Electric firing control device for police and explosion-proof unmanned aerial vehicle

Abstract

The utility model discloses an electric firing control device for a police and anti-explosion unmanned aerial vehicle, and relates to the technical field of unmanned aerial vehicle control equipment, the device comprises a mounting assembly, the mounting assembly is provided with a first connecting section and a second connecting section which are arranged in parallel, and an adjusting assembly is arranged in the first connecting section and comprises a driving motor and a transmission structure; the driving end of the driving motor is in meshed connection with the transmission structure; the bearing assembly comprises a bearing shell and a plurality of control units arranged in the bearing shell. A bearing cylinder is arranged on the bearing shell, and the control unit is used for controlling corresponding to-be-launched equipment to execute projection operation; a first connecting shaft and a second connecting shaft are arranged on the two sides of the bearing shell correspondingly. The first connecting shaft is connected with the transmission structure, and the second connecting shaft is rotationally connected with the second connecting section; the driving motor drives the transmission structure to rotate, so that the bearing assembly rotates relative to the mounting assembly, and the projection angle of the to-be-launched equipment is adjusted; the projection precision and the coverage range of the transmitting equipment can be improved.

Description

TECHNICAL FIELD

[0001] The present application generally relates to the technical field of unmanned aerial vehicle control devices, and particularly relates to a shock launch control device for police and explosion-proof unmanned aerial vehicles. BACKGROUND

[0002] In the field of police and explosion-proof, unmanned aerial vehicles are widely used in the launching of non-lethal weapons such as smoke bombs and tear gas bombs as an efficient and flexible equipment. The shock launch control device is usually installed at the bottom of the unmanned aerial vehicle or other suitable positions, which is generally composed of a circuit control system, an ignition mechanism, a power module, etc. The circuit control system is responsible for receiving and processing command signals from the flight control system or remote control device of the unmanned aerial vehicle. The ignition mechanism ignites the fuse of the ammunition such as smoke bombs and tear gas bombs quickly after receiving the shock signal. The power module provides the required power for the entire shock launch process, which is usually connected to the on-board power supply of the unmanned aerial vehicle, and some are equipped with independent small batteries. The circuit control system sends a shock signal to the ignition mechanism in the launcher to achieve the rapid ignition and launching of the ammunition. When the flight control system or remote control device of the unmanned aerial vehicle issues a launching command, the circuit control system of the shock launch control device generates a momentary high-voltage or large-current pulse. This pulse signal is transmitted to the ignition mechanism, causing the electric heating wire or electric detonator in the ignition mechanism to heat up, thereby igniting the fuse of the ammunition and triggering the launching of the ammunition. However, the existing shock launch controller lacks flexibility in operation and cannot meet the needs of complex and variable field conditions. Therefore, we propose a shock launch control device for police and explosion-proof unmanned aerial vehicles to solve the above problems. CONTENT OF THE INVENTION

[0003] In view of the above-mentioned defects or deficiencies in the prior art, it is desirable to provide a shock launch control device for police and explosion-proof unmanned aerial vehicles that improves the launching precision and coverage range of the launching equipment.

[0004] The present application provides a shock launch control device for police and explosion-proof unmanned aerial vehicles, comprising:

[0005] A mounting assembly is connected to the unmanned aerial vehicle, the mounting assembly has a first connecting section and a second connecting section arranged in parallel, and an installation space is formed between the first connecting section and the second connecting section. An adjusting assembly is arranged inside the first connecting section, the adjusting assembly comprises a driving motor and a transmission structure used in cooperation, and the driving end of the driving motor is engaged with the transmission structure.

