CN214504224U - Chinese lantern cluster performance unmanned aerial vehicle - Google Patents
Chinese lantern cluster performance unmanned aerial vehicle Download PDFInfo
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- CN214504224U CN214504224U CN202120902382.2U CN202120902382U CN214504224U CN 214504224 U CN214504224 U CN 214504224U CN 202120902382 U CN202120902382 U CN 202120902382U CN 214504224 U CN214504224 U CN 214504224U
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Abstract
The utility model belongs to the technical field of unmanned aerial vehicles, and discloses a Chinese lantern cluster performance unmanned aerial vehicle and application thereof, wherein a vehicle body comprises a lower shell, an upper shell and a carbon plate frame; the lower shell is provided with a heat dissipation hole for heat dissipation; a waterproof and dustproof structure is arranged in the upper shell; a flight control module sub-assembly is arranged in a cavity defined by the lower shell and the upper shell, and comprises a circuit board assembly and a battery cabin assembly; the circuit board assembly is arranged around the battery bin assembly to form an integrated module assembly structure; the lamp panel is installed on the circuit board assembly; the lamp panel is arranged on the carbon plate rack; the carbon plate frame is connected with the lantern. The utility model provides a Chinese lantern cluster performance unmanned aerial vehicle, which is characterized in that a waterproof and dustproof structure is arranged at the position of the radiating holes of the upper shell, so that the whole vehicle has better waterproof and dustproof performance while having better heat dissipation performance; the utility model discloses pass through the fixed column with the battery compartment subassembly and fix in the frame, avoided the plastic casing atress, make the complete machine reliability strengthen greatly.
Description
Technical Field
The utility model belongs to the technical field of unmanned aerial vehicle, especially, relate to a chinese style lantern cluster performance unmanned aerial vehicle and application.
Background
At present, in the field of lantern cluster performance unmanned aerial vehicles, modified airplanes are used as the main part, the existing consumer-grade unmanned aerial vehicle is utilized, a lantern outer cover which is simply built is fixed on the lantern outer cover, a framework and the lantern outer cover are both completed in a splicing mode, the lantern outer cover and a complete machine are poor in integrated design feeling, and the aesthetic feeling of current audiences is not met; in the existing lantern cluster performance unmanned aerial vehicle, a battery needs to be fixed on an airplane on site, and then the battery supplies power to the airplane through a plug-in connector, so that the site operation efficiency is low; the existing lantern cluster performance unmanned aerial vehicle has poor wind resistance, so that the application scene of the lantern cluster performance unmanned aerial vehicle is greatly limited; the existing lantern cluster performance unmanned aerial vehicle is not designed in a modularized manner, so that the reliability is insufficient, the assembly, disassembly and maintenance are inconvenient, and the explosion rate is high;
through the above analysis, the problems and defects of the prior art are as follows:
(1) the existing lantern cluster performance unmanned aerial vehicle is refitted by using the existing consumption unmanned aerial vehicle, the integral design feeling is poor, the product grade is low, and the commercial value of the product is reduced;
(2) the existing lantern cluster performance unmanned aerial vehicle needs long early-stage preparation work in field operation, so that the field operation efficiency is greatly reduced;
(3) the existing lantern cluster performance unmanned aerial vehicle is poor in pneumatic performance and insufficient in wind resistance, so that the application scene is greatly limited, and the commercial value of the unmanned aerial vehicle is reduced;
(4) the existing lantern cluster performance unmanned aerial vehicle is not designed in a modularized manner, so that the reliability is insufficient, the assembly, disassembly and maintenance are inconvenient, and the explosion rate is high;
(5) the existing lantern cluster performance unmanned aerial vehicle has the advantages that the lantern is small in size, low in brightness and poor in aerial performance effect;
(6) the existing lantern cluster performance unmanned aerial vehicle is short in flight time, insufficient in performance picture and poor in watching effect;
(7) the unmanned aerial vehicle for lantern cluster performance in the prior art has poor waterproof performance, and can cause the damage of the aircraft when encountering sudden weather.
