CN211391707U - Unmanned plane - Google Patents
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- CN211391707U CN211391707U CN202020039703.6U CN202020039703U CN211391707U CN 211391707 U CN211391707 U CN 211391707U CN 202020039703 U CN202020039703 U CN 202020039703U CN 211391707 U CN211391707 U CN 211391707U
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E60/00—Enabling technologies; Technologies with a potential or indirect contribution to GHG emissions mitigation
- Y02E60/10—Energy storage using batteries
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
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Landscapes
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Abstract
The utility model provides an unmanned aerial vehicle relates to the flight machinery field. The utility model provides an unmanned aerial vehicle, which comprises a vehicle body and an integrated battery arranged in the vehicle body, wherein a battery cabin is arranged at the top of the vehicle body; the integrated battery is arranged in the battery bin and comprises an electric core and an encapsulation structure used for encapsulating the electric core, the encapsulation structure comprises a photovoltaic film layer arranged on the outermost layer, and the photovoltaic film layer is electrically connected with the electric core to charge the electric core. The photovoltaic film layer is used for receiving sunlight and converting solar energy into electric energy, and therefore the battery cell is charged. The utility model provides an among the unmanned aerial vehicle, through forming integrated battery with electric core and packaging structure integration together, integrated battery is convenient for install in unmanned aerial vehicle's battery compartment, need not moreover to set up the wire of overlength on unmanned aerial vehicle, consequently the utility model provides an unmanned aerial vehicle battery installation loaded down with trivial details problem.
Description
Technical Field
The utility model relates to a flying machine technical field especially relates to an unmanned aerial vehicle.
Background
Unmanned aerial vehicle is a new concept aircraft, has the advantage that flexible, response is rapid, the operation requirement is low, and unmanned aerial vehicle technique is in the rapid development process at present, has extensive usage, and unmanned aerial vehicle can carry out activities such as some small-scale information transfer, monitoring, through carrying on multiclass sensor, can also realize functions such as image real-time transmission, high-risk area detection, is the favourable replenishment of satellite remote sensing and traditional aerial remote sensing. The unmanned aerial vehicle can be applied to multiple fields such as military affairs, scientific research, communication, agriculture and photography.
In the related art, the unmanned aerial vehicle is usually powered by a lithium battery, or the lithium battery is charged by a solar battery installed on the unmanned aerial vehicle, and then the lithium battery supplies power to the unmanned aerial vehicle. Wherein, the lithium cell sets up inside unmanned aerial vehicle usually, and solar cell lays usually on unmanned aerial vehicle's fuselage, still needs the wire to be connected between solar cell and the lithium cell, and consequently the installation of battery is loaded down with trivial details in this kind of unmanned aerial vehicle power supply mode.
SUMMERY OF THE UTILITY MODEL
An embodiment of the utility model provides an unmanned aerial vehicle for solve the loaded down with trivial details problem of unmanned aerial vehicle battery installation.
In order to achieve the purpose, the embodiment of the utility model provides an unmanned aerial vehicle, including the fuselage and setting up the integrated battery in the fuselage, the top of fuselage is provided with the battery compartment;
the integrated battery is arranged in the battery bin and comprises an electric core and an encapsulation structure used for encapsulating the electric core, the encapsulation structure comprises a photovoltaic thin film layer arranged on the outermost layer, and the photovoltaic thin film layer is electrically connected with the electric core to charge the electric core.
The embodiment of the utility model provides an unmanned aerial vehicle has following advantage: the unmanned aerial vehicle provided by the embodiment of the utility model comprises a vehicle body and an integrated battery, wherein the vehicle body is provided with a battery cabin; the integrated battery is placed in the battery bin and comprises a battery core and an encapsulation structure for encapsulating the battery core, the encapsulation structure comprises a photovoltaic film layer, and the photovoltaic film layer is electrically connected with the battery core; the photovoltaic film layer is arranged on the outermost layer and used for receiving sunlight and converting solar energy into electric energy so as to supply power to the battery cell; the embodiment of the utility model provides an unmanned aerial vehicle, through forming integrated battery with electric core and packaging structure integration together, integrated battery is convenient for install in the battery compartment, need not to set up the wire of overlength moreover on unmanned aerial vehicle, has solved the loaded down with trivial details problem of current unmanned aerial vehicle battery installation.