[0006] A bearing assembly is arranged at the mounting space, and the bearing assembly comprises a bearing shell and a plurality of control units arranged inside the bearing shell; the bearing shell is provided with a bearing cylinder corresponding to the number of control units, and the bearing cylinder is used for mounting a to-be-launched device; the control unit and the to-be-launched device are in one-to-one correspondence and communication connection, and the control unit is used for controlling the corresponding to-be-launched device to perform a projection operation; the bearing shell is provided with a first connecting shaft and a second connecting shaft on both sides respectively; the first connecting shaft is connected with the transmission structure, and the second connecting shaft is rotationally connected with the second connecting section;

[0007] The driving motor drives the transmission structure to rotate, so that the bearing assembly rotates relative to the mounting assembly, thereby adjusting the projection angle of the to-be-launched device.

[0008] According to the technical scheme provided in the embodiment of the application, the mounting assembly comprises:

[0009] A first connecting piece, a second connecting piece and a third connecting piece, the first connecting piece and the second connecting piece are arranged at two ends of the third connecting piece respectively, and are arranged in parallel;

[0010] The side of the first connecting piece away from the third connecting piece is the first connecting section, and the inside of the first connecting section is hollow to form an accommodation chamber, and the accommodation chamber is used for mounting the adjusting assembly;

[0011] The side of the second connecting piece away from the third connecting piece is the second connecting section;

[0012] The third connecting piece is connected with the unmanned aerial vehicle through a quick release structure.

[0013] According to the technical scheme provided in the embodiment of the application, the transmission structure comprises:

[0014] The first bevel gear and the second bevel gear are engagedly connected, the first bevel gear is connected with a first spur gear through a connecting rod, a driving shaft of the driving motor is provided with a second spur gear, the first spur gear and the second spur gear are engagedly connected, and the second bevel gear penetrates through the accommodation chamber and is connected with the first connecting shaft.

[0015] According to the technical scheme provided in the embodiment of the application, the bearing shell comprises:

[0016] An upper shell and a lower shell are rotationally connected through a rotating shaft, a bearing space is formed between the upper shell and the lower shell, and the bearing space is used for mounting the control unit; when the control unit in the bearing shell is assembled, the upper shell and the lower shell are locked through a buckle structure;

[0017] The upper housing is also provided with a plurality of mounting grooves, which are used to mount the bearing cylinder.

[0018] According to the technical solution provided in the embodiments of this application, the lower housing has a receiving groove on its edge, and the receiving groove is filled with a sealing ring;

[0019] When the upper housing and the lower housing are in the locked state, the sealing ring is in contact with the edge surface of the upper housing.

[0020] The technical solution provided according to the embodiments of this application also includes:

[0021] The processing module is communicatively connected to the drive structure and all the control units. The processing module is used to control the start and stop of the drive structure and to control the corresponding control units to generate control commands. The control commands are used to guide the corresponding launch device to perform a projection operation.

[0022] According to the technical solution provided in the embodiments of this application, the upper shell and / or the lower shell are provided with a plurality of ventilation holes, and a filter screen is installed at the ventilation holes.

[0023] According to the technical solution provided in the embodiments of this application, thermally conductive silicone is provided between the lower housing and the control unit.

[0024] As can be seen from the above technical solution, this application has at least the following beneficial effects:

[0025] This application provides an electric firing control device for police and explosion-proof drones, comprising: a mounting assembly connected to the drone, the mounting assembly having a first connecting section and a second connecting section arranged in parallel, forming an installation space between the first connecting section and the second connecting section; an adjustment assembly inside the first connecting section, the adjustment assembly including: a drive motor and a transmission structure used in cooperation, the drive end of the drive motor and the transmission structure being meshed; a carrier assembly disposed at the installation space, the carrier assembly including: a carrier housing and a plurality of control units disposed inside the carrier housing; a carrier cylinder corresponding to the number of control units on the carrier housing, the carrier cylinder being used to mount the device to be launched; a one-to-one correspondence between the control units and the device to be launched and a communication connection, the control unit being used to control the corresponding device to be launched to perform a projection operation; a first connecting shaft and a second connecting shaft respectively provided on both sides of the carrier housing; the first connecting shaft being connected to the transmission structure, the second connecting shaft being rotatably connected to the second connecting section; the drive motor drives the transmission structure to rotate, causing the carrier assembly to rotate relative to the mounting assembly, thereby adjusting the projection angle of the device to be launched.