The difficulty in solving the above problems and defects is:
in order to solve the above problems, the integral design of the lantern cluster performance unmanned aerial vehicle is needed, the integrated effect of the airplane is needed to be considered, the modular design of the airplane is needed to be considered, the pneumatic appearance of the airplane is needed to be considered, stronger power needs to be selected for the airplane, the waterproof design needs to be carried out on the airplane, the plugging and unplugging mode of the battery needs to be redesigned, the size of the lantern is needed to be considered, so that the better light performance effect is achieved, the problems are comprehensively solved, and the multifunctional lantern cluster performance unmanned aerial vehicle is a complex and huge project.
The significance of solving the problems and the defects is as follows:
after the problem is solved above, in lantern cluster performance market, it will be that a subversion changes, redefined lantern cluster performance unmanned aerial vehicle's performance, the modularized design makes things convenient for dismouting and maintenance, the integrated design has promoted complete machine reliability can, better pneumatic appearance and power lectotype have promoted the anti-wind ability of aircraft, higher luminance has promoted the performance effect of aircraft, the aircraft possesses certain waterproof ability simultaneously, its environmental suitability has been promoted.
SUMMERY OF THE UTILITY MODEL
Problem to prior art existence, the utility model provides a chinese style lantern cluster performance unmanned aerial vehicle and application.
The utility model is realized in such a way that the Chinese lantern cluster performance unmanned aerial vehicle comprises a body, wherein the body comprises a lower shell, an upper shell and a carbon plate frame; the lower shell is provided with a heat dissipation hole for heat dissipation; a waterproof and dustproof structure is arranged in the upper shell;
a flight control module sub-assembly is arranged in a cavity defined by the lower shell and the upper shell, and comprises a circuit board assembly and a battery cabin assembly; the circuit board assembly is arranged around the battery bin assembly to form an integrated module assembly structure;
the lamp panel is installed on the circuit board assembly;
the lamp panel is arranged on the carbon plate rack;
the carbon plate frame is connected with the lantern.
Further, a motor is mounted on the body;
the carbon plate frame is of a hollow structure.
Further, the battery compartment assembly is connected with the carbon plate rack through four battery compartment assembly fixing structures.
Further, a communication antenna is integrated in the lower shell.
Further, install the battery in the battery compartment subassembly, the skull of battery is as the structure of fuselage, the fuselage adopts streamlined.
Furthermore, the circuit board assembly is provided with a flight control module for controlling a flight track and controlling the unmanned aerial vehicle to fly according to a pattern preset in the air by lamplight.
Further, the lantern comprises a lantern sub-assembly and a lantern sub-assembly fixing structure; the lantern subassembly is arranged at the lower part of the lantern subassembly fixing structure; the lantern subassembly fixed knot constructs and links up with the carbon plate frame.
Another object of the present invention is to provide a chinese lantern cluster performance unmanned aerial vehicle in scenic spot parking and large public welfare activities cluster performance, brand propaganda, aerial advertisement cluster performance in the application.
Combine foretell all technical scheme, the utility model discloses the advantage that possesses and positive effect are: the utility model provides a Chinese lantern cluster performance unmanned aerial vehicle, which is provided with a waterproof and dustproof structure at the position of the radiating holes of the upper shell, so that the whole vehicle has better waterproof and dustproof performance while having better heat dissipation performance; the utility model fixes the battery compartment component on the frame through the fixing column, avoids the stress of the plastic shell and greatly enhances the reliability of the whole machine; the utility model discloses a lantern has improved maintenance efficiency with the quick detach of frame.
The utility model discloses a chinese style lantern cluster performance unmanned aerial vehicle integrated design and modular design make things convenient for module maintenance.
The utility model discloses under the prerequisite that satisfies light effect, realized the streamlined design of fuselage, promoted anti-wind ability.
The utility model discloses utilize wind field and the natural wind that aircraft self produced to dispel the heat to the aircraft, cancelled the radiator fan of aircraft, effectively reduced complete machine weight.
The utility model provides a chinese style lantern cluster performance unmanned aerial vehicle is used for doing the unmanned aerial vehicle formation light performance, and unmanned aerial vehicle in the formation can utilize light to draw preset's pattern aloft by flying control module control flight orbit, uses the scene to be scenic spot parking, large-scale public welfare activity, brand propaganda, advertisement in the air.
