Unmanned aerial vehicle launching controller

Abstract

The utility model discloses an unmanned aerial vehicle launch controller which comprises a shell, a launch controller body fixedly installed at the bottom of the shell, a cover plate clamped at the upper end of the shell, movable plates and a heat dissipation copper sheet, the movable plates are connected to the left side and the right side of the upper end of the shell in a sliding mode respectively, and the heat dissipation copper sheet is embedded into the bottom of the shell. The heat dissipation copper sheet and the emission controller body are arranged in an attached mode, and the dustproof net is arranged at the front end of the shell in an attached mode. According to the unmanned aerial vehicle launching controller, heat in the shell can be assisted to be dissipated outwards through the arrangement of a heat dissipation copper sheet and heat dissipation fins, the heat dissipation effect is very good, the cover plate and the shell can be conveniently detached through the arrangement of a fixed column and a movable plate, and therefore rapid maintenance and overhaul can be conveniently conducted between the launching controller body and the shell; and the dustproof net is attached to the front side of the shell, dust is prevented from entering the shell, and the dustproof net can be conveniently detached and cleaned.

Description

Technical Field

[0001] The utility model relates to the technical field related to UAV launch, in particular to a UAV launch controller. Background Art

[0002] A drone is an unmanned aerial vehicle controlled by a radio remote control device or its own program control device. The use of drones is becoming more and more widespread. When launching a drone, it is necessary to use a corresponding drone launch controller.

[0003] For example, the patent authorization announcement number CN218585205U, the authorization announcement date is, discloses a drone cluster launch controller, which belongs to the field of drone cluster launch technology. The drone cluster launch controller includes a shell, both sides of the shell are fixedly connected with a mounting plate, both sides of the shell are provided with ventilation holes, the interior of the shell is provided with a circuit board, the circuit board is respectively provided with a central processing unit, a communication module, an inflation control module, an air pressure detection module and a launch control module, and the communication module, inflation control module, air pressure detection module and launch control module are all electrically connected to the central processing unit. The drone cluster launch controller, through the cooperation between the central processing unit, the communication module, the inflation control module, the air pressure detection module and the launch control module, can first detect the air pressure when the drone is launched. If the air pressure is too low, the air replenishment program is started, so that the drone launch has the appropriate air pressure, reducing the impact on the drone launch speed;

[0004] However, the existing technology has the problem that it is not convenient to quickly disassemble and assemble the transmitter controller. When the controller fails, it is not convenient to disassemble and maintain it in time. In addition, the heat dissipation is closely connected to the fan, and the actual heat dissipation effect is poor. When the dust screen is removed for cleaning, the dust screen is closely connected to the shell by magnetic attraction. Although it is convenient to disassemble, the fastening is poor and it is easy to fall off. For example, the comparative patents listed above have such problems.

[0005] To this end, we proposed a drone launch controller to solve the above problems. Utility Model Content

[0006] The purpose of the present utility model is to provide a UAV launch controller to solve the problems raised in the above-mentioned background technology, such as the inconvenience in quickly disassembling and assembling the launch controller, the inconvenience in timely disassembling and maintaining the controller when a fault occurs, the heat dissipation is closely dependent on the fan, and the actual heat dissipation effect is poor. When the dust net is removed for cleaning, the dust net and the shell are closely limited by magnetic attraction. Although it is convenient to disassemble, the tightness is poor and it is easy to fall off.

[0007] To achieve the above-mentioned object, the present invention provides the following technical solution: a UAV launch controller, comprising a housing, a launch controller body fixedly mounted on the bottom of the housing, and a cover plate engaged with the upper end of the housing;

[0008] Also includes:

[0009] A movable plate, wherein the movable plate is slidably connected to the left and right sides of the upper end of the shell, and the movable plate is combined with the protrusion and the fixed column to limit the position between the cover plate and the shell;

[0010] A heat dissipation copper sheet, the heat dissipation copper sheet being embedded in the bottom of the housing and being fitted to the transmitter controller body, the heat dissipation copper sheet being provided with heat dissipation fins at equal intervals at the lower end of the heat dissipation copper sheet, and the lower ends of the heat dissipation fins extending outward from the outer side of the housing;

[0011] Wherein, a cooling fan is fixedly installed at the rear end of the housing;

[0012] The dustproof net is fitted on the front end of the shell and placed on the outside of the heat dissipation slot. The dustproof net and the heat dissipation slot are limited by an installation mechanism, and the installation mechanism drives the dustproof net to form a disassembly structure at the front end of the shell. The dustproof net is inserted in the middle of the upper support plate and the lower support plate.