[0026] The application drives the transmission structure to rotate by the driving motor, realizes the rotation of the bearing assembly relative to the mounting assembly, and further adjusts the projection angle of the to-be-launched device. This design enables the unmanned aerial vehicle to flexibly change the launching angle according to the actual situation on the scene when performing a task, and accurately drops non-lethal weapons such as smoke bombs, tear gas bombs and the like into the target area, greatly improves the projection accuracy, expands the coverage range, and enhances the ability to cope with complex scenes. For example, when performing an anti-explosion task in a narrow street or a densely built-up area, the launching angle can be accurately adjusted to drop the tear gas bomb into the designated position to disperse the dangerous crowd, while avoiding unnecessary harm to the surrounding innocent personnel and facilities. BRIEF DESCRIPTION OF DRAWINGS

[0027] Other features, objects, and advantages of the application will become more apparent from the following detailed description of non-limiting embodiments made with reference to the drawings.

[0028] Figure 1 Structure diagram of the electric shock launching control device for police and anti-explosion unmanned aerial vehicle.

[0029] Figure 2 Structure diagram of the adjusting assembly.

[0030] Figure 3 Top view of the bearing shell.

[0031] Figure 4 Sectional view of the bearing shell.

[0032] Figure 5 Structure diagram of the lower shell.

[0033] Figure 6 Structure diagram of the upper shell.

[0034] Figure 7 Schematic diagram of the ventilation hole.

[0035] Figure 8 Principle diagram of the processing module.

[0036] Reference signs in the drawings: 1, driving motor; 2, bearing shell; 3, bearing cylinder; 4, first connecting shaft; 5, second connecting shaft; 6, first connecting piece; 7, second connecting piece; 8, third connecting piece; 9, first bevel gear; 10, second bevel gear; 11, first spur gear; 12, second spur gear; 13, upper shell; 14, lower shell; 15, sealing ring; 16, processing module; 17, ventilation hole; 18, quick release structure; 19, buckle structure. DETAILED DESCRIPTION

[0037] The application will be described in further detail below with reference to the drawings and embodiments. It can be understood that the specific embodiments described herein are only used to explain the related application, and not to limit the application. In addition, it should be noted that only parts related to the application are shown in the drawings for ease of description.

[0038] It should be noted that the embodiments in the present application and the features in the embodiments can be combined with each other without conflict. The present application will be described in detail below with reference to the drawings and embodiments.

[0039] As shown in Figure 1 The present application provides a structure diagram of a shock and explosion-proof unmanned aerial vehicle electric shock launch control device, which comprises:

[0040] The mounting assembly is connected with the unmanned aerial vehicle, and has a first connecting section and a second connecting section arranged in parallel, and a mounting space is formed between the first connecting section and the second connecting section; the first connecting section is internally provided with an adjusting assembly, which comprises: a driving motor 1 and a transmission structure used in cooperation, and the driving end of the driving motor 1 is meshed and connected with the transmission structure;

[0041] The bearing assembly is arranged at the mounting space, and comprises: a bearing shell 2 and a plurality of control units arranged in the bearing shell 2; the bearing shell 2 is provided with a bearing cylinder 3 corresponding in number to the control units, and the bearing cylinder 3 is used for mounting a to-be-launched device; the control units and the to-be-launched device are in one-to-one correspondence and communication connection, and the control units are used for controlling the corresponding to-be-launched device to perform a projection operation; the bearing shell 2 is respectively provided with a first connecting shaft 4 and a second connecting shaft 5 on both sides; the first connecting shaft 4 is connected with the transmission structure, and the second connecting shaft 5 is rotationally connected with the second connecting section;

[0042] The driving motor 1 drives the transmission structure to rotate, so that the bearing assembly rotates relative to the mounting assembly, thereby adjusting the projection angle of the to-be-launched device.

