Professional unmanned aerial vehicle-mounted sensing and task management computing device

Abstract

The utility model discloses a professional unmanned aerial vehicle-mounted sensing and task management computing device, which comprises an airborne bracket, damping mounting frames are mounted at four corners of the airborne bracket, a 5G expansion module is mounted on the airborne bracket, a main shell is mounted at the top of the 5G expansion module, and a task management module is mounted on the main shell. A front protective cover plate and a rear protective cover plate are movably installed on the two sides of the main shell respectively, a fan is installed in the center of the top of the main shell, a WIFI antenna support is installed above the fan, the WIFI antenna support is installed on the main shell, and a cooling fan guide plate is connected to the upper portion of the WIFI antenna support in a threaded mode. Therefore, hot air gathered on the main shell is driven to be discharged out of the device through the cooling fan guide plate, hot air flow in the device is reduced, the situation that the hot air flow in the device is continuously gathered, so that the temperature is too high, and operation of the device is affected is further avoided, the stability of the device is improved, and the working requirements of different working environments are met.

Description

Technical Field

[0001] The utility model relates to the technical field of task management computing devices, and in particular to a professional unmanned aerial vehicle onboard sensing and task management computing device. Background Art

[0002] In recent years, drones, as a new application platform, have accelerated the pace of drones towards intelligence along with the introduction of advanced robotics technology, creating unlimited possibilities for the application of drones in many fields. Among them, micro drones have been widely used in military and civilian fields such as reconnaissance and environment due to their small size, strong maneuverability, flexible operation and low cost. Since drones need to collect information in a large area in a short time and ensure real-time transmission of information, it is necessary to carry task management computing devices on drones to meet the real-time control of drones and effective data transmission.

[0003] Currently, most of the task management computing devices on the market have poor waterproof performance and are difficult to meet the working requirements in rainy weather. In addition, the existing task management computing devices with large computing power are often too large and heavy, and have poor heat dissipation. When mounted on a drone, it is easy to reduce the performance of the drone and affect the operation of the task management computing device itself, and cannot be applied to special working environments. Utility Model Content

[0004] The purpose of the utility model is to provide a professional unmanned aerial vehicle onboard sensing and task management computing device to solve the problems of poor waterproof performance, heavy weight and poor heat dissipation effect of the existing task management computing device mentioned in the above background technology.

[0005] To achieve the above-mentioned purpose, the utility model provides the following technical solutions: a professional unmanned aerial vehicle onboard perception and task management computing device, comprising an onboard bracket, shock-absorbing mounting frames are installed at the four corners of the onboard bracket, a 5G expansion module is installed on the onboard bracket, a main shell is installed on the top of the 5G expansion module, a front protective cover plate and a rear protective cover plate are movably installed on both sides of the main shell, a fan is installed at the top center of the main shell, a WIFI antenna bracket is installed above the fan, the WIFI antenna bracket is installed on the main shell, and a cooling fan guide plate is threadedly connected to the top of the WIFI antenna bracket.

[0006] Preferably, a plurality of fins are mounted on the main shell, the plurality of fins are evenly distributed around the main shell, and there is a spacing between two adjacent fins.

[0007] Preferably, a plurality of the fins form a notch at the top of the main shell, the fan, the WIFI antenna bracket and the cooling fan guide plate are all installed at the notch position, and the top of the cooling fan guide plate is flush with the tops of the plurality of fins.

[0008] Preferably, a connecting groove is provided at the center of the WIFI antenna bracket, the connecting groove is located directly above the fan, and the diameter of the connecting groove is larger than the diameter of the fan.

[0009] Preferably, a plurality of flow holes are provided on the heat dissipation fan guide plate, and the plurality of flow holes are distributed in a ring shape on the heat dissipation fan guide plate, and the ring-shaped distribution of the flow holes and the connecting groove and the center of the fan are on the same axis.

[0010] Preferably, a plurality of debugging interfaces are installed at both ends of the main shell body close to the front protective cover plate and the rear protective cover plate, and the front protective cover plate and the rear protective cover plate are threadedly connected to the main shell body by bolts.

[0011] Preferably, the airborne bracket is of a skeleton structure design, the main shell is made of AZ-31-B magnesium alloy, and the cooling fan guide plate is made of carbon fiber.

