Intelligent defense low-altitude safety comprehensive management and control integrated system
By introducing components such as lifting cylinders, adjustment screws and drive motors into the low-altitude safety integrated management and control integrated system, the position and height of the detection equipment are dynamically adjusted, and the problem of small detection range in the existing technology is solved and a wider low-altitude airspace detection is achieved .
Patent Information
- Application Number
- CN202421333599.6
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-06-12
- Publication Date
- 2025-01-14
- Estimated Expiration
- 2034-06-12
AI Technical Summary
The existing low-altitude safety integrated management and control integrated system has a small detection range due to the fixed direction and position of the detection probe, and it is impossible to conduct large-scale inspections of the surrounding low-altitude airspace.
An intelligent defense low-altitude safety integrated management and control system was designed, including control box, detection equipment and installation components. By lifting and lowering cylinders, adjustment screws, drive motors and other components, the height and position of the detection equipment are adjusted and the detection range is expanded.
By dynamically adjusting the position and height of the detection equipment, the detection range is significantly expanded and the detection effect is improved.
Smart Images
Figure CN222352009U_ABST
Abstract
Description
Technical Field
[0001] The utility model relates to the technical field of low-altitude safety management, and in particular to an intelligent defense low-altitude safety comprehensive management and control integrated system. Background Art
[0002] With the rapid development and widespread popularization of drone technology, incidents in which consumer-grade drones pose potential security threats to civil aviation, electricity, important national defense targets, etc. occur frequently. Therefore, it is now very important to control the safety of low-altitude airspace.
[0003] At present, since manual control of low altitude is difficult, most of the detection and warning of low-altitude drones are carried out through the use of detection agencies and corresponding integrated circuit systems.
[0004] However, when the above method is used, when the existing equipment detects low-altitude aircraft through the integrated safety management and control system, since the direction and position of the detection probe are fixed, the overall detection range will be small, and large-scale detection of the surrounding low-altitude airspace cannot be performed. Utility Model Content
[0005] The purpose of the utility model is to provide an intelligent defense low-altitude safety comprehensive management and control integrated system, which can allow users to adjust the detection range of the equipment accordingly according to actual operating conditions through the provided components, thereby expanding the overall detection range and achieving better results during detection.
[0006] To achieve the above-mentioned purpose, the utility model provides an intelligent defense low-altitude safety comprehensive management and control integrated system, including a control box and a detection device, the detection device is electrically connected to the control box, and also includes an installation component;
[0007] The mounting assembly includes an adjustment plate, a rotating bracket, a lifting frame, a supporting base, a driving component, an adjusting component and an auxiliary component; the adjusting plate is connected to the control box and to the detection device, the rotating bracket is slidably connected to the adjusting plate and is located on one side of the adjusting plate, the lifting frame is rotatably connected to the rotating bracket and is located on one side of the rotating bracket, the supporting base is slidably connected to the lifting frame and is located on one side of the lifting frame, the driving component is connected to the lifting frame, the adjusting component is connected to the adjusting plate, and the auxiliary component is connected to the adjusting plate.
[0008] Among them, the driving component includes a lifting cylinder, a sleeve gear, a driving gear and a driving motor, the output end of the lifting cylinder is connected to the lifting frame, and the lifting cylinder is fixedly installed on one side of the supporting base frame; the sleeve gear is fixedly connected to the rotating frame and is located on one side of the rotating frame; the driving gear is meshed with the sleeve gear and is rotatably installed on one side of the lifting frame; the output shaft of the driving motor is connected to the driving gear, and the driving motor is fixedly installed on one side of the lifting frame.
[0009] Wherein, the adjusting component includes an adjusting screw and an adjusting motor, the adjusting screw is threadedly connected to the adjusting plate and rotatably mounted on one side of the rotating bracket; the output shaft of the adjusting motor is connected to the adjusting screw, and the adjusting motor is fixedly mounted on one side of the rotating bracket.
[0010] Wherein, the lifting frame has a connecting boss and a mounting boss, wherein the connecting boss is located on a side of the lifting frame close to the supporting base frame; and the mounting boss is located on a side of the lifting frame close to the driving motor.