The utility model discloses a systematic design this time has effectively reduced the cost of maintenance and the time of module, has improved maintenance efficiency, and efficiency promotes more than 50%.
Drawings
In order to more clearly illustrate the technical solutions of the embodiments of the present invention, the drawings required to be used in the embodiments of the present invention will be briefly described below, and it is obvious that the drawings described below are only some embodiments of the present invention, and for those skilled in the art, other drawings can be obtained according to the drawings without creative efforts.
Fig. 1 is a schematic structural diagram of a chinese lantern cluster performance unmanned aerial vehicle provided by an embodiment of the present invention;
fig. 2 is a modularized exploded view of a chinese lantern cluster performance unmanned aerial vehicle provided by an embodiment of the present invention;
in the figure: 1. a motor; 2. a carbon plate frame; 3. an upper shell; 4. a lower case; 5. a lantern; 6. a rack sub-assembly; 7. a flight control module sub-assembly; 8. the lantern sub-assembly; 9. a battery compartment assembly fixing structure; 10. lantern subassembly fixed knot constructs.
Fig. 3 is the embodiment of the utility model provides a chinese style lantern cluster performance unmanned aerial vehicle's battery compartment subassembly and lantern and the enlargements of frame interconnection.
Detailed Description
In order to make the objects, technical solutions and advantages of the present invention more apparent, the present invention is further described in detail with reference to the following embodiments. It should be understood that the specific embodiments described herein are merely illustrative of the invention and are not intended to limit the invention.
To the problem that prior art exists, the utility model provides a chinese style lantern cluster performance unmanned aerial vehicle and control method and application thereof, it is right below to combine the figure and concrete embodiment the utility model discloses a technical scheme makes detailed description.
As shown in fig. 1-3, the embodiment of the utility model provides a chinese style lantern cluster performance unmanned aerial vehicle includes:
the device comprises a machine body, a battery bin assembly connected with the machine body, a lantern 5 and a motor 1 installed on the machine body;
the machine body comprises an upper shell 3, a lower shell 4 and a carbon plate frame 2; the carbon plate frame 2 is of a hollow structure, so that the weight of the airplane can be reduced; the lower shell and the upper shell are sequentially installed on the carbon plate frame 2 from bottom to top.
The flight control module sub-assembly 7 is installed inside the lower shell 4 and the upper shell 3, and the flight control module sub-assembly 7 comprises a circuit board assembly and a battery compartment assembly;
the circuit board assembly is arranged around the battery bin assembly to form an integrated module assembly structure;
the lamp panel is installed on the circuit board assembly; the battery compartment assembly is connected with the carbon plate rack 2 through four battery compartment assembly fixing structures 9, and the lower shell 4 and the upper shell 3 are not used as bearing structures and are only used as appearance parts; the heat dissipation structure of the lower shell 4 is a heat dissipation hole; a waterproof and dustproof structure is arranged in the upper shell 3; and a communication antenna is integrated in the lower shell 4 to form a modular design.
The lantern 5 comprises a lantern subassembly 8 and a lantern subassembly fixing structure 10. The lantern subassembly 8 is arranged at the lower part of the lantern subassembly fixing structure 10; the lantern subassembly fixed knot constructs 10 and links up with carbon plate frame 2.
The embodiment of the utility model provides a chinese style lantern cluster performance unmanned aerial vehicle's modularization is disassembled and is shown in fig. 2, the utility model provides a chinese style lantern cluster performance unmanned aerial vehicle's battery compartment subassembly and lantern and the enlargements of frame interconnection are shown in fig. 3.
The technical solution of the present invention will be further described with reference to the working principle and the embodiments.
Examples
The embodiment of the utility model provides an among the unmanned aerial vehicle flight performance of chinese style lantern cluster performance:
the unmanned aerial vehicle controls the flight track through the carried flight control module and flies according to the pattern preset in the air by light.
The heat generated in the unmanned aerial vehicle aircraft is carried out through a plurality of heat dissipation structures arranged on the lower shell for the self wind field and the natural wind generated in the unmanned aerial vehicle flight;
and the heat radiation structure is provided with a waterproof and dustproof structure for preventing water and dust.