As the utility model discloses unmanned aerial vehicle's further improvement, packaging structure sets up to flexible packaging film, flexible packaging film still includes heat-seal layer, first tie coat, aluminium rete, second tie coat and the barrier layer that sets gradually from inside to outside, the photovoltaic thin layer sets up the outside of barrier layer.
As the utility model discloses unmanned aerial vehicle's further improvement, integrated battery includes first wire and second wire, the both ends of first wire are connected respectively the first electrode of flexible encapsulating film with the first utmost point ear of electric core, the both ends of second wire are connected respectively the second electrode of flexible encapsulating film with the second utmost point ear of electric core.
As the embodiment of the utility model provides an unmanned aerial vehicle's further improvement, the barrier layer is polyimide, polyethylene terephthalate, polyethylene naphthalate, or polyamide.
As the embodiment of the utility model provides an unmanned aerial vehicle's further improvement, the top of battery compartment is provided with the transparent sealing lid.
As the embodiment of the utility model provides an unmanned aerial vehicle's further improvement, the transparent sealing lid with fuselage bolted connection.
As the embodiment of the utility model provides an unmanned aerial vehicle's further improvement, transparent sealing lid is transparent glass lid or transparent plastic lid.
As the embodiment of the utility model provides an unmanned aerial vehicle's further improvement, unmanned aerial vehicle still includes at least one screw, the screw sets up on the fuselage, and with integrated battery electric connection.
As the utility model discloses unmanned aerial vehicle's further improvement, be provided with a plurality of wings on the fuselage, every install one on the wing the screw.
As the embodiment of the utility model provides an unmanned aerial vehicle's further improvement, unmanned aerial vehicle still includes the landing frame, the landing frame sets up the bottom of fuselage.
In addition to the technical problems solved by the embodiments of the present invention, the technical features constituting the technical solutions, and the advantageous effects brought by the technical features of these technical solutions, further detailed descriptions will be made in specific embodiments for other technical problems that can be solved by the unmanned aerial vehicle provided by the embodiments of the present invention, other technical features included in the technical solutions, and advantageous effects brought by these technical features.
Drawings
In order to illustrate more clearly the embodiments of the invention or the technical solutions in the prior art, the drawings which are needed in the description of the embodiments of the invention or the prior art will be briefly described below, it is obvious that the drawings in the following description are only a part of the embodiments of the invention, and the drawings and the description are not intended to limit the scope of the disclosed concept in any way, but to illustrate the disclosed concept for a person skilled in the art by referring to a specific embodiment, and for a person skilled in the art, other drawings can be obtained from the drawings without inventive effort.
Fig. 1 is a schematic structural diagram of an unmanned aerial vehicle according to an embodiment of the present invention;
fig. 2 is a schematic structural diagram of an unmanned aerial vehicle according to an embodiment of the present invention;
fig. 3 is a cross-sectional view of an integrated battery according to an embodiment of the present invention.
Description of reference numerals:
100-a fuselage;
110-a battery compartment;
120-transparent sealing lid;
130-a propeller;
140-an airfoil;
150-a drop frame;
200-an integrated battery;
210-a cell;
220-packaging structure.
Detailed Description
The unmanned aerial vehicle is usually supplied with power by a lithium battery, or the lithium battery is charged by a solar battery installed on the unmanned aerial vehicle, and then the lithium battery supplies power to the unmanned aerial vehicle. The lithium cell sets up inside unmanned aerial vehicle usually, and solar cell lays on unmanned aerial vehicle's fuselage usually, still needs the wire to be connected between solar cell and the lithium cell, and this kind of mode battery installation is loaded down with trivial details. In order to solve the problem that the existing unmanned aerial vehicle battery installation process is complicated, the embodiment of the utility model provides an unmanned aerial vehicle, which comprises a vehicle body and an integrated battery, wherein a battery cabin is arranged on the vehicle body; the integrated battery is placed in the battery bin and comprises a battery cell and an encapsulation structure for encapsulating the battery cell, the encapsulation structure comprises a photovoltaic film layer arranged on the outermost layer, and the photovoltaic film layer is electrically connected with the battery cell to charge the battery cell; through forming integrated battery with electric core and packaging structure integration together to be convenient for install, and need not to set up the wire of overlength on unmanned aerial vehicle.