[0043] It should be noted that the mounting assembly has a first connecting section and a second connecting section arranged in parallel, and the mounting space formed between the two sections provides a position for the installation of the bearing assembly. The adjusting assembly is arranged in the first connecting section, and the adjusting assembly is composed of a driving motor 1 and a transmission structure. The driving motor serves as a power source, and its driving end is closely meshed with the transmission structure. When the driving motor 1 starts, it will transmit power to the transmission structure, and then drive the bearing assembly connected therewith to rotate.

[0044] The carrier assembly is installed within the mounting space of the mounting component. The carrier assembly includes a carrier housing 2 and multiple control units housed within the carrier housing 2. The carrier housing 2 has a number of carrier cylinders 3 corresponding to the number of control units, which are used to hold the devices to be launched, such as smoke grenades and tear gas grenades. Each control unit establishes a communication connection with the corresponding device to be launched, controlling the device to perform the projection operation. A first connecting shaft 4 and a second connecting shaft 5 are respectively provided on both sides of the carrier housing 2, coaxially arranged. The first connecting shaft 4 is connected to the transmission structure, and the second connecting shaft 5 is rotatably connected to the second connecting section of the mounting component. This connection method allows the carrier assembly to rotate on the mounting component. When the drive motor 1 starts, its drive end drives the transmission structure to rotate. Since the first connecting shaft 4 is connected to the transmission structure, the rotation of the transmission structure drives the first connecting shaft 4 to rotate, thereby causing the carrier assembly to rotate relative to the mounting component about the second connecting shaft 5. Simultaneously, the projection angle of the device to be launched, installed within the carrier cylinder 3, changes accordingly. In this way, the projection angle of the device to be launched can be flexibly adjusted according to the actual needs of police and explosion-proof scenarios, thereby improving the projection accuracy and coverage of the device and enabling it to cope with complex and ever-changing on-site situations.

[0045] Furthermore, such as Figure 1 , Figure 5 and Figure 6 As shown, the installation components include:

[0046] The first connector 6, the second connector 7, and the third connector 8 are respectively disposed at both ends of the third connector 8 and are arranged in parallel.

[0047] The side of the first connector 6 away from the third connector 8 is the first connecting section, which is hollow inside to form a receiving chamber for installing the adjustment component.

[0048] The side of the second connector 7 furthest from the third connector 8 is the second connecting segment;

[0049] The third connector 8 is connected to the drone via a quick-release structure 18.

[0050] It should be noted that the installation component mainly consists of a first connector 6, a second connector 7, and a third connector 8. The first connector 6 and the second connector 7 are located at the two ends of the third connector 8 and are arranged parallel to each other. This layout design provides a stable basic architecture for the subsequent installation and collaborative work of various components.

[0051] The side of the first connecting piece 6 away from the third connecting piece 8 is the first connecting section described above, which is hollow inside to form a receiving chamber for mounting the adjusting assembly, and the drive motor 1 and transmission structure and other components in the adjusting assembly play a key role in the angle adjustment of the electric shock launching control device. The first connecting piece 6 not only provides mounting space for the adjusting assembly, but also protects and supports these components to some extent, ensuring their stable operation. The side of the second connecting piece 7 away from the third connecting piece 8 is the second connecting section, which is arranged in parallel with the first connecting section. In the entire mounting assembly, the second connecting section mainly serves to connect with the bearing assembly. The second connecting shafts 5 on both sides of the bearing assembly are rotationally connected with the second connecting section, so that the bearing assembly can rotate relative to the mounting assembly, thereby realizing the adjustment of the projection angle of the to-be-launched device, which is an important connection node for the flexible adjustment function of the entire device. The third connecting piece 8 serves to connect the unmanned aerial vehicle in the mounting assembly, and the third connecting piece 18 is connected with the unmanned aerial vehicle through a quick release structure 18. The design of the quick release structure 18 greatly improves the convenience of installation and disassembly. In actual application scenarios, when the electric shock launching control device needs to be maintained, replaced, or upgraded, the staff can quickly disassemble the device from the unmanned aerial vehicle with the help of the quick release structure 18, saving time and labor costs. When installing, the device can also be quickly and accurately installed on the unmanned aerial vehicle, ensuring its stable connection and the reliability of the device during the flight of the unmanned aerial vehicle.