[0012] The beneficial effects of the utility model are:

[0013] In the utility model, the mainboard inside the device runs rapidly, causing the temperature inside the device to rise and gather on the main shell. At this time, the fan runs, thereby driving the hot air gathered on the main shell to be discharged from the device through the heat dissipation fan guide plate, thereby reducing the hot air flow in the device, and further avoiding the situation in which the hot air flow in the device continues to gather and causes the temperature to be too high to affect the operation of the device, thereby improving the stability of the device and meeting the working requirements of different working environments. BRIEF DESCRIPTION OF THE DRAWINGS

[0014] Figure 1 This is a front view structural diagram of a professional unmanned aerial vehicle-mounted sensing and mission management computing device proposed by the utility model;

[0015] Figure 2 This is a rear view structural diagram of a professional unmanned aerial vehicle-mounted perception and mission management computing device proposed by the utility model;

[0016] Figure 3 This is a schematic diagram of the exploded structure of a professional unmanned aerial vehicle-mounted perception and mission management computing device proposed by the utility model.

[0017] In the figure: 1. Airborne bracket; 2. Shock-absorbing mounting bracket; 3. 5G expansion module; 4. Main shell; 5. Front protective cover; 6. Rear protective cover; 7. Fan; 8. WIFI antenna bracket; 9. Cooling fan guide plate; 10. Fins; 11. Connecting groove; 12. Flow hole. DETAILED DESCRIPTION

[0018] The technical solutions in the embodiments of the present invention will be described clearly and completely below in conjunction with the drawings in the embodiments of the present invention. Obviously, the described embodiments are only part of the embodiments of the present invention, rather than all of the embodiments.

[0019] refer to Figure 1-3 A professional unmanned aerial vehicle sensing and task management computing device comprises an airborne bracket 1, shock-absorbing mounting brackets 2 are installed at the four corners of the airborne bracket 1, a 5G expansion module 3 is installed on the airborne bracket 1, a main shell 4 is installed on the top of the 5G expansion module 3, a front protective cover plate 5 and a rear protective cover plate 6 are movably installed on both sides of the main shell 4, a fan 7 is installed at the top center of the main shell 4, a WIFI antenna bracket 8 is installed above the fan 7, the WIFI antenna bracket 8 is installed on the main shell 4, and a cooling fan guide plate 9 is threadedly connected above the WIFI antenna bracket 8.

[0020] When the device is running, the mainboard inside it runs quickly, causing the temperature inside the device to rise and accumulate on the main shell 4. At this time, the fan 7 runs, thereby driving the hot air accumulated on the main shell 4 to be discharged from the device through the heat dissipation fan guide plate 9, thereby reducing the hot air flow in the device, and further avoiding the situation where the hot air flow in the device continues to accumulate and causes the temperature to be too high to affect the operation of the device, thereby improving the stability of the device and meeting the working requirements of different working environments.

[0021] Specifically, in the present embodiment, a plurality of fins 10 are mounted on the main shell 4, and the plurality of fins 10 are evenly distributed around the main shell 4, and there is a spacing between two adjacent fins 10, so that the hot air flow in the device can contact the plurality of fins 10, thereby dissipating the heat in the device through the plurality of fins 10, thereby reducing the heat in the device and further improving the heat dissipation performance of the device.

[0022] Specifically, in the present embodiment, a plurality of fins 10 form a slot at the top of the main shell 4, and the fan 7, the WIFI antenna bracket 8 and the cooling fan guide plate 9 are all installed at the slot position, and the top of the cooling fan guide plate 9 is flush with the tops of the plurality of fins 10, so that when the hot air that cannot be dissipated is gathered in the slot through the fins 10, the heat in the slot is guided out of the device through the cooling fan guide plate 9 by the rotation of the fan 7, thereby achieving the purpose of cooling the air in the slot.

[0023] Specifically, in the present embodiment, a connecting groove 11 is provided at the center of the WIFI antenna bracket 8, the connecting groove 11 is located directly above the fan 7, and the diameter of the connecting groove 11 is larger than the diameter of the fan 7, so that when the fan 7 is running, the hot air flow around the fan 7 can pass through the WIFI antenna bracket 8 through the connecting groove 11, thereby avoiding the WIFI antenna bracket 8 from blocking the air flow, causing the heat in the device to be unable to be discharged through the fan.

[0024] Specifically, in the present embodiment, a plurality of flow holes 12 are provided on the heat dissipation fan guide plate 9, and the plurality of flow holes 12 are distributed in a ring shape on the heat dissipation fan guide plate 9, and the ring-shaped distribution of flow holes 12 and the connecting groove 11 and the center of the fan 7 are on the same axis, so that the airflow around the fan 7 can be discharged from the device through the plurality of flow holes 12, thereby providing a flow channel for the discharge of the airflow, and further achieving the cooling effect of the device.