In order to make the above objects, features and advantages of the embodiments of the present invention more obvious and understandable, the technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention. It is obvious that the described embodiments are only some of the embodiments of the present invention, and not all of them. Based on the embodiments of the present invention, all other embodiments obtained by a person skilled in the art without creative efforts all belong to the protection scope of the present invention.
Referring to fig. 1, an unmanned aerial vehicle according to an embodiment of the present invention includes a main body 100 and an integrated battery 200 disposed in the main body 100, wherein a battery compartment 110 is disposed at a top of the main body 100; the integrated battery 200 is disposed in the battery compartment 110, the integrated battery 200 includes a battery cell 210 and an encapsulation structure 220 for encapsulating the battery cell 210, and the encapsulation structure 220 includes a photovoltaic film layer disposed at an outermost layer, and the photovoltaic film layer is electrically connected to the battery cell 210 to charge the battery cell 210.
Specifically, the unmanned aerial vehicle that this embodiment provided includes fuselage 100 and integrated battery 200, is provided with the battery compartment 110 that is used for placing integrated battery 200 on fuselage 100. As shown in fig. 1, the battery compartment 110 is disposed at the top of the fuselage 100, and it should be noted that, in this embodiment, the top of the fuselage 100 refers to a side of the fuselage 100 that faces away from the ground when the drone is in a normal flight or normal parking state. The integrated battery 200 is placed in the battery compartment 110, and specifically, a card slot may be provided in the battery compartment 110, so as to connect the integrated battery 200 in the card slot, thereby preventing the integrated battery 200 from falling off.
Further, the battery compartment 110 is specifically located in the middle of the body 100, for example, when the top view shape of the body 100 is a circle, the battery compartment 110 may be located at the center of the circle; for another example, when the top view shape of the body 100 is a rectangle, the battery compartment 110 may be located at an intersection of two diagonals of the rectangle.
Because integrated battery 200 has been placed in the battery compartment 110, integrated battery 200 is used for supplying power to each component or position of unmanned aerial vehicle, consequently, set up integrated battery 200 and be convenient for integrated battery 200 to supply power to component all around in the middle part of unmanned aerial vehicle's fuselage 100, avoided the too much or overlength of power supply line to lead to the circuit confusion.
In this embodiment, the integrated battery 200 includes a battery cell 210 and a package structure 220, and specifically, the battery cell 210 may be a lithium ion battery cell. As shown in fig. 3, the encapsulation structure 220 is formed on the outer surface of the battery cell 210, the encapsulation structure 220 includes a photovoltaic thin film layer, and thus has a photovoltaic property, and the encapsulation structure 220 can be used not only to encapsulate the battery cell 210, but also to charge the battery cell 210 by converting solar energy into electric energy. Specifically, the photovoltaic thin film layer in the package structure 220 is electrically connected to the battery cell 210, specifically, the photovoltaic thin film layer may be electrically connected to the battery cell by a metal gate line.
Further, in the embodiment, the photovoltaic thin film layer includes at least one photovoltaic thin film unit, and the photovoltaic thin film unit has photovoltaic characteristics and can independently convert solar energy into electric energy; the photovoltaic thin film units respectively comprise a substrate and photovoltaic thin film subunits arranged on the upper surface of the substrate. When the number of the photovoltaic thin film units is provided in plurality, the plurality of photovoltaic thin film units may be connected in series or in parallel.
In addition to the above embodiments, the battery compartment 110 may be a groove integrally formed on the body 100, or may be a box structure mounted on the body 100. Taking the battery compartment 110 as a groove as an example, in the embodiment, the battery compartment 110 is disposed on the top of the body 100, so that the upper end of the battery compartment 110 has an opening, so that sunlight can be irradiated into the battery compartment 110, and the photovoltaic thin film layer on the package structure 220 realizes conversion from solar energy to electric energy.
