Concealed defense radar
By designing a concealed defense radar with components such as rotating seats, hinges, adjustment seats and telescopic rods, the problem of inconvenient adjustment of radar monitoring angles in the prior art is solved, and flexible adjustment of radar plate angles and expansion of monitoring ranges are achieved.
Patent Information
- Application Number
- CN202421417840.3
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-06-20
- Publication Date
- 2025-03-28
- Estimated Expiration
- 2034-06-20
AI Technical Summary
The existing concealed defense radar used for low-altitude aircraft detection is inconvenient to adjust the radar's monitoring angle when used, making the radar's monitoring range relatively fixed.
A concealed defense radar including support columns, adjustment components, fixing components and support components is designed. Through components such as rotating seats, hinges, adjustment seats and telescopic rods, the angle adjustment of the radar plate is realized and the monitoring range is expanded.
By adjusting the angle of the radar plate, the radar monitoring range is significantly increased, the problem of fixed radar monitoring range is solved, and the flexibility and adaptability of the radar are improved.
Smart Images

Figure CN222687823U_ABST
Abstract
Description
Technical Field
[0001] The utility model relates to the technical field of radars, in particular to a concealed defense radar. Background Art
[0002] Defense radar involves the commander's judgment, task allocation, and target strike according to actual needs. However, the environment for detecting aircraft may be relatively poor and the ground may be uneven, which may cause the radar to deviate, and thus may lead to errors in the radar detection area.
[0003] The existing announcement number CN220525991U discloses a concealed defense radar for low-altitude aircraft detection, including: a plurality of fixing components are arranged on the side of the support column, the fixing component is used to fix the support column, a sliding component is arranged between the fixing component and the support column, the sliding component is used to place the fixing component, a storage component is arranged between the support plate and the radar plate, the storage component is used to store the radar plate, and the storage component is threadedly connected to one end of the fixing plate by setting a lead screw, the lead screw is used to adjust the height of the fixing plate, the handle is fixedly connected to one end of the lead screw, the adjustment plate is rotatably connected to the other end of the lead screw, the spring sleeve is arranged on the outer wall of the lead screw, and the spring is arranged between the fixing plate and the adjustment plate, the spring is used to support the fixing plate, according to different environments, the handle is rotated, thereby driving the lead screw to rotate, so that the fixing plate moves vertically on the lead screw, the height of the fixed plate is adjusted, and then the radar plate is adjusted to keep the radar plate parallel to prevent errors in radar detection results.
[0004] However, when the above-mentioned concealed defense radar for detecting low-altitude aircraft is used, it is not convenient to adjust the monitoring angle of the radar, so that the monitoring range of the radar is relatively fixed. Utility Model Content
[0005] The utility model aims to provide a concealed defense radar, which solves the problem that the monitoring angle of the concealed defense radar used for low-altitude aircraft detection is not easy to adjust when in use, so that the monitoring range of the radar is relatively fixed.
[0006] To achieve the above-mentioned purpose, the utility model provides a concealed defense radar, including a support column, an adjustment component, a fixed component and a support component; the adjustment component includes a rotating seat, a hinge, an adjustment seat and a radar board, the rotating seat is rotatably connected to the support column and is located at the top of the support column, the hinge is rotatably connected to the rotating seat and is located at the top of the rotating seat, the adjustment seat is rotatably connected to the hinge and is located at the top of the hinge, the radar board is fixedly connected to the adjustment seat and is located at the top of the adjustment seat, a slide groove is provided at the bottom of the adjustment seat, and the fixed component and the support assembly are respectively connected to the support column.
[0007] Among them, the adjustment component also includes a hydraulic cylinder, a telescopic rod and a slider. The hydraulic cylinder is fixedly connected to the rotating seat and is located on the outside of the rotating seat. The telescopic rod is fixedly connected to the hydraulic cylinder and is located between the hydraulic cylinder and the adjustment seat. There are two sliders, and the two sliders are respectively rotatably connected to the telescopic rod and are respectively located inside the slide groove.
[0008] Among them, the fixing assembly includes a fixing seat and a fixing screw, the fixing seat is fixedly connected to the support column and is located at the bottom of the support column. There are multiple fixing screws, and the multiple fixing screws are respectively threadedly connected to the fixing seat and pass through the fixing seat respectively.
[0009] Among them, the fixing assembly also includes a fixing spring and a fixing plate. There are multiple fixing springs, and the multiple fixing springs are respectively fixedly connected to the fixing seat and are respectively located on the outside of the fixing screw. There are multiple fixing plates, and the multiple fixing plates are respectively fixedly connected to the fixing springs and are respectively located at the bottom of the fixing springs.
[0010] Wherein, the support assembly includes a connecting seat and a reinforcing rod, the number of the connecting seats is two, the two connecting seats are respectively fixedly connected to the support columns and are respectively located on the outside of the support columns, and the number of the reinforcing rods is multiple, the multiple reinforcing rods are respectively fixedly connected to the connecting seats and are respectively located between the two connecting seats.