[0052] Here, the specific structure of the quick release structure 18 is, for example, two quick release pieces capable of being connected by clamping, one of which is installed on the unmanned aerial vehicle, and the other of which is installed on the third connecting piece 8, and the quick connection is achieved by clamping the two.

[0053] Further, as shown in Figure 2 , the transmission structure includes:

[0054] The first bevel gear 9 and the second bevel gear 10 are meshingly connected, the first bevel gear 9 is connected with the first spur gear 11 through a connecting rod, the drive shaft of the drive motor 1 is provided with a second spur gear 12, the first spur gear 11 and the second spur gear 12 are meshingly connected, and the second bevel gear 10 penetrates the receiving chamber and is connected with the first connecting shaft 4.

[0055] It should be noted that the transmission structure mainly consists of the first bevel gear 9, the second bevel gear 10, the first spur gear 11, the second spur gear 12, and the connecting rod and other components, which cooperate with each other to realize the transmission and conversion of power.

[0056] The first bevel gear 9 and the second bevel gear 10 are engaged with each other, and the engagement can change the direction of force transmission. In the transmission structure, the bevel gears are used to transmit the power of the driving motor in different directions to meet the mechanical structure and functional requirements of the device. When one of the bevel gears rotates, the other bevel gear engaged with it will rotate synchronously, thereby transmitting power to different axial directions. The first bevel gear 9 is connected to the first spur gear 11 through a connecting rod, and the second spur gear 12 is arranged on the driving shaft of the driving motor 1, and the first spur gear 11 and the second spur gear 12 are engaged with each other; when the driving motor 1 is started, the driving shaft of the driving motor 1 drives the second spur gear 12 to rotate, and due to the engagement characteristics of the spur gears, the rotation of the second spur gear 12 will drive the first spur gear 11 engaged with it to rotate. The first spur gear 11 drives the first bevel gear 9 to rotate through the connecting rod, thereby transmitting the power of the driving motor 1 to the bevel gear part. The second bevel gear 10 penetrates the accommodating chamber and is connected with the first connecting shaft 4; when the first bevel gear 9 drives the second bevel gear 10 to rotate, the second bevel gear 10 drives the first connecting shaft 4 to rotate. Because the first connecting shaft 4 is connected with the bearing shell 2 of the bearing assembly, the rotation of the first connecting shaft 4 drives the bearing assembly to rotate relative to the mounting assembly with the second connecting shaft 5 as the axis, thereby adjusting the projection angle of the to-be-launched device mounted in the bearing cylinder 3.

[0057] Further, as shown in Figure 3 and Figure 4 , the bearing shell 2 comprises:

[0058] The upper shell 13 and the lower shell 14 are rotatably connected through a rotating shaft, and a bearing space is formed between the upper shell 13 and the lower shell 14 for mounting the control unit; when the control unit in the bearing shell 2 is assembled, the upper shell 13 and the lower shell 14 are locked through a buckle structure.

[0059] A plurality of mounting grooves are further formed in the upper shell 13, and the mounting grooves are used to mount the bearing cylinder 3.

[0060] It should be noted that the bearing shell 2 is composed of the upper shell 13 and the lower shell 14, and the two are rotatably connected through a rotating shaft; this connection mode provides convenience for the installation and maintenance of the control unit. When assembling or overhauling the control unit, the upper shell 13 can be opened by rotating the rotating shaft, which is convenient for operation; after the operation is completed, the upper shell 13 is closed again to ensure the integrity and stability of the device.

