An integrated drone ground reference station

Abstract

The utility model discloses an integrated unmanned vehicle ground reference station, including shell and front cover, the front cover sets up at the front of shell, the front of front cover and the back of shell all is provided with the fin, the front of fin is provided with the cooling fan, the back of shell inner chamber is provided with power module, picture transmits module, flight control module, conversion module, data exchange module and satellite time service module in proper order. The utility model discloses through fin is a kind of passive heat dissipation equipment, usually made of metal material, its working principle is through increasing radiating area to improve heat conduction efficiency, and fin is in close contact with heating element, and the heat generated by element is rapidly conducted to the surface of fin, and the heat is dissipated to air through natural convection, and through cooling fan is a kind of active heat dissipation equipment, and the rotation of fan blade is driven by motor, and forced convection air is used to accelerate the dissipation of heat, to further improve the heat dissipation efficiency.

Description

Technical Field

[0001] This utility model relates to the field of integrated UAV ground reference station technology, specifically an integrated UAV ground reference station. Background Technology

[0002] With the rapid development of drone technology, long-range drones are slow to deploy and carry more and more equipment, which puts a heavy burden on ground staff. Compared with the multiple devices in a separate ground station, integrating multiple devices into a single enclosure makes it easier to control the drone. Therefore, integrated drone ground reference stations are needed.

[0003] Currently available integrated UAV ground base stations have poor heat dissipation. In high-temperature environments, this can affect the use of equipment components. Long-term use can lead to heat buildup, causing damage to equipment components. It is also inconvenient to disassemble and replace equipment components, thus shortening their lifespan.

[0004] Therefore, it is necessary to provide an integrated UAV ground reference station to solve the above-mentioned technical problems. The information disclosed in this background section is only intended to enhance the understanding of the overall background of this utility model, and is not necessarily to be regarded as an admission or to imply in any way that the information constitutes prior art known to those skilled in the art. Utility Model Content

[0005] The purpose of this invention is to provide an integrated UAV ground reference station, which solves the problems of poor heat dissipation in the integrated UAV ground reference station mentioned in the background, which affects the use of equipment components in high-temperature environments, and causes damage to equipment components due to the inability to dissipate heat after long-term use, making it inconvenient to disassemble and replace equipment components and shortening the service life of equipment components.

[0006] To achieve the above objectives, this utility model provides the following technical solution: an integrated UAV ground reference station, comprising a shell and a front cover, the front cover being disposed on the front of the shell, heat sinks being disposed on both the front of the front cover and the back of the shell, a cooling fan being disposed on the front of the heat sinks, a power module, an image transmission module, a flight control module, a conversion module, a data exchange module, and a satellite timing module being disposed sequentially on the back of the inner cavity of the shell, the number of image transmission modules being two, and both being symmetrically disposed vertically on the left side of the back of the inner cavity of the shell, the data exchange module being disposed on the right side of the upper end of the image transmission module, the flight control module being disposed on the right side of the image transmission module and the data exchange module, the conversion module being disposed above the flight control module, and the power module being disposed on the left side of the conversion module, input and output interfaces being disposed on both the upper end and the bottom sides of both sides of the shell, a dual-channel filter and a power amplifier being disposed sequentially on the back of the front cover, the dual-channel filter being disposed above the power amplifier, the dual-channel filter comprising a single-channel filter and a dielectric filter, the dielectric filter being disposed in front of the single-channel filter.

[0007] Preferably, hinge seats are installed on both sides of the top of the front cover, and the bottom of the hinge seats is fixed to both sides of the top of the outer shell. The hinge seats are made of metal.

[0008] Preferably, the inner walls of both the outer casing and the front cover are coated with a conductive coating.

[0009] Preferably, the outer surface of the inner wall of the outer shell is provided with a sealing ring groove, and the inner cavity of the sealing ring groove is provided with a conductive and waterproof sealing ring.

[0010] Preferably, screws are provided around the front of the cooling fan, and the back of the screws penetrates through the back of the cooling fan and is fixed to the front of the heat sink.

[0011] Preferably, the number of input / output interfaces is six, and the six input / output interfaces are distributed sequentially on the upper and lower sides of the outer casing.

[0012] Compared with the prior art, the beneficial effects of this utility model are as follows:

[0013] 1. This utility model uses a heat sink, which is a passive heat dissipation device, usually made of metal. Its working principle is to increase the heat dissipation area to improve the heat conduction efficiency. The heat sink is in close contact with the heat-generating element, which quickly conducts the heat generated by the element to the surface of the heat sink, and dissipates the heat into the air through natural convection. The cooling fan is an active heat dissipation device. The fan blades are driven by a motor to rotate, which forces the air to convect and accelerate the dissipation of heat, further improving the heat dissipation efficiency.