[0011] The utility model provides a concealed defense radar, wherein the support column provides a supporting function for the device, the rotating seat provides a rotating effect for the adjusting component, the hinge provides a rotating effect for the adjusting seat, and the rotating seat provides a supporting function for the radar board. The radar board is used to send and receive signals. When the angle of the radar board is adjusted, the adjusting seat is extended or shortened by the telescopic rod so that the adjusting seat is rotated along the hinge to achieve the purpose of adjusting the angle of the radar board, thereby increasing the monitoring range of the radar board, and solving the problem that when the concealed defense radar used for low-altitude aircraft detection is used, it is inconvenient to adjust the monitoring angle of the radar, so that the monitoring range of the radar is relatively fixed. BRIEF DESCRIPTION OF THE DRAWINGS
[0012] 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.
[0013] Figure 1 It is a schematic diagram of the overall structure of a concealed defense radar according to the first embodiment of the utility model.
[0014] Figure 2It is a schematic cross-sectional structure diagram of the adjustment component of the first embodiment of the utility model.
[0015] Figure 3 It is a structural schematic diagram of the fixing assembly of the first embodiment of the utility model.
[0016] Figure 4 It is a front view of a concealed defense radar according to the second embodiment of the utility model.
[0017] In the figure: 101-support column, 102-rotating seat, 103-hinge, 104-adjusting seat, 105-radar plate, 106-slide, 107-hydraulic cylinder, 108-telescopic rod, 109-slider, 110-fixed seat, 111-fixed screw, 112-fixed spring, 113-fixed plate, 201-connecting seat, 202-reinforcement rod. DETAILED DESCRIPTION
[0018] 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.
[0019] The first embodiment of the present application is:
[0020] See also Figures 1 to 3 ,in, Figure 1 This is a schematic diagram of the overall structure of a concealed defense radar according to the first embodiment of the utility model. Figure 2 : is a schematic cross-sectional structure diagram of the adjustment component of the first embodiment of the utility model, Figure 3 It is a structural schematic diagram of the fixing component of the first embodiment of the utility model. The utility model provides a concealed defense radar, including a support column 101, an adjustment component and a fixing component. The adjustment component includes a rotating seat 102, a hinge 103, an adjustment seat 104, a radar plate 105, a hydraulic cylinder 107, a telescopic rod 108 and a slider 109. The fixing component includes a fixing seat 110, a fixing screw 111, a fixing spring 112 and a fixing plate 113. The above-mentioned scheme solves the problem that the concealed defense radar used for low-altitude aircraft detection is not convenient to adjust the monitoring angle of the radar when in use, so that the monitoring range of the radar is relatively fixed. It can be understood that the above-mentioned scheme can be used in the scenario of adjusting the radar angle, and can also be used to solve the radar installation problem.
[0021] According to the present specific embodiment, the rotating seat 102 is rotatably connected to the support column 101 and is located at the top of the support column 101. The hinge 103 is rotatably connected to the rotating seat 102 and is located at the top of the rotating seat 102. The adjustment seat 104 is rotatably connected to the hinge 103 and is located at the top of the hinge 103. The radar board 105 is fixedly connected to the adjustment seat 104 and is located at the top of the adjustment seat 104. A slide groove 106 is provided at the bottom of the adjustment seat 104. The fixing assembly and the supporting assembly are respectively connected to the support column 101. The support column 101 provides support for the device, the rotating seat 102 provides a rotation effect for the adjustment component, the hinge 103 provides a rotation effect for the adjustment seat 104, and the rotating seat 102 provides support for the radar board 105. The radar board 105 is used to send and receive signals. When the angle of the radar board 105 is adjusted, the telescopic rod 108 is extended or shortened to make the adjustment seat 104 rotate along the hinge 103, so as to achieve the purpose of adjusting the angle of the radar board 105, so that the monitoring range of the radar board 105 is increased.
[0022] Among them, the hydraulic cylinder 107 is fixedly connected to the rotating seat 102 and is located on the outside of the rotating seat 102, the telescopic rod 108 is fixedly connected to the hydraulic cylinder 107 and is located between the hydraulic cylinder 107 and the adjusting seat 104, the number of the sliders 109 is two, the two sliders 109 are respectively rotatably connected to the telescopic rod 108 and are respectively located inside the slide groove 106, the hydraulic device in the hydraulic cylinder 107 provides power for the adjusting component, the telescopic rod 108 is a telescopic sleeve rod, and the slider 109 provides a limiting effect for the adjusting seat 104 and the telescopic rod 108. When the angle of the adjusting seat 104 is adjusted, the telescopic rod 108 is pushed to extend by the hydraulic device in the hydraulic cylinder 107, so that the slider 109 slides along the inside of the adjusting seat 104, and the adjusting seat 104 is rotated and lifted along the hinge 103, so as to achieve the purpose of adjusting the angle of the radar board 105.
[0023] Secondly, the fixing seat 110 is fixedly connected to the support column 101 and is located at the bottom of the support column 101. There are multiple fixing screws 111, and the multiple fixing screws 111 are respectively threadedly connected to the fixing seat 110 and pass through the fixing seat 110 respectively. The fixing seat 110 provides support for the device. The fixing screws 111 are convenient for installing the fixing seat 110 and the support column 101 in a fixed position. By adjusting the height of each fixing screw 111, the fixing seat 110 can be easily adapted to different terrains.