[0013] Preferably, the left and right sides of the lower end of the cover plate are fixedly connected with fixing columns, and the sides of the fixing columns are provided with fixing holes.

[0014] Preferably, a spring is provided between the movable plate and the housing, and the movable plate is sleeved on the outside of the fixed column. A protrusion is fixedly connected to the inner side of the movable plate, and the protrusion is inserted into the fixing hole.

[0015] Preferably, a heat dissipation slot is provided on the front side of the shell, and an upper support plate is fixedly connected to the upper end of the front side of the shell, and a lower support plate is fixedly connected to the lower end of the front side of the shell.

[0016] Preferably, the mounting mechanism includes a movable frame hingedly connected to the front side of the upper support plate, a connecting column for limiting, a fixed rod fixedly connected to the lower end of the movable frame, an auxiliary plate fixedly connected to the upper end of the mounting mechanism, and a fixed cap for locking and limiting.

[0017] Preferably, the movable frame is snap-connected to the connecting columns, and the connecting columns are fixedly connected to the left and right ends of the dustproof net respectively.

[0018] Preferably, the fixing rod is connected to the auxiliary plate by a slot, and the lower end of the auxiliary plate is threadedly connected to a fixing cap.

[0019] Preferably, the fixing cap is fitted on the lower end of the auxiliary plate.

[0020] Compared with the prior art, the beneficial effects of the present invention are as follows: the UAV launch controller can assist in dissipating the heat in the shell outwards by providing the heat dissipation copper sheet and the heat dissipation fins, and the heat dissipation effect is very good. The provision of the fixed column and the movable plate facilitates the disassembly of the cover plate and the shell, thereby facilitating rapid maintenance and repair between the launch controller body and the shell. The dustproof net is fitted on the front side of the shell to prevent dust from entering the shell, and the provision of the mounting mechanism facilitates the disassembly and cleaning of the dustproof net.

[0021] 1. It is equipped with heat dissipation copper sheet, heat dissipation fins and heat dissipation fan. The heat dissipation copper sheet is attached to the lower end of the transmitter controller body, and the heat dissipation fins extend outward from the outer shell. Combined with the setting of the heat dissipation fan, it can help dissipate the heat inside the shell to the outside, and the actual heat dissipation effect is very good.

[0022] 2. It is equipped with a fixed column and a movable plate, which are slidably connected to the upper end of the shell, and the movable plate and the fixed column are symmetrically arranged on the left and right sides of the upper end of the shell, so as to facilitate the disassembly between the cover and the shell and the maintenance and repair of the launch controller body;

[0023] 3. It is equipped with a dustproof net and an installation mechanism. The setting of the dustproof net can achieve a good dustproof effect. Combined with the setting of the installation mechanism, it is convenient to install and position the dustproof net, and it is also convenient to disassemble and clean the dustproof net. BRIEF DESCRIPTION OF THE DRAWINGS

[0024] Figure 1 This is a schematic diagram of the overall structure of the utility model;

[0025] Figure 2 This is a schematic diagram of the front view cutaway structure of the utility model;

[0026] Figure 3 This is a schematic diagram of the exploded structure of the housing, heat dissipation copper sheet, heat dissipation fins and heat dissipation fan of the utility model;

[0027] Figure 4 This is a schematic diagram of the exploded structure of the movable plate, protrusions and fixed columns of the utility model;

[0028] Figure 5 This is a schematic diagram of the exploded structure of the housing, cover, heat sink and dust screen of the utility model;

[0029] Figure 6 This is a schematic diagram of the overall structure of the installation mechanism of the utility model.

[0030] In the figure: 1. Housing; 2. Transmitter controller body; 3. Heat dissipation copper sheet; 4. Heat dissipation fins; 5. Cover plate; 6. Fixing column; 7. Fixing hole; 8. Movable plate; 9. Spring; 10. Bump; 11. Heat dissipation slot; 12. Dust screen; 13. Upper support plate; 14. Lower support plate; 15. Mounting mechanism; 16. Movable frame; 17. Connecting column; 18. Fixing rod; 19. Auxiliary plate; 20. Fixing cap; 21. Cooling fan. DETAILED DESCRIPTION

[0031] The following will be combined with the drawings in the embodiments of the present invention to clearly and completely describe the technical solutions in the embodiments of the present invention. Obviously, the embodiments described are only part of the embodiments of the present invention, not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by ordinary technicians in this field without making creative efforts are within the scope of protection of the present invention.