[0014] 2. This utility model has a conductive coating applied to the inner wall of both the outer shell and the front cover. The conductive coating can effectively absorb, conduct and attenuate electromagnetic waves, thereby shielding electromagnetic interference. This is very important for controlling the induction and radiation of electric fields, magnetic fields and electromagnetic waves. The conductive coating usually contains conductive metal powder, such as copper and silver. The paint film formed after drying has excellent conductivity. Attached Figure Description

[0015] Figure 1 This is a schematic diagram of the structure of this utility model;

[0016] Figure 2 This is a bottom view of the left side of the outer shell and front cover structure of this utility model;

[0017] Figure 3 This is a front sectional view of the outer shell structure of this utility model;

[0018] Figure 4 This is a cross-sectional view of the back of the front cover structure of this utility model;

[0019] Figure 5 This is a rear sectional view of the satellite timing module and power amplifier structure of this utility model;

[0020] Figure 6 This is a cross-sectional view of the back of the dielectric filter structure of this utility model.

[0021] In the diagram: 1. Outer shell; 2. Front cover; 3. Heat sink; 4. Cooling fan; 5. Power module; 6. Image transmission module; 7. Flight control module; 8. Conversion module; 9. Data exchange module; 10. Satellite timing module; 11. Input / output interface; 12. Dual-channel filter; 13. Power amplifier; 14. Single-channel filter; 15. Medium filter; 16. Hinge seat; 17. Waterproof sealing ring. Detailed Implementation

[0022] To enable those skilled in the art to better understand the technical solution of this utility model, the present utility model will be described in detail below with reference to the accompanying drawings. The description in this part is only exemplary and explanatory, and should not be used to limit the scope of protection of this utility model in any way.

[0023] It should be noted that similar labels and letters in the following figures indicate similar items. Therefore, once an item is defined in one figure, it does not need to be further defined and explained in subsequent figures.

[0024] It should be noted that the terms "center," "upper," "lower," "left," "right," "vertical," "horizontal," "inner," and "outer," etc., indicate the orientation or positional relationship based on the orientation or positional relationship shown in the accompanying drawings, or the orientation or positional relationship commonly used when the product is in use. They are only for the convenience of describing the present invention and simplifying the description, and do not indicate or imply that the device or element referred to must have a specific orientation, or be constructed and operated in a specific orientation. Therefore, they should not be construed as limitations on the present invention. In addition, the terms "first," "second," and "third," etc., are only used to distinguish descriptions and should not be construed as indicating or implying relative importance.

[0025] Furthermore, terms such as "horizontal," "vertical," and "sag" do not imply that components must be absolutely horizontal or suspended, but rather that they can be slightly tilted. For example, "horizontal" simply means that its direction is more horizontal relative to "vertical," and does not mean that the structure must be completely horizontal, but can be slightly tilted.

[0026] In the description of this utility model, it should also be noted that, unless otherwise explicitly specified and limited, the terms "set," "install," "connect," and "link" should be interpreted broadly. For example, they can refer to a fixed connection, a detachable connection, or an integral connection; they can refer to a mechanical connection or an electrical connection; they can refer to a direct connection or an indirect connection through an intermediate medium; and they can refer to the internal connection of two components. Those skilled in the art can understand the specific meaning of the above terms in this utility model based on the specific circumstances.

[0027] Please see Figures 1-6 An integrated UAV ground reference station includes a shell 1 and a front cover 2. The front cover 2 is located on the front of the shell 1. Heat sinks 3 are provided on both the front of the front cover 2 and the back of the shell 1. A cooling fan 4 is provided on the front of the heat sink 3. A power module 5, an image transmission module 6, a flight control module 7, a conversion module 8, a data exchange module 9, and a satellite timing module 10 are arranged sequentially on the back of the inner cavity of the shell 1. There are two image transmission modules 6, and both are symmetrically arranged vertically on the left side of the back of the inner cavity of the shell 1. The data exchange module 9 is located on the right side above the image transmission modules 6. The flight control module 7 is located to the right of the image transmission module 6 and the data exchange module 9. The conversion module 8 is located above the flight control module 7. The power module 5 is located to the left of the conversion module 8. Input and output interfaces 11 are provided on the upper and lower sides of both sides of the outer shell 1. A dual-channel filter 12 and a power amplifier 13 are arranged sequentially on the back of the front cover 2. The dual-channel filter 12 is located above the power amplifier 13. The dual-channel filter 12 includes a single-channel filter 14 and a medium filter 15. The medium filter 15 is located in front of the single-channel filter 14.