[0061] When the upper shell 13 and the lower shell 14 are closed, a bearing space is formed between the two for installing the control unit. The control unit, as a key part of controlling the projection operation of the to-be-launched device, is safely and stably placed in the space to avoid external environmental interference and ensure its normal operation. The design of the bearing space is also conducive to centralized management and wiring of the control unit, making the overall device structure more compact and orderly. When the control unit in the bearing shell 2 is assembled, the upper shell 13 and the lower shell 14 are locked by a buckle structure. The design of the buckle structure can ensure that the upper and lower shells are tightly connected to prevent the shells from being separated due to vibration or other external forces during the flight of the unmanned aerial vehicle, affecting the normal work of the control unit and the to-be-launched device. At the same time, the buckle structure is simple to operate, facilitating workers to quickly complete the installation and disassembly of the shell and improving work efficiency.

[0062] In addition, a plurality of mounting grooves are formed on the upper shell 13, which are used to install the bearing cylinder 3. The bearing cylinder 3 is a component for placing the to-be-launched device, and the mounting grooves are adapted to the bearing cylinder 3, which can stably install the bearing cylinder 3 on the upper shell 13, ensure that the to-be-launched device is in the correct position before launching, and improve the launching accuracy. The design of multiple mounting grooves can also flexibly install different numbers and types of bearing cylinders 3 according to actual needs, enhancing the applicability of the device.

[0063] Further, as shown in Figure 5 The edge of the lower shell 14 is provided with a receiving groove, and the receiving groove is filled with a sealing ring 15.

[0064] When the upper shell 13 and the lower shell 14 are in the locked state, the sealing ring 15 is in contact with the edge of the upper shell 13.

[0065] It should be noted that in the actual use process of the electric shock control device, the unmanned aerial vehicle may fly in various environments, such as humid environment and dusty area. The sealing ring 15 can effectively block water vapor, dust, debris and other external impurities from entering the bearing shell 2. If these impurities enter, it may cause the control unit to short circuit and corrode, affecting the control of the control unit on each to-be-launched device, and even causing a safety accident. For example, water vapor may cause the electronic components of the control unit (circuit board, etc.) to short circuit, and excessive dust accumulation may affect heat dissipation, thereby affecting the performance and safety of the entire device.

[0066] When the upper shell 13 and the lower shell 14 are in the locked state, the sealing ring 15 is in close contact with the edge of the upper shell 13, forming an effective sealing barrier and further enhancing the sealing performance of the bearing shell 2. Through this sealing design, a relatively stable and clean environment can be created for the control unit inside the bearing shell 2, ensuring that the control unit can operate normally and that the electric shock control device can work reliably in various complex environments, thereby improving the stability and safety of the device.

[0067] Further, as shown in Figure 8 , it also comprises:

[0068] The processing module 16 is in communication connection with the driving structure and all the control units. The processing module 16 is used to control the start and stop of the driving structure and control the corresponding control unit to generate control instructions for guiding the corresponding to-be-launched device to perform the projection operation.

[0069] It should be noted that the processing module 16 is used to control the start and stop of the driving structure. In actual application, when it is needed to adjust the projection angle of the to-be-launched device, the processing module 16 sends a start instruction to the driving motor 1, the driving motor 1 is started to drive the transmission structure to rotate, and then the bearing assembly is rotated relative to the mounting assembly to realize the adjustment of the projection angle. When the angle adjustment is completed or the angle does not need to be continuously adjusted, the processing module 16 sends a stop instruction to stop the driving motor 1 from working. The accurate start and stop control ensures that the bearing assembly can be accurately adjusted to the required angle, and improves the adjustment accuracy of the projection angle of the to-be-launched device.