In this embodiment, the photovoltaic thin film layer converts solar energy into electric energy by receiving sunlight, and charges the battery cell 210. Specifically, the photovoltaic thin film layer is electrically connected to the battery cell 210, so as to charge the battery cell 210.
In addition, the unmanned aerial vehicle that this embodiment provided can also include devices such as light, loudspeaker, displacement sensor, temperature sensor and camera, and devices such as light, loudspeaker, displacement sensor, temperature sensor and camera are installed on unmanned aerial vehicle's fuselage 100 to respectively with integrated battery 200 electric connection, integrated battery 200 supplies power for above-mentioned a plurality of devices.
To sum up, the unmanned aerial vehicle provided by the embodiment of the present invention includes a body 100 and an integrated battery 200, wherein the body 100 is provided with a battery compartment 110; the integrated battery 200 is placed in the battery compartment 110, the integrated battery 200 includes a battery cell 210 and an encapsulation structure 220 for encapsulating the battery cell 210, the encapsulation structure 220 includes a photovoltaic film layer disposed at an outermost layer, and the photovoltaic film layer is electrically connected with the battery cell 210 to charge the battery cell 210; in the present embodiment, the photovoltaic thin film layer is disposed on the outermost layer of the integrated battery 200, and is configured to receive sunlight and convert solar energy into electric energy, so as to charge the battery cell 210. The embodiment of the utility model provides a form integrated battery 200 for packaging structure 220 that has the photovoltaic effect through the encapsulating film with on electric core 210, not only be convenient for install in the battery compartment, need not to set up the wire of overlength moreover on unmanned aerial vehicle, solved the loaded down with trivial details problem of unmanned aerial vehicle battery installation.
Further, in a possible implementation manner, the packaging structure 220 is configured as a flexible packaging film, the flexible packaging film further includes a heat sealing layer, a first bonding layer, an aluminum film layer, a second bonding layer and a blocking layer, which are sequentially disposed from inside to outside, and the photovoltaic thin film layer is disposed on the outer side of the blocking layer. The flexible encapsulation film serves to package and protect the internal structure of the cell 210.
Further, in one possible implementation, the heat seal layer is a polypropylene film layer. Polypropylene is a polymer obtained by addition polymerization of propylene, is a thermoplastic synthetic resin with excellent performance, and is colorless translucent thermoplastic light general-purpose plastic. The polypropylene film layer has chemical resistance, heat resistance, electrical insulation, high-strength mechanical properties and good high-wear-resistance processability, and the stability of the integrated battery 200 is improved by using the polypropylene film layer as a heat-sealing layer.
Further, the photovoltaic thin film layer positioned on the outermost layer is bonded with the barrier layer. The material of the barrier layer can be polyimide, polyethylene terephthalate, polyethylene naphthalate or polyamide. The second bonding layer is positioned in the barrier layer, and the aluminum film layer is formed on one side of the second bonding layer, which is far away from the barrier layer; the first bonding layer and the second bonding layer can be made of one or more of polyethyleneimine adhesive, polyurethane adhesive and melamine adhesive; the heat seal layer is positioned at the innermost side.
The photovoltaic thin film layer in the flexible packaging film and the battery cell 210 may be electrically connected by a metal gate line, and specifically, in a possible implementation manner, the integrated battery 200 includes a first wire and a second wire, a first electrode of the flexible packaging film and a first tab of the battery cell 210 are respectively connected to two ends of the first wire, and a second electrode of the flexible packaging film and a second tab of the battery cell 210 are respectively connected to two ends of the second wire.
Specifically, when a plurality of photovoltaic thin film units are disposed on the photovoltaic thin film layer, the plurality of photovoltaic thin film units form a photovoltaic unit array on the surface of the electric core 210, and the N photovoltaic thin film units are connected to each other to form an output end of electric energy of the flexible encapsulation film with photovoltaic characteristics, that is, the first electrode and the second electrode, where the first electrode may be a positive electrode or a negative electrode, and the polarity of the second electrode is opposite to that of the first electrode. Wherein, the connection relationship between any two photovoltaic thin film units can be further determined according to the charging voltage of the integrated battery 200.