[0024] Again, there are multiple fixing springs 112, and the multiple fixing springs 112 are respectively fixedly connected to the fixing seat 110 and are respectively located on the outside of the fixing screw 111. There are multiple fixing plates 113, and the multiple fixing plates 113 are respectively fixedly connected to the fixing springs 112 and are respectively located at the bottom of the fixing springs 112. The fixing springs 112 provide support for the fixing plates 113, and the fixing plates 113 are in contact with the ground. The elastic force provided by the fixing springs 112 makes the fixing plates 113 press against the ground, so that the fixing effect of the fixing screw 111 is better.
[0025] In a concealed defense radar using the present embodiment, the support column 101 provides support for the device, the rotating seat 102 provides a rotation effect for the adjustment component, the hinge 103 provides a rotation effect for the adjustment seat 104, and the rotating seat 102 provides support for the radar board 105. The radar board 105 is used to send and receive signals. When the angle of the radar board 105 is adjusted, the telescopic rod 108 is extended or shortened to make the adjustment seat 104 rotate along the hinge 103, so as to achieve the purpose of adjusting the angle of the radar board 105, so that the monitoring range of the radar board 105 is increased, which solves the problem that the concealed defense radar used for low-altitude aircraft detection is not convenient to adjust the monitoring angle of the radar when in use, so that the monitoring range of the radar is relatively fixed.
[0026] The second embodiment of the present application is:
[0027] Based on the first embodiment, please refer to Figure 4 ,in, Figure 4 It is a front view of a concealed defense radar according to the second embodiment of the utility model.
[0028] The concealed defense radar of this embodiment further includes a supporting assembly, and the supporting assembly includes a connecting seat 201 and a reinforcing rod 202 .
[0029] According to this specific embodiment, the number of the connecting seats 201 is two, and the two connecting seats 201 are respectively fixedly connected to the support column 101 and are respectively located on the outside of the support column 101. The number of the reinforcing rods 202 is multiple, and the multiple reinforcing rods 202 are respectively fixedly connected to the connecting seats 201 and are respectively located between the two connecting seats 201. The connecting seats 201 provide support for the reinforcing rods 202, and the reinforcing rods 202 provide reinforced support for the support column 101, so that when the equipment encounters bad weather, the support column 101 is not easy to bend.
[0030] In a concealed defense radar using the present embodiment, the connection seat 201 provides support for the reinforcing rod 202, and the reinforcing rod 202 provides reinforced support for the support column 101, so that when the equipment encounters severe weather, the support column 101 is not easily bent.
[0031] 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. A concealed defense radar, comprising a support column, characterized in that: Also includes an adjustment component, a fixing component and a supporting component; The adjustment assembly includes a rotating seat, a hinge, an adjustment seat and a radar board. The rotating seat is rotatably connected to the support column and is located at the top of the support column. The hinge is rotatably connected to the rotating seat and is located at the top of the rotating seat. The adjustment seat is rotatably connected to the hinge and is located at the top of the hinge. The radar board is fixedly connected to the adjustment seat and is located at the top of the adjustment seat. A sliding groove is provided at the bottom of the adjustment seat. The fixed assembly and the supporting assembly are respectively connected to the support column.
2. A concealed defense radar as claimed in claim 1, characterized in that: The adjustment assembly also includes a hydraulic cylinder, a telescopic rod and a slider. The hydraulic cylinder is fixedly connected to the rotating seat and is located on the outside of the rotating seat. The telescopic rod is fixedly connected to the hydraulic cylinder and is located between the hydraulic cylinder and the adjustment seat. There are two sliders. The two sliders are respectively rotatably connected to the telescopic rod and are respectively located inside the slide groove.
3. A concealed defense radar as claimed in claim 1, characterized in that: The fixing assembly includes a fixing seat and a fixing screw. The fixing seat is fixedly connected to the support column and is located at the bottom of the support column. There are multiple fixing screws, and the multiple fixing screws are respectively threadedly connected to the fixing seat and pass through the fixing seat respectively.
4. A concealed defense radar as claimed in claim 3, characterized in that: The fixing assembly also includes a fixing spring and a fixing plate. There are multiple fixing springs, each of which is fixedly connected to the fixing seat and located on the outside of the fixing screw. There are multiple fixing plates, each of which is fixedly connected to the fixing spring and located on the bottom of the fixing spring.
5. A concealed defense radar as claimed in claim 1, characterized in that: The support assembly includes a connecting seat and a reinforcing rod. There are two connecting seats, and the two connecting seats are respectively fixedly connected to the support columns and are respectively located on the outsides of the support columns. There are multiple reinforcing rods, and the multiple reinforcing rods are respectively fixedly connected to the connecting seats and are respectively located between the two connecting seats.
Citation Information
Patent Citations
Concealed defense radar for low-altitude aircraft detection
CN220525991U