[0032] See also Figures 1-6 , the utility model provides the following technical solutions.

[0033] Embodiment 1: In order to solve the problem in the prior art that it is inconvenient to quickly disassemble and assemble the launch controller, and it is inconvenient to disassemble and maintain the controller in time when a fault occurs, this embodiment adopts the following technical scheme: a drone launch controller, provided with a shell 1, a launch controller body 2, a cover plate 5, a fixing column 6, a fixing hole 7, a movable plate 8, a spring 9 and a protrusion 10. The launch controller body 2 in this scheme has the same structure as the existing launch controller, including a central processing unit, a communication module and a launch control module, etc. It is an existing mature technology and is well known to those skilled in the art. It will not be described in detail here. The movable plate 8 is slidably connected to the left and right sides of the upper end of the shell 1, and the movable plate 8 is combined with the protrusion 10 and the fixing column 6 to limit the position between the cover plate 5 and the shell 1. The left and right sides of the lower end of the cover plate 5 are fixedly connected with the fixing column 6, and the side of the fixing column 6 is provided with a fixing hole 7, and a spring 9 is provided between the shell 1, and the movable plate 8 is sleeved on the outside of the fixing column 6, and the inner side of the movable plate 8 is fixedly connected with the protrusion 10, and the protrusion 10 is inserted into the fixing hole 7. Figure 1 、 Figure 2 and Figure 4As shown, the launch controller body 2 is fixedly installed in the shell 1 by bolts, and then by pressing the movable plate 8, the movable plate 8 slides with the shell 1, and the movable plate 8 squeezes the spring 9, causing the spring 9 to undergo elastic deformation, and then the cover plate 5 is engaged with the upper end of the shell 1. At the same time, the cover plate 5 drives the fixing column 6 to be placed in the middle of the movable plate 8, and then the movable plate 8 is directly released. At this time, the spring 9 restores its elastic deformation, driving the movable plate 8 to slide with the shell 1, so that the movable plate 8 drives the protrusion 10 to be inserted into the fixing hole 7, thereby facilitating the limiting of the cover plate 5 and the shell 1 and facilitating installation. Moreover, when a failure occurs in the launch controller body 2, the cover plate 5 can be removed from the upper end of the shell 1 by performing the reverse operation on the above operation, thereby facilitating maintenance and repair of the launch controller body 2.

[0034] Example 2: The existing UAV launch controller relies on the fan to heat the air, but the actual heat dissipation effect is poor. Therefore, a heat dissipation copper sheet 3, heat dissipation fins 4, heat dissipation slots 11 and a heat dissipation fan 21 are provided. Figure 2 and Figure 3 As shown, the cooling fan 21 is fixedly installed at the rear end of the shell 1, and the cooling fan 21 is used to blow air to the launch controller body 2 to achieve heat dissipation. At the same time, the heat dissipation groove 11 is opened on the front side of the shell 1, which can quickly dissipate the heat inside the shell 1 to the outside, and the heat dissipation copper sheet 3 is embedded in the bottom of the shell 1, and the heat dissipation copper sheet 3 and the launch controller body 2 are fitted together. The lower end of the heat dissipation copper sheet 3 is provided with heat dissipation fins 4 at equal intervals, and the lower end of the heat dissipation fins 4 extends out of the outside of the shell 1. Through the setting of the heat dissipation copper sheet 3 and the heat dissipation fins 4, the heat inside the shell 1 can be assisted to dissipate outward, thereby improving the actual heat dissipation effect and high practicality.