[0070] The processing module 16 is also used to control the corresponding control unit to generate control instructions. Each control unit is in communication connection with the corresponding to-be-launched device. The processing module 16 sends signals to different control units according to actual combat or task requirements to instruct them to generate specific control instructions. These control instructions are the key to guide the corresponding to-be-launched device to perform the projection operation. For example, in a police scene, when it is needed to launch a smoke bomb according to the on-site situation, the processing module 16 controls the control unit responsible for the launching of the smoke bomb to generate a launching instruction. After the control unit receives the instruction, it sends a signal to the launching device of the smoke bomb to trigger the launching action of the smoke bomb.

[0071] In addition, the processing module 16 comprehensively considers various information and coordinates the work of the driving structure and the control unit. First, according to the parameters set by the operator or the pre-written program, it is judged whether it is needed to adjust the projection angle of the to-be-launched device. If it is needed, the driving structure is controlled to start the angle adjustment. After the angle adjustment is completed, the corresponding control unit is controlled to launch the to-be-launched device according to the actual situation. In the whole process, the processing module 16 ensures the collaborative work of the driving structure and the control unit, and guarantees that the electric shock launching control device can efficiently and accurately complete the projection task. Moreover, it can be wirelessly controlled through the remote controller and the processing module 16. For example, the remote controller is in the form of a knob. One turn of the knob can launch one to-be-launched device, and continuous turns can realize the launching of all to-be-launched devices.

[0072] Further, as shown in Figure 7 , a plurality of ventilation holes 17 are formed in the upper shell 13 and / or the lower shell 14, and a filter screen is installed at the ventilation holes 17.

[0073] It should be noted that when the electric shock delivery control device is in operation, the electronic components such as the control unit will continuously run and generate heat. If the heat cannot be dissipated in time, it will cause the internal temperature of the device to be too high. The high temperature will affect the performance and stability of the electronic components, shorten their service life, and even cause malfunctions, affecting the normal operation of the entire device. The presence of the ventilation hole 17 allows air to circulate between the inside and outside of the device, bringing heat out of the device and thus reducing the internal temperature, ensuring that the electronic components work in a suitable temperature environment.

[0074] Although the ventilation hole can achieve air circulation and heat dissipation, there are small particles such as dust and impurities in the external environment. If these particles enter the inside of the device along with the air, they will accumulate on the circuit board of the control unit and the surface of the electronic components, possibly causing short circuits, poor contact, and other problems, which will also affect the normal operation of the device. The filter screen can effectively block these dust and impurities, allowing only air to enter the inside of the device through the ventilation hole, ensuring the heat dissipation effect while ensuring the cleanliness of the internal environment of the device and reducing the risk of malfunctions caused by the entry of impurities.

[0075] Further, heat-conducting silicone is provided between the lower housing 14 and the control unit.

[0076] Here, the heat-conducting silicone is a material with high heat-conducting performance, which has good heat conduction capacity. When heat-conducting silicone is provided between the lower housing 14 and the control unit, the heat generated by the control unit will be quickly transferred to the heat-conducting silicone. Since the heat-conducting silicone is in close contact with the lower housing 14, the heat will be quickly conducted to the lower housing 14 through the heat-conducting silicone. The lower housing 14 has a large surface area, which can more effectively dissipate heat to the surrounding environment, thus achieving the heat dissipation effect of the control unit and ensuring that the control unit is always within the appropriate operating temperature range.

[0077] The above description is only the preferred embodiment of the present application and the explanation of the technical principles applied. Those skilled in the art should understand that the scope of the invention involved in the present application is not limited to the technical solutions formed by the specific combination of the above technical features, and should also cover other technical solutions formed by any combination of the above technical features or their equivalent features without departing from the inventive concept. For example, the above features can be replaced with technical features disclosed in the present application (but not limited to) having similar functions to form technical solutions.

