Supporting device for anti-unmanned aerial vehicle equipment

Abstract

The supporting device for the anti-unmanned aerial vehicle equipment comprises a shell and a mounting plate, a groove is formed in the shell, the mounting plate can ascend and descend in the groove, a plurality of adsorption assemblies are arranged on the shell, a plurality of protruding blocks are arranged on the mounting plate, each adsorption assembly comprises a suction cup, a supporting rod, a swinging rod, a lifting rod and a spring, the suction cups are arranged on the outer surface of the shell, and the supporting rods are arranged on the outer surface of the shell. The swing rod is arranged on the inner surface of the shell through a supporting rod, the top end of the swing rod is connected with the suction cup through a lifting rod, the spring can provide elastic force for the bottom end of the swing rod, a protrusion matched with the protruding block is arranged at the bottom end of the swing rod, and when the mounting plate descends, the protruding block can press the protrusion so that the swing rod can swing to pull the lifting rod to tension the suction cup and adsorb the suction cup to the wall. When the mounting plate ascends, the convex block leaves the bulge, the swinging rod resets under the action of elastic force, and the sucker is loosened and is separated from adsorption; the at least one adsorption assembly is arranged on the shell through the lifting assembly; the mounting plate is further provided with a movable protruding block capable of enabling the suction cup on the lifting assembly to be adsorbed to the wall face.

Description

Technical Field

[0001] The utility model belongs to the field of anti-UAV equipment, and in particular relates to a supporting device for anti-UAV equipment. Background Art

[0002] At present, drone technology has been widely used in the inspection, troubleshooting and even planning and construction stages of power grids and power stations. At the same time, the risk of drones invading power facilities is getting higher and higher. Since the power grid has a huge impact on social production and residents' lives, and even has great significance for military layout, the security and even anti-terrorism of power facilities are facing an extremely severe situation. The current drone countermeasures include drone detection equipment and radio active defense equipment. Drone detection equipment mainly detects, tracks and identifies drones by capturing drone remote control, image transmission and other communication signals. Radio active defense equipment drives away, interferes with, and forces drones to land through navigation deception and interference.

[0003] Anti-UAV equipment needs to be deployed as high as possible, but due to the relevant safety requirements of power stations, existing anti-UAV equipment is mostly deployed by erecting new poles and towers, which is costly and inefficient. Since drone intrusion is random, but it is a "low, slow and small" aircraft, after discovering illegal drone intrusion, the rapid deployment of anti-UAV equipment and the insufficient coverage of existing anti-UAV equipment are issues that need to be addressed. Utility Model Content

[0004] In view of this, the utility model aims to propose a support device for anti-UAV equipment to solve the above technical problems. To achieve the above purpose, the technical solution of the utility model is as follows:

[0005] A support device for anti-UAV equipment comprises: a shell and a mounting plate, wherein a groove for accommodating the mounting plate is provided in the shell, the mounting plate can be lifted and lowered in the groove, a plurality of adsorption components are provided on the shell, a plurality of protrusions are provided on the mounting plate, the adsorption components comprise a suction cup, a support rod, a swing rod, a lifting rod and a spring, the suction cup is provided on the outer surface of the shell, the support rod is provided on the inner surface of the shell, the middle part of the swing rod is rotatably connected to one end of the support rod, one end of the lifting rod is rotatably connected to the top end of the swing rod, and the other end of the lifting rod passes through the shell The housing is connected to the suction cup, one end of the spring is connected to the bottom end of the swing rod, and the other end of the spring is connected to the inner surface of the housing. A protrusion that can cooperate with the protrusion is also provided at the bottom end of the swing rod. When the mounting plate descends, the protrusion can press the protrusion to make the swing rod swing and pull the lifting rod to move into the housing. At this time, the other end of the lifting rod can tighten the suction cup so that the suction cup can be adsorbed on the wall. When the mounting plate rises, the protrusion leaves the protrusion, and the swing rod resets and swings under the elastic force of the spring. At this time, the lifting rod moves out of the housing and relaxes the suction cup to make the suction cup detached from adsorption.

[0006] The shell is also provided with a lifting component, and at least one adsorption component is arranged on the lifting component; the mounting plate is also provided with a movable protrusion that can be lifted and lowered, and the movable protrusion can cooperate with the lifting component so that the suction cup on the lifting component can be adsorbed on the wall.

[0007] Furthermore, the suction cup includes a suction cup cover and a suction cup bowl, and the lifting rod is connected to the center of the suction cup bowl. The lifting rod can tighten the suction cup bowl to generate a negative pressure space between the suction cup bowl and the wall.

[0008] Furthermore, a sliding groove is provided on the shell, and the lifting assembly is lifted and lowered in the sliding groove. The sliding groove is provided with a plurality of locking grooves, and the plurality of locking grooves are evenly arranged on one side of the sliding groove.

[0009] Furthermore, the mounting plate is provided with a slot, a slider is provided in the slot, the movable protrusion is provided on the slider, the slot is provided with a plurality of slots, and the plurality of slots are evenly arranged on one side of the slot.

[0010] Furthermore, the lifting assembly includes a lifting plate and a locking pin, wherein the locking pin is slidably arranged on the lifting plate and can cooperate with the locking groove to lock the lifting plate.

[0011] Furthermore, the slider is provided with a latch, which can be inserted into the slot to lock the slider.

[0012] Furthermore, a clamping section is provided on the suction cup cover, and the suction cup bowl includes a straight section and a raised section. The clamping section can press the straight section against the wall, and the lifting rod is connected to the center of the raised section and can lift the center of the raised section to generate a negative pressure space between the raised section and the wall.

[0013] Furthermore, a device seat is provided at the top of the mounting plate. The device seat is vertically arranged on the mounting plate, and one end of the device seat is fixedly connected to the top of the mounting plate.

[0014] Furthermore, the shell