[0011] Among them, the auxiliary components include a battery box, a fixed bracket and a solar panel, the battery box is electrically connected to the control box and installed on one side of the adjustment plate; the fixed bracket is fixedly connected to the adjustment plate and is located on one side of the adjustment plate; the solar panel is electrically connected to the battery box and fixedly installed on one side of the fixed bracket.
[0012] The utility model provides an intelligent defense low-altitude safety comprehensive management and control integrated system, which drives the lifting frame through the lifting cylinder to adjust the detection height of the entire equipment. After that, the user can also drive the adjustment plate through the adjustment motor in cooperation with the adjustment screw according to the actual operation situation, so as to adjust the detection position of the control box and the detection equipment through the sliding of the adjustment plate. When performing the detection, the driving motor will drive the driving gear to rotate, and then drive the sleeve gear and the rotating bracket to rotate through the driving gear, so that the control box and the detection equipment can perform dynamic detection of the corresponding range, and realize that the user can make corresponding adjustments to the detection range of the equipment according to the actual operation situation through the provided components, thereby expanding the overall detection range, so that the effect is better when performing the detection. BRIEF DESCRIPTION OF THE DRAWINGS
[0013] In order to more clearly illustrate the embodiments of the present application or the technical solutions in the prior art, the drawings required for use in the embodiments or the description of the prior art are briefly introduced below.
[0014] Figure 1It is a schematic diagram of the overall structure of the intelligent defense low-altitude safety comprehensive management and control integrated system of the first embodiment of the utility model.
[0015] Figure 2 It is a side view of the entire intelligent defense low-altitude safety comprehensive management and control integrated system of the first embodiment of the utility model.
[0016] Figure 3 It is a structural schematic diagram of the driving component of the first embodiment of the utility model.
[0017] Figure 4 It is a schematic diagram of the overall structure of the intelligent defense low-altitude safety comprehensive management and control integrated system of the second embodiment of the utility model.
[0018] In the figure: 101-control box, 102-detection equipment, 103-adjustment plate, 104-rotating bracket, 105-lifting frame, 106-support base frame, 107-lifting cylinder, 108-set gear, 109-driving gear, 110-driving motor, 111-adjusting screw, 112-adjusting motor, 113-connecting boss, 114-mounting boss, 201-battery box, 202-fixed bracket, 203-solar panel. DETAILED DESCRIPTION
[0019] Embodiments of the present invention are described in detail below, and examples of the embodiments are shown in the accompanying drawings. The embodiments described below with reference to the accompanying drawings are exemplary and are intended to be used to explain the present invention, but should not be understood as limiting the present invention.
[0020] The first embodiment of the present application is:
[0021] See also Figures 1 to 3 ,in Figure 1 It is a schematic diagram of the overall structure of the intelligent defense low-altitude safety integrated management and control integrated system. Figure 2 It is a side view of the integrated system of intelligent defense low-altitude safety comprehensive management and control. Figure 3 It is a structural schematic diagram of the driving component.
[0022] The utility model provides an intelligent defense low-altitude safety comprehensive management and control integrated system: including a control box 101, a detection device 102 and an installation component, the installation component includes an adjustment plate 103, a rotating bracket 104, a lifting frame 105, a supporting base frame 106, a driving component, an adjusting component and an auxiliary component, the driving component includes a lifting cylinder 107, a sleeve gear 108, a driving gear 109 and a driving motor 110, the adjusting component includes an adjusting screw 111 and an adjusting motor 112, the lifting frame 105 has a connecting boss 113 and a mounting boss 114, and the above-mentioned solution solves the problem that when the existing equipment detects low-altitude aircraft through the safety comprehensive management and control integrated system, because the direction and position of the detection probe are fixed, the overall detection range is small, and a large-scale detection of the surrounding low-altitude airspace cannot be performed.
[0023] In this embodiment, the detection device 102 is electrically connected to the control box 101, and the detection device 102 and the control box 101 constitute an existing equipment body equipped with an integrated low-altitude safety comprehensive management and control integrated system. The corresponding detection module and the sensing module provided in the integrated system can complete the detection of aircraft in the low-altitude airspace, and then the detected aircraft can be forced to land or warned through the corresponding interference module, thereby completing the corresponding low-altitude airspace safety management and control.
