion device on the bottom metal.

Preferably, the solar energy conduction device comprises a heat conduction pipe and a fin, and the number of the heat conduction pipe is multiple.

Preferably, the side face of the solar energy conversion device is fixedly connected with an electric wire, and the electric wire is fixedly connected with an internal battery of the unmanned aerial vehicle.

Preferably, the side surface of the wing is in a shape of a rounded arc.

Compared with the prior art, the beneficial effects of the utility model are that:

the utility model discloses, through setting up solar energy absorption board, can realize the absorption to solar energy, through setting up solar energy conduction device, can improve conduction efficiency, the reinforcing energy utilization ratio, can convert heat energy into electric energy through setting up solar energy conversion equipment, realize storing the use, the device adopts solar energy absorption board, the bottom metal, solar energy conversion equipment and electric wire, can the variable increase energy on the original basis of unmanned aerial vehicle, promote unmanned aerial vehicle's continuation of the journey ability in the air, alleviate the proportion of the shared unmanned aerial vehicle weight of the energy, make unmanned aerial vehicle increase more functions, whole device is rational in infrastructure, high durability and convenient use, therefore, the clothes hanger is strong in practicability.

Drawings

The accompanying drawings are included to provide a further understanding of the invention, and are incorporated in and constitute a part of this specification, illustrate embodiments of the invention, and together with the description serve to explain the invention and not to limit the invention. In the drawings:

fig. 1 is a schematic structural view of a front view section of the present invention;

FIG. 2 is a schematic structural diagram of the bottom metal of the present invention;

in the figure: 1. an airfoil; 2. a solar energy conversion device; 3. an electric wire; 4. a solar energy absorbing panel; 5. a bottom layer metal; 6. a solar energy conduction device; 61. a heat conducting pipe; 62. and a fin.

Detailed Description

The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.

Examples

Referring to fig. 1-2, the present invention provides the following technical solutions: the solar unmanned aerial vehicle wing comprises a wing 1, wherein the surface of the wing 1 is fixedly connected with a bottom layer metal 5, the bottom metal 5 is provided with a solar energy conduction device 6, the surface of the bottom metal 5 is fixedly connected with a solar energy absorption plate 4, the solar energy absorption plate 4 is arranged to absorb solar energy, the solar energy conversion device 2 is arranged on the bottom metal 5, the solar energy conversion device is arranged to convert heat energy into electric energy to realize storage and use, the device adopts a solar energy absorbing plate 4, a bottom layer metal 5, a solar energy conversion device and an electric wire 3, can the variable increase energy on the original basis of unmanned aerial vehicle, promote unmanned aerial vehicle's the ability of continuing to move in the air, alleviate the proportion of the shared unmanned aerial vehicle weight of the energy, make unmanned aerial vehicle increase more functions, whole device is rational in infrastructure, convenient to use, the practicality is strong.

Specifically, solar energy conduction device 6 includes heat pipe 61 and fin 62, the quantity of heat pipe 61 is a plurality of, through setting up solar energy conduction device 6, can improve conduction efficiency, reinforcing energy utilization.

Specifically, the side fixedly connected with electric wire 3 of solar energy conversion device 2 through setting up electric wire 3, can realize the electric connection to electric wire 3 and battery, electric wire 3 and unmanned aerial vehicle internal battery fixed connection.

Specifically, the side surface of the wing 1 is set to be a smooth arc shape.

The utility model discloses a theory of operation and use flow: the utility model discloses, during the use, absorb solar energy through solar energy absorption plate 4, then transmit the solar energy of absorption to solar energy conversion device 2 and carry to the battery through electric wire 3 and store the use of being convenient for through heat pipe 61 and fin 62 among the 5 cooperation solar energy conduction devices 6 of bottom metal.

Finally, it should be noted that: although the present invention has been described in detail with reference to the foregoing embodiments, it will be apparent to those skilled in the art that modifications may be made to the embodiments described in the foregoing embodiments, or equivalents may be substituted for elements thereof. Any modification, equivalent replacement, or improvement made within the spirit and principle of the present invention should be included in the protection scope of the present invention.

Claims

1. Solar energy unmanned aerial vehicle wing, including wing (1), its characterized in that: the solar energy conversion wing is characterized in that a bottom layer metal (5) is fixedly connected to the surface of the wing (1), a solar energy conduction device (6) is arranged on the bottom layer metal (5), a solar energy absorption plate (4) is fixedly connected to the surface of the bottom layer metal (5), and a solar energy conversion device (2) is arranged on the bottom layer metal (5).

2. The solar drone wing of claim 1, wherein: the solar energy conduction device (6) comprises a heat conduction pipe (61) and a fin (62), and the number of the heat conduction pipe (61) is multiple.

3. The solar drone wing of claim 1, wherein: the side fixedly connected with electric wire (3) of solar energy conversion device (2), electric wire (3) and unmanned aerial vehicle internal battery fixed connection.

4. The solar drone wing of claim 1, wherein: the side surface of the wing (1) is in a smooth arc shape.