[0025] Specifically, in the present embodiment, a plurality of debugging interfaces 13 are installed at both ends of the main shell 4 close to the front protective cover plate 5 and the rear protective cover plate 6. The front protective cover plate 5 and the rear protective cover plate 6 are threadedly connected to the main shell 4 by bolts. The debugging interface 13 is protected by the setting of the front protective cover plate 5 and the rear protective cover plate 6, thereby preventing water flow and dust from contacting the debugging interface 13 and causing failure of the debugging interface 13. The connection method in which the front protective cover plate 5 and the rear protective cover plate 6 are threadedly connected to the main shell 4 by bolts enables the front protective cover plate 5 and the rear protective cover plate 6 to be flexibly installed or removed from the device, thereby facilitating the use of the debugging interface 13.

[0026] Specifically, in the present embodiment, the airborne bracket 1 is of a skeleton-type structural design, the main shell 4 is made of AZ-31-B magnesium alloy, and the cooling fan guide plate 9 is made of carbon fiber, so that the airborne bracket 1 can reduce the weight of the equipment through the skeleton-type structural design, increase the buffering between the UAV and the equipment, and improve the shock resistance of the equipment; the main shell 4 is made of AZ-31-B magnesium alloy to make the device have high thermal conductivity, light weight and corrosion resistance; the cooling fan guide plate 9 is made of carbon fiber to further reduce the weight of the device while maintaining its required hardness, thereby optimizing the endurance of the UAV.

[0027] The above are only preferred specific implementation methods of the utility model, but the protection scope of the utility model is not limited to this. Any technician familiar with the technical field within the technical scope disclosed by the utility model, who makes equivalent replacements or changes based on the technical scheme and utility model concept of the utility model, should be covered by the protection scope of the utility model.

Claims

1. A professional unmanned aerial vehicle onboard sensing and task management computing device, comprising an onboard bracket (1), characterized in that: Shock-absorbing mounting frames (2) are installed at the four corners of the airborne bracket (1), a 5G expansion module (3) is installed on the airborne bracket (1), a main housing (4) is installed on the top of the 5G expansion module (3), a front protective cover plate (5) and a rear protective cover plate (6) are movably installed on both sides of the main housing (4), a fan (7) is installed at the top center of the main housing (4), a WIFI antenna bracket (8) is installed above the fan (7), the WIFI antenna bracket (8) is installed on the main housing (4), and a heat dissipation fan guide plate (9) is threadedly connected to the top of the WIFI antenna bracket (8).

2. A professional unmanned aerial vehicle sensing and mission management computing device according to claim 1, characterized in that: A plurality of fins (10) are mounted on the main housing (4); the plurality of fins (10) are evenly distributed around the main housing (4), and a spacing exists between two adjacent fins (10).

3. A professional unmanned aerial vehicle sensing and mission management computing device according to claim 2, characterized in that: A plurality of the fins (10) form a notch at the top of the main housing (4); the fan (7), the WIFI antenna bracket (8) and the cooling fan guide plate (9) are all installed at the notch position, and the top end of the cooling fan guide plate (9) is flush with the top ends of the plurality of fins (10).

4. A professional unmanned aerial vehicle sensing and mission management computing device according to claim 1, characterized in that: A connecting groove (11) is provided at the center of the WIFI antenna bracket (8), the connecting groove (11) is located directly above the fan (7), and the diameter of the connecting groove (11) is greater than the diameter of the fan (7).

5. A professional unmanned aerial vehicle sensing and mission management computing device according to claim 1, characterized in that: The heat dissipation fan guide plate (9) is provided with a plurality of flow holes (12), which are distributed in an annular shape on the heat dissipation fan guide plate (9), and the annularly distributed flow holes (12) are located on the same axis as the connecting groove (11) and the center of the fan (7).

6. A professional unmanned aerial vehicle sensing and mission management computing device according to claim 1, characterized in that: A plurality of debugging interfaces (13) are installed at both ends of the main housing (4) close to the front protective cover plate (5) and the rear protective cover plate (6); the front protective cover plate (5) and the rear protective cover plate (6) are threadedly connected to the main housing (4) via bolts.

7. A professional unmanned aerial vehicle sensing and mission management computing device according to claim 1, characterized in that: The airborne bracket (1) is of skeleton-type structural design, the main housing (4) is made of AZ-31-B magnesium alloy, and the cooling fan guide plate (9) is made of carbon fiber.

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