[0024] The adjusting plate 103 is connected to the control box 101 and to the detecting device 102; the rotating bracket 104 is slidably connected to the adjusting plate 103 and is located on one side of the adjusting plate 103; the lifting frame 105 is rotatably connected to the rotating bracket 104 and is located on one side of the rotating bracket 104; the supporting base frame 106 is slidably connected to the lifting frame 105 and is located on one side of the lifting frame 105; the driving member is connected to the lifting frame 105; the adjusting member is connected to the adjusting plate 103; the auxiliary member is connected to the adjusting plate 103; the connecting boss 113 is located on a side of the lifting frame 105 close to the supporting base frame 106; the mounting boss 114 is located on a side of the lifting frame 105 close to the driving motor 110; The lowering frame 105 cooperates with the expenditure boss provided on the supporting base frame 106 through the connecting boss 113 provided at the bottom, so that the lifting frame 105 can slide on the supporting base, and the rotating bracket 104 is rotatably installed above the lifting frame 105, and the adjusting plate 103 is slidably installed on the rotating bracket 104, and the control box 101 and the detection device 102 are both installed on the adjusting plate 103, so that the user can adjust the detection position of the control box 101 and the detection device 102 by sliding the adjusting plate 103 on the rotating bracket 104, and then through the rotation of the rotating bracket 104, the control box 101 and the detection device 102 can be in a dynamic detection state during detection, so that the entire detection range is wider.
[0025] Secondly, the output end of the lifting cylinder 107 is connected to the lifting frame 105, and the lifting cylinder 107 is fixedly installed on one side of the supporting frame 106; the sleeve gear 108 is fixedly connected to the rotating bracket 104 and is located on one side of the rotating bracket 104; the driving gear 109 is meshed with the sleeve gear 108 and is rotatably installed on one side of the lifting frame 105; the output shaft of the driving motor 110 is connected to the driving gear 109, and the driving motor 110 is fixedly installed on one side of the lifting frame 105, and the output end of the lifting cylinder 107 is fixed to the bottom of the lifting frame 105, so that the user can directly control the lifting frame 105 through the lifting cylinder 107 The driving mechanism 106 is a method for driving a rotary table 104 to drive the rotary table 104. The driving mechanism 106 is a method for driving a rotary table 104 to drive the rotary table 104. The driving mechanism 106 is a method for driving a rotary table 104 to drive the rotary table 104. The driving mechanism 106 is a method for driving a rotary table 104 to drive the rotary table 104. The driving mechanism 106 is a method for driving a rotary table 104 to drive the rotary table 104.
[0026] At the same time, the adjusting screw 111 is threadedly connected to the adjusting plate 103 and is rotatably installed on one side of the rotating bracket 104; the output shaft of the adjusting motor 112 is connected to the adjusting screw 111, and the adjusting motor 112 is fixedly installed on one side of the rotating bracket 104. The adjusting screw 111 is adapted to the threaded hole provided on the adjusting plate 103, and the output shaft of the adjusting motor 112 is fixed to the adjusting screw 111. When the adjusting motor 112 drives the adjusting screw 111 to rotate, the adjusting plate 103 will slide under the action of the adjusting screw 111, thereby completing the corresponding drive of the adjusting plate 103.
[0027] When the intelligent defense low-altitude safety comprehensive management and control integrated system of this embodiment is in use, the lifting frame 105 is driven by the lifting cylinder 107 to adjust the detection height of the entire device. After that, the user can also drive the adjustment plate 103 through the adjustment motor 112 in cooperation with the adjustment screw 111 according to the actual operation situation, so as to adjust the detection position of the control box 101 and the detection device 102 by sliding the adjustment plate 103. When performing detection, the drive motor 110 will drive the drive gear 109 to rotate, and then drive the sleeve gear 108 and the rotating bracket 104 to rotate through the drive gear 109, so that the control box 101 and the detection device 102 can perform dynamic detection of the corresponding range, so that the user can adjust the detection range of the equipment according to the actual operation situation through the provided components, thereby expanding the overall detection range, so that the effect is better when performing detection.