Claims

1. A taser launch control device for police and bomb disposal drones, characterized by, The utility model relates to a kind of unmanned aerial vehicle equipment, including: Mounting assembly, which is connected with unmanned aerial vehicle, the mounting assembly has the first connecting section and the second connecting section arranged in parallel, and the mounting space is formed between the first connecting section and the second connecting section; The first connecting section is internally provided with adjusting assembly, and the adjusting assembly includes: driving motor (1) and transmission structure used in cooperation, the driving end of the driving motor (1) is engaged with the transmission structure; Bearing assembly, which is provided at the mounting space, includes: bearing shell (2) and a plurality of control units provided inside the bearing shell (2);The bearing shell (2) is provided with a bearing cylinder (3) corresponding to the number of control units, and the bearing cylinder (3) is used for mounting the to-be-launched device;The control unit and the to-be-launched device are one-to-one correspondence and communication connection, and the control unit is used for controlling the corresponding to-be-launched device to execute projection operation;The first connecting shaft (4) and the second connecting shaft (5) are respectively arranged on both sides of the bearing shell (2);The first connecting shaft (4) is connected with the transmission structure, and the second connecting shaft (5) is rotatably connected with the second connecting section; The transmission structure is driven to rotate by the driving motor (1), so that the bearing assembly rotates relative to the mounting assembly, thereby adjusting the projection angle of the to-be-launched device.

2. The electric shock launching control device for police and anti-explosion drones according to claim 1, characterized in that, The mounting assembly includes: First connecting piece (6), second connecting piece (7) and third connecting piece (8), the first connecting piece (6) and the second connecting piece (7) are respectively arranged at both ends of the third connecting piece (8), and are arranged in parallel; The side of the first connecting piece (6) away from the third connecting piece (8) is the first connecting section, and the inside is hollow to form a containing chamber, and the containing chamber is used for mounting the adjusting assembly; The side of the second connecting piece (7) away from the third connecting piece (8) is the second connecting section; The third connecting piece (8) is connected with unmanned aerial vehicle through quick release structure (18).

3. The electric shock launching control device for police and anti-explosion drones according to claim 2, characterized in that, The transmission structure includes: Engaged first bevel gear (9) and second bevel gear (10), the first bevel gear (9) is connected with first spur gear (11) through connecting rod, the driving shaft of the driving motor (1) is provided with second spur gear (12), the first spur gear (11) and the second spur gear (12) are engaged, and the second bevel gear (10) penetrates the containing chamber and is connected with the first connecting shaft (4).

4. The electric shock launching control device for police and anti-explosion drones according to claim 1, characterized in that, The bearing shell (2) includes: Upper shell (13) and lower shell (14), which are rotatably connected through a rotating shaft, and the bearing space is formed between the upper shell (13) and the lower shell (14) for mounting the control unit;When the control unit in the bearing shell (2) is assembled, the upper shell (13) and the lower shell (14) are locked by buckle structure; A plurality of mounting grooves are further formed in the upper shell (13), and the mounting grooves are used for mounting the bearing cylinder (3).

5. The electric shock launching control device for police and anti-explosion drones according to claim 4, characterized in that, The edge of the lower shell (14) is provided with a containing groove, and the containing groove is filled with a sealing ring (15). When the upper shell (13) and the lower shell (14) are in the locked state, the sealing ring (15) is in contact with the edge surface of the upper shell (13).

6. The electric shock launching control device for police and anti-explosion drones according to claim 1, characterized in that, Also comprising: A processing module (16) in communication connection with the driving motor (1) and all the control units, used for controlling the driving motor (1) to start and stop and controlling the corresponding control units to generate control instructions for guiding the corresponding to-be-launched device to perform projection operation.

7. The electric shock launching control device for police and anti-explosion drones according to claim 4, characterized in that, A plurality of ventilation holes (17) are formed on the upper shell (13) and / or the lower shell (14), and a filter screen is installed at the ventilation holes (17).

8. The electric shock launching control device for police and anti-explosion drones according to claim 7, characterized in that, Heat-conducting silica gel is arranged between the lower shell (14) and the control unit.

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