[0035] The dustproof net 12 is convenient to disassemble, but the tightness is poor and it is easy to fall off. Therefore, a dustproof net 12, an upper support plate 13, a lower support plate 14 and a mounting mechanism 15 are provided. The mounting mechanism 15 includes a movable frame 16 hingedly connected to the front side of the upper support plate 13, a connecting column 17 for limiting, a fixing rod 18 fixedly connected to the lower end of the movable frame 16, an auxiliary plate 19 fixedly connected to the upper end of the mounting mechanism 15 and a fixing cap 20 for locking and limiting. The movable frame 16 is snap-fitted to the connecting column 17, and the connecting column 17 is fixedly connected to the left and right ends of the dustproof net 12 respectively. The fixing rod 18 is connected to the auxiliary plate 19 by a slot, and the lower end of the auxiliary plate 19 is threadedly connected to the fixing cap 20, and the fixing cap 20 is fitted at the lower end of the auxiliary plate 19. The provision of the dustproof net 12 can prevent external dust from entering the housing 1 during ventilation and heat dissipation. Figure 5 and Figure 6As shown, when there is too much dust adsorbed on the dustproof net 12, the fixing cap 20 threadedly connected to the outer surface of the fixing rod 18 can be rotated, the fixing cap 20 and the fixing rod 18, and then the movable frame 16 is flipped outward, and the movable frame 16 and the upper support plate 13 are rotated. The movable frame 16 is disengaged from the connecting column 17, and at the same time, the movable frame 16 drives the fixing rod 18 to disengage from the auxiliary plate 19, thereby loosening the limit on the dustproof net 12, and then pulling the dustproof net 12 to move the dustproof net 12 out from the middle of the upper support plate 13 and the lower support plate 14, thereby facilitating the disassembly and cleaning of the dustproof net 12 to prevent the dustproof net 12 from being blocked during long-term use.

[0036] Although the embodiments of the present invention have been shown and described, it will be understood by those skilled in the art that various changes, modifications, substitutions and variations may be made to these embodiments without departing from the principles and spirit of the present invention, and the scope of the present invention is defined by the appended claims and their equivalents.

Claims

1. A UAV launch controller, comprising a housing (1), a launch controller body (2) fixedly mounted on the bottom of the housing (1), and a cover (5) engaged with the upper end of the housing (1); It is characterized in that Also includes: A movable plate (8), wherein the movable plate (8) is slidably connected to the left and right sides of the upper end of the housing (1), and the movable plate (8) is combined with the protrusion (10) and the fixed column (6) to limit the position between the cover plate (5) and the housing (1); a heat dissipation copper sheet (3), wherein the heat dissipation copper sheet (3) is embedded in the bottom of the housing (1), and the heat dissipation copper sheet (3) and the emission controller body (2) are arranged in a close fit, and heat dissipation fins (4) are arranged at equal intervals at the lower end of the heat dissipation copper sheet (3), and the lower ends of the heat dissipation fins (4) extend outward from the housing (1); Wherein, a heat dissipation fan (21) is fixedly installed at the rear end of the housing (1); A dustproof net (12) is fitted on the front end of the housing (1), and the dustproof net (12) is placed on the outside of the heat dissipation slot (11). The dustproof net (12) and the heat dissipation slot (11) are limited by a mounting mechanism (15), and the mounting mechanism (15) drives the dustproof net (12) to form a disassembly structure at the front end of the housing (1). The dustproof net (12) is plugged into the middle of the upper support plate (13) and the lower support plate (14).

2. The UAV launch controller according to claim 1, characterized in that: The left and right sides of the lower end of the cover plate (5) are fixedly connected with fixing columns (6), and the sides of the fixing columns (6) are provided with fixing holes (7).

3. The UAV launch controller according to claim 1, characterized in that: A spring (9) is provided between the movable plate (8) and the housing (1), and the movable plate (8) is sleeved on the outside of the fixed column (6). A protrusion (10) is fixedly connected to the inside of the movable plate (8), and the protrusion (10) is inserted into the fixed hole (7).

4. The UAV launch controller according to claim 1, characterized in that: A heat dissipation slot (11) is provided on the front side of the housing (1), and an upper support plate (13) is fixedly connected to the upper end of the front side of the housing (1), and a lower support plate (14) is fixedly connected to the lower end of the front side of the housing (1).

5. The UAV launch controller according to claim 1, characterized in that: The mounting mechanism (15) comprises a movable frame (16) hingedly connected to the front side of the upper support plate (13), a connecting column (17) for limiting position, a fixing rod (18) fixedly connected to the lower end of the movable frame (16), an auxiliary plate (19) fixedly connected to the upper end of the mounting mechanism (15), and a fixing cap (20) for locking and limiting position.

6. The UAV launch controller according to claim 5, characterized in that: The movable frame (16) is snap-connected to the connecting column (17), and the connecting column (17) is fixedly connected to the left and right ends of the dustproof net (12).

7. The UAV launch controller according to claim 5, characterized in that: The fixing rod (18) and the auxiliary plate (19) are connected by a slot, and the lower end of the auxiliary plate (19) is threadedly connected with a fixing cap (20).

8. The UAV launch controller according to claim 7, characterized in that: The fixing cap (20) is fitted on the lower end of the auxiliary plate (19).

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