As a preferred embodiment, a flight control module sub-assembly is installed in a cavity formed by a lower shell and an upper shell of the unmanned aerial vehicle, and comprises a circuit board assembly and a battery compartment assembly; the circuit board assembly is arranged around the battery bin assembly to form an integrated module assembly structure.
As a preferred embodiment, a battery is installed in the battery bin assembly, a head cover of the battery is used as a structure of the machine body, and the machine body is streamlined.
The circuit board assembly is provided with a flight control module;
the flight control module sub-assembly is connected with the carbon plate rack through a battery bin component fixing structure;
and the lantern subassembly fixing structure designed on the lantern is connected with the carbon plate frame.
As preferred embodiment, the utility model provides a chinese style lantern cluster performance unmanned aerial vehicle's control system, include:
and the flight control module is used for controlling the flight track of the unmanned aerial vehicle, and the flight track is used for drawing preset patterns in the air by utilizing lamplight.
In the description of the present invention, "a plurality" means two or more unless otherwise specified; the terms "upper", "lower", "left", "right", "inner", "outer", "front", "rear", "head", "tail", and the like indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are merely for convenience of description and simplicity of description, and do not indicate or imply that the device or element being referred to must have a particular orientation, be constructed and operated in a particular orientation, and thus, should not be construed as limiting the present invention. Furthermore, the terms "first," "second," "third," and the like are used for descriptive purposes only and are not to be construed as indicating or implying relative importance.
The above description is only for the specific embodiments of the present invention, but the protection scope of the present invention is not limited thereto, and any modification, equivalent replacement, and improvement made within the spirit and principle of the present invention should be covered within the protection scope of the present invention by those skilled in the art within the technical scope of the present invention.
Claims (7)
1. A Chinese lantern cluster performance unmanned aerial vehicle comprises a vehicle body, and is characterized in that the vehicle body comprises a lower shell, an upper shell and a carbon plate rack; the lower shell is provided with a heat dissipation hole for heat dissipation; a waterproof and dustproof structure is arranged in the upper shell;
a flight control module sub-assembly is arranged in a cavity defined by the lower shell and the upper shell, and comprises a circuit board assembly and a battery cabin assembly; the circuit board assembly is arranged around the battery bin assembly to form an integrated module assembly structure;
the lamp panel is installed on the circuit board assembly;
the lamp panel is arranged on the carbon plate rack;
the carbon plate frame is connected with the lantern.
2. The Chinese lantern cluster performance unmanned aerial vehicle of claim 1, wherein a motor is mounted on the body;
the carbon plate frame is of a hollow structure.
3. The Chinese lantern cluster performance unmanned aerial vehicle of claim 1, wherein the battery compartment assembly is connected to the carbon plate frame by four battery compartment assembly fixing structures.
4. The lantern cluster performance drone of claim 1, wherein a communication antenna is integrated into the lower shell.
5. The unmanned aerial vehicle for Chinese lantern cluster performances as claimed in claim 1, wherein a battery is installed in the battery compartment assembly, a head cover of the battery is used as a structure of the body, and the body is streamlined.
6. The Chinese lantern cluster performance unmanned aerial vehicle of claim 1, wherein the circuit board assembly is provided with a flight control module for controlling a flight trajectory and controlling the unmanned aerial vehicle to fly according to a preset pattern of lights in the air.
7. The unmanned aerial vehicle for Chinese lantern cluster performance as claimed in claim 1, wherein the lantern comprises a lantern subassembly and a lantern subassembly fixing structure; the lantern subassembly is arranged at the lower part of the lantern subassembly fixing structure; the lantern subassembly fixed knot constructs and links up with the carbon plate frame.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202120902382.2U CN214504224U (en) | 2021-04-28 | 2021-04-28 | Chinese lantern cluster performance unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202120902382.2U CN214504224U (en) | 2021-04-28 | 2021-04-28 | Chinese lantern cluster performance unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN214504224U true CN214504224U (en) | 2021-10-26 |
Family
ID=78204617
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202120902382.2U Active CN214504224U (en) | 2021-04-28 | 2021-04-28 | Chinese lantern cluster performance unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN214504224U (en) |
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2021
- 2021-04-28 CN CN202120902382.2U patent/CN214504224U/en active Active
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