Further, in one possible implementation, the barrier layer is a polyimide, polyethylene terephthalate, polyethylene naphthalate, or polyamide. The polyamide is commonly called nylon, is developed on the basis of polyamide fiber, is a thermoplastic plastic capable of bearing load and has an insulating effect.
Further, in one possible implementation, as shown in fig. 2, the top of the battery compartment 110 is provided with a transparent sealing cover 120. In the embodiment, the battery compartment 110 is taken as a groove disposed on the body 100 for example, as shown in fig. 1, a transparent sealing cover 120 is disposed on the top of the battery compartment 110, and the transparent sealing cover 120 is tightly fitted with the battery compartment 110 for preventing dust, rain water or other contaminants from entering the battery compartment 110.
On the basis of the above embodiment, the top of the transparent sealing cover 120 may be flush with the surface of the body 100 or higher than the surface of the body 100. It should be noted that, the surface of the main body 100 herein refers to a side of the main body 100 where the battery compartment 110 is disposed, i.e., a top surface of the main body 100.
In this embodiment, the transparent sealing cover 120 is connected above the battery compartment 110 in various ways, for example, the battery compartment 110 and the transparent sealing cover 120 may be connected in a clamping manner, specifically, a plurality of clamping slots may be disposed on a side wall of the battery compartment 110, a plurality of fasteners are disposed on an edge of the transparent sealing cover 120 facing the battery compartment 110, and the clamping of the battery compartment 110 and the transparent sealing cover 120 is realized by the cooperation of the fasteners and the clamping slots; for another example, when the cross-sectional shapes of the battery compartment 110 and the transparent sealing cover 120 are circular, the battery compartment 110 and the transparent sealing cover 120 may be in threaded connection, specifically, an internal thread may be provided on an inner wall of the battery compartment 110, an external thread may be provided on an outer wall of a side of the transparent sealing cover 120 facing the battery compartment 110, and the internal thread and the external thread cooperate to realize the threaded connection between the battery compartment 110 and the transparent sealing cover 120.
In a preferred implementation, the transparent sealing cover 120 is bolted to the body 100. The bolt connection is not limited by the shapes of the transparent sealing cover 120 and the battery compartment 110, and specifically, the transparent sealing cover 120 may be directly fastened to the body 100 above the battery compartment 110, a flange is provided at an edge of the transparent sealing cover 120, the flange is in contact with the body 100, connection holes are respectively provided at the flange and the body 100 in contact therewith, and bolts pass through the connection holes to connect the transparent sealing cover 120 to the body 100, so that the transparent sealing cover 120 is mounted above the battery compartment 110.
Further, in one possible implementation, the transparent sealing cover 120 is a transparent glass cover or a transparent plastic cover. In this embodiment, the transparent sealing cover 120 is provided to ensure that sunlight can enter the battery compartment 110, so that the photovoltaic thin film layer on the integrated battery 200 can absorb solar energy to convert electric energy. The transparent sealing cover 120 may be a transparent glass cover or a transparent plastic cover, and is preferably a transparent plastic cover, which is light in weight and easy to install.
Further, in a possible implementation manner, the unmanned aerial vehicle provided in this embodiment further includes at least one propeller 130, and the propeller 130 is disposed on the fuselage 100 and electrically connected to the integrated battery 200. In this embodiment, the number of the propellers 130 may be one or more. When one propeller 130 is provided, the propeller 130 is close to the center of the body 100; when the number of the propeller 130 is plural, two, three, or four may be specific. The propeller 130 is electrically connected with the integrated battery 200, and the integrated battery 200 supplies power to the propeller 130.
Specifically, the integrated battery 200 may power the propeller 130 in the following manner: the photovoltaic thin film layer on the integrated battery 200 absorbs solar energy and converts the solar energy into electric energy to charge the electric core 210, and the electric core 210 supplies power to the propeller 130.
Further, in one possible implementation, the fuselage 100 is provided with a plurality of wings 140, each wing 140 having a propeller 130 mounted thereon. The number of the wings 140 is multiple, specifically, two, three or four, each wing 140 is connected with one propeller 130, and the stability of the unmanned aerial vehicle in the flying state is ensured by the arrangement.
As shown in fig. 1, in the present embodiment, four wings 140 are disposed on the fuselage 100, and the four wings 140 are arranged at equal intervals; on top of each wing 140 there is a propeller 130, the propeller 130 being connected to the wing 140.