[0028] Hinges 16 are installed on both sides of the top of the front cover 2. The bottom of the hinges 16 is fixed to the two sides of the top of the outer shell 1. The hinges 16 are made of metal. A conductive coating is applied to the inner wall of both the outer shell 1 and the front cover 2. The conductive coating can effectively absorb, conduct and attenuate electromagnetic waves, thereby shielding electromagnetic interference. This is very important for controlling the induction and radiation of electric fields, magnetic fields and electromagnetic waves.

[0029] The inner walls of the outer casing 1 and the front cover 2 are coated with a conductive coating. The conductive coating usually contains conductive metal powder, such as copper and silver. The paint film formed after drying has excellent conductivity. The conductive coating can serve as a protective energy absorption layer, providing excellent static conductivity and shielding protection. It can reflect and release static charges, protecting the device from electrostatic damage.

[0030] The outer surface of the inner wall of the outer shell 1 is provided with a sealing ring groove, and the inner cavity of the sealing ring groove is provided with a conductive waterproof sealing ring 17. The heat sink 3 is a passive heat dissipation device, usually made of metal material. Its working principle is to increase the heat dissipation area to improve the heat conduction efficiency. The heat sink 3 is in close contact with the heat-generating element, and the heat generated by the element is quickly conducted to the surface of the heat sink 3 and dissipated into the air through natural convection. The cooling fan 4 is an active heat dissipation device.

[0031] Screws are provided around the front of the cooling fan 4, and the back of the screws penetrates through the back of the cooling fan 4 and is fixed to the front of the heat sink 3. The fan blades are driven to rotate by a motor, which forces the air to convect and accelerate the dissipation of heat. The cooling fan 4 is usually used in conjunction with the heat sink 3 to form a so-called "air-cooled" heat dissipation system. In this system, the airflow generated by the cooling fan 4 can effectively remove the heat from the surface of the heat sink 3, further improving the heat dissipation efficiency. The cooling fan 4 is suitable for high power consumption or devices that need to work continuously for a long time.

[0032] There are six input / output interfaces 11, which are distributed sequentially on the upper and lower sides of the outer casing 1. The hinge seat 16 facilitates the assembly of the outer casing 1 and the front cover 2, increasing the stability of the assembly. The waterproof sealing ring 17 is mainly used to prevent the intrusion of liquids, gases or solids, providing watertightness and airtightness. It is widely used in various applications requiring sealing to ensure the normal operation and safety of the internal components of the outer casing 1 and the front cover 2. The waterproof sealing ring 17 is used for insulation and sealing, protecting the electronic components inside the outer casing 1 and the front cover 2 from moisture and water. The sealing ring groove facilitates the assembly of the waterproof sealing ring 17.

[0033] In use, conductive coatings are applied to the inner walls of both the outer casing 1 and the front cover 2. These conductive coatings effectively absorb, conduct, and attenuate electromagnetic waves, thus shielding against electromagnetic interference. This is crucial for controlling the induction and radiation of electric fields, magnetic fields, and electromagnetic waves. The conductive coating typically contains conductive metal powders, such as copper and silver. The resulting film after drying has excellent conductivity. The conductive coating acts as a protective energy absorption layer, providing excellent static conductivity and shielding performance. It can reflect and release static charges, protecting the device from electrostatic damage. The heat sink 3 is a passive heat dissipation device, usually made of metal. Its working principle is to increase the heat dissipation area to improve heat conduction efficiency. The heat sink 3 is in close contact with the heat-generating element, rapidly conducting the heat generated by the element to the surface of the heat sink 3, and then dissipating the heat into the air through natural convection. The cooling fan 4 is an active heat dissipation device, driven by a motor to rotate the fan blades, forcibly dissipating heat. Convection air accelerates heat dissipation. The cooling fan 4 is usually used in conjunction with the heat sink 3 to form a so-called "air-cooled" heat dissipation system. In this system, the airflow generated by the cooling fan 4 can effectively remove the heat from the surface of the heat sink 3, further improving heat dissipation efficiency. The cooling fan 4 is suitable for high-power devices or devices that need to work continuously for a long time. The hinge seat 16 facilitates the assembly of the outer shell 1 and the front cover 2, increasing the stability of the assembly of the outer shell 1 and the front cover 2. The main function of the waterproof sealing ring 17 is to prevent the intrusion of liquids, gases or solids, and to provide water and air tightness. It is widely used in various occasions that require sealing to ensure the normal operation and safety of the internal components of the outer shell 1 and the front cover 2. The waterproof sealing ring 17 is used for insulation and sealing, protecting the electronic components inside the outer shell 1 and the front cover 2 from moisture and water. The sealing ring groove facilitates the assembly of the waterproof sealing ring 17.