[0028] Second embodiment:
[0029] See also Figure 4 , Figure 4 This is a schematic diagram of the overall structure of the intelligent defense low-altitude safety comprehensive management and control integrated system of the second embodiment. The auxiliary components provided by the utility model include a battery box 201, a fixed bracket 202 and a solar panel 203.
[0030] Among them, the power storage box 201 is electrically connected to the control box 101 and is installed on one side of the adjustment plate 103; the fixed bracket 202 is fixedly connected to the adjustment plate 103 and is located on one side of the adjustment plate 103; the solar panel 203 is electrically connected to the power storage box 201 and is fixedly installed on one side of the fixed bracket 202. The solar panel 203 is installed on one side of the adjustment plate 103 through the fixed bracket 202. The solar panel 203 can convert solar energy into electrical energy and transmit it to the power storage box 201, thereby providing energy for the detection system.
[0031] When using an intelligent defense low-altitude safety integrated management and control integrated system of the present embodiment, the solar energy can be converted into electrical energy through the solar panel 203, and then stored through the power storage box 201 and subsequently output for use, so that resources can be used more reasonably and effectively, greatly enhancing the practicality of the entire device.
[0032] What is disclosed above is only one or more preferred embodiments of the present application, and cannot be used to limit the scope of rights of the present application. Ordinary technicians in this field can understand that all or part of the processes of implementing the above embodiments and equivalent changes made according to the claims of the present application are still within the scope covered by the present application.
Claims
1. An intelligent defense low-altitude safety integrated management and control integrated system, comprising a control box and a detection device, wherein the detection device is electrically connected to the control box, and is characterized in that: Also included are mounting components; The mounting assembly includes an adjustment plate, a rotating bracket, a lifting frame, a supporting base, a driving component, an adjusting component and an auxiliary component; the adjusting plate is connected to the control box and to the detection device, the rotating bracket is slidably connected to the adjusting plate and is located on one side of the adjusting plate, the lifting frame is rotatably connected to the rotating bracket and is located on one side of the rotating bracket, the supporting base is slidably connected to the lifting frame and is located on one side of the lifting frame, the driving component is connected to the lifting frame, the adjusting component is connected to the adjusting plate, and the auxiliary component is connected to the adjusting plate.
2. The intelligent defense low-altitude safety integrated management and control integrated system as claimed in claim 1 is characterized in that: The driving component includes a lifting cylinder, a sleeve gear, a driving gear and a driving motor. The output end of the lifting cylinder is connected to the lifting frame, and the lifting cylinder is fixedly installed on one side of the supporting base frame; the sleeve gear is fixedly connected to the rotating frame and is located on one side of the rotating frame; the driving gear is meshed with the sleeve gear and is rotatably installed on one side of the lifting frame; the output shaft of the driving motor is connected to the driving gear, and the driving motor is fixedly installed on one side of the lifting frame.
3. The intelligent defense low-altitude safety integrated management and control integrated system as claimed in claim 1 is characterized in that: The adjusting component includes an adjusting screw and an adjusting motor. The adjusting screw is threadedly connected to the adjusting plate and rotatably mounted on one side of the rotating bracket. The output shaft of the adjusting motor is connected to the adjusting screw, and the adjusting motor is fixedly mounted on one side of the rotating bracket.
4. The intelligent defense low-altitude safety integrated management and control integrated system as claimed in claim 2 is characterized in that: The lifting frame has a connecting boss and a mounting boss. The connecting boss is located on a side of the lifting frame close to the supporting base frame; the mounting boss is located on a side of the lifting frame close to the driving motor.
5. The intelligent defense low-altitude safety integrated management and control integrated system as claimed in claim 1 is characterized in that: The auxiliary components include a battery box, a fixed bracket and a solar panel. The battery box is electrically connected to the control box and installed on one side of the adjustment plate; the fixed bracket is fixedly connected to the adjustment plate and is located on one side of the adjustment plate; the solar panel is electrically connected to the battery box and fixedly installed on one side of the fixed bracket.