Further, in a possible implementation manner, a falling frame 150 is further included, and the falling frame 150 is disposed at the bottom of the fuselage 100. As shown in fig. 1, the falling frame 150 is a U-shaped bracket connected to the bottom of the fuselage 100, and the falling frame 150 and the fuselage 100 may be connected by welding or integrally formed; the number of the drop frames 150 may be two or more. When the unmanned aerial vehicle lands on the ground or other landing planes, the landing frame 150 arranged at the bottom of the fuselage 100 contacts with the ground or other landing planes, and the landing frame 150 is used for supporting the fuselage 100.
The embodiments or implementation modes in the present specification are described in a progressive manner, each embodiment focuses on differences from other embodiments, and the same and similar parts among the embodiments may be referred to each other.
In the description of the present specification, reference to the terms "one embodiment", "some embodiments", "illustrative embodiments", "example", "specific example", or "some examples" or the like means that a particular feature, structure, material, or characteristic described in connection with the embodiment or example is included in at least one embodiment or example of the present invention. In this specification, schematic representations of the above terms do not necessarily refer to the same embodiment or the same example. Furthermore, the particular features, structures, materials, or characteristics described may be combined in any suitable manner in any one or more embodiments or examples.
Finally, it should be noted that: the above embodiments are only used to illustrate the technical solution of the present invention, and not to limit the same; although the present invention has been described in detail with reference to the foregoing embodiments, it should be understood by those skilled in the art that: the technical solutions described in the foregoing embodiments may still be modified, or some or all of the technical features may be equivalently replaced; such modifications and substitutions do not depart from the spirit and scope of the present invention.
Claims (10)
1. An unmanned aerial vehicle is characterized by comprising a body and an integrated battery arranged in the body, wherein a battery bin is arranged at the top of the body;
the integrated battery is arranged in the battery bin and comprises an electric core and an encapsulation structure used for encapsulating the electric core, the encapsulation structure comprises a photovoltaic thin film layer arranged on the outermost layer, and the photovoltaic thin film layer is electrically connected with the electric core to charge the electric core.
2. The unmanned aerial vehicle of claim 1, wherein the packaging structure is a flexible packaging film, the flexible packaging film further comprises a heat sealing layer, a first bonding layer, an aluminum film layer, a second bonding layer and a blocking layer, the heat sealing layer, the first bonding layer, the aluminum film layer, the second bonding layer and the blocking layer are sequentially arranged from inside to outside, and the photovoltaic film layer is arranged on the outer side of the blocking layer.
3. The unmanned aerial vehicle of claim 2, wherein the integrated battery comprises a first wire and a second wire, two ends of the first wire are respectively connected to the first electrode of the flexible encapsulation film and the first tab of the battery cell, and two ends of the second wire are respectively connected to the second electrode of the flexible encapsulation film and the second tab of the battery cell.
4. The drone of claim 2, wherein the barrier layer is polyimide, polyethylene terephthalate, polyethylene naphthalate, or polyamide.
5. The unmanned aerial vehicle of claim 1, wherein a transparent sealing cover is disposed on a top of the battery compartment.
6. The drone of claim 5, wherein the transparent sealing cover is bolted to the fuselage.
7. The unmanned aerial vehicle of claim 6, wherein the transparent sealing cover is a clear glass cover or a clear plastic cover.
8. The drone of claim 1, further comprising at least one propeller disposed on the fuselage and electrically connected to the integrated battery.
9. A drone as claimed in claim 8, wherein the fuselage is provided with a plurality of wings, one propeller being mounted on each wing.
10. The drone of claim 1, further comprising a landing shelf disposed at a bottom of the fuselage.
Priority Applications (1)
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| CN112757933A (en) * | 2021-02-03 | 2021-05-07 | 北京视讯伟业科技有限公司 | Unmanned aerial vehicle's full-automatic electricity charging platform that trades |
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| CN112757933A (en) * | 2021-02-03 | 2021-05-07 | 北京视讯伟业科技有限公司 | Unmanned aerial vehicle's full-automatic electricity charging platform that trades |
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