[0034] All standard parts used in this application can be purchased from the market, and can be customized according to the description and drawings. The specific connection methods of each part adopt conventional methods such as bolts, rivets, and welding that are mature in the prior art. The machinery, parts and equipment adopt conventional models in the prior art. The control method is automatic control through a controller. The control circuit of the controller can be implemented by simple programming by those skilled in the art and is common knowledge in the field. Since this utility model is mainly used to protect mechanical devices, this utility model will not explain the control method and circuit connection in detail. The external controller mentioned in the specification can play a control role for the electrical components mentioned in this article, and the external controller is a conventional known device.

[0035] It should be noted that, in this document, the terms “comprising,” “including,” or any other variations thereof are intended to cover non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements includes not only those elements but also other elements not expressly listed, or elements inherent to such process, method, article, or apparatus.

[0036] It will be apparent to those skilled in the art that this invention is not limited to the details of the exemplary embodiments described above, and that it can be implemented in other specific forms without departing from the spirit or essential characteristics of this invention. Therefore, the embodiments should be considered illustrative and non-limiting in all respects, and the scope of this invention is defined by the appended claims rather than the foregoing description. Thus, it is intended that all variations falling within the meaning and scope of equivalents of the claims be included within this invention. No reference numerals in the claims should be construed as limiting the scope of the claims.

[0037] Furthermore, it should be understood that although this specification describes embodiments, not every embodiment contains only one independent technical solution. This narrative style is merely for clarity. Those skilled in the art should consider the specification as a whole, and the technical solutions in each embodiment can also be appropriately combined to form other embodiments that can be understood by those skilled in the art.

Claims

1. An integrated UAV ground reference station, comprising a shell (1) and a front cover (2), characterized in that: The front cover (2) is located on the front of the outer shell (1). Heat sinks (3) are provided on both the front of the front cover (2) and the back of the outer shell (1). A cooling fan (4) is provided on the front of the heat sink (3). A power module (5), an image transmission module (6), a flight control module (7), a conversion module (8), a data exchange module (9), and a satellite timing module (10) are arranged sequentially on the back of the inner cavity of the outer shell (1). There are two image transmission modules (6), and both are symmetrically arranged on the left side of the back of the inner cavity of the outer shell (1). The data exchange module (9) is located on the right side of the upper end of the image transmission module (6). The flight control module (7) is located on the right side of the inner cavity of the outer shell (1). The image transmission module (6) and data exchange module (9) are located on the right side. The conversion module (8) is located above the flight control module (7). The power module (5) is located on the left side of the conversion module (8). Input and output interfaces (11) are provided on the upper and lower sides of both sides of the outer shell (1). A dual-channel filter (12) and a power amplifier (13) are arranged sequentially on the back of the front cover (2). The dual-channel filter (12) is located above the power amplifier (13). The dual-channel filter (12) includes a single-channel filter (14) and a medium filter (15). The medium filter (15) is located in front of the single-channel filter (14).

2. The integrated UAV ground reference station according to claim 1, characterized in that: Hinges (16) are installed on both sides of the top of the front cover (2). The bottom of the hinges (16) is fixed to both sides of the top of the outer shell (1). The hinges (16) are made of metal.

3. An integrated UAV ground reference station according to claim 1, characterized in that: The inner walls of both the outer shell (1) and the front cover (2) are coated with a conductive coating.

4. An integrated UAV ground reference station according to claim 1, characterized in that: The outer surface of the inner wall of the outer shell (1) is provided with a sealing ring groove, and the inner cavity of the sealing ring groove is provided with a conductive waterproof sealing ring (17).

5. An integrated UAV ground reference station according to claim 1, characterized in that: Screws are provided around the front of the cooling fan (4), and the back of the screws penetrates through the back of the cooling fan (4) and is fixed to the front of the heat sink (3).

6. An integrated UAV ground reference station according to claim 1, characterized in that: The number of input / output interfaces (11) is six, and the six input / output interfaces (11) are distributed sequentially on the upper and lower sides of the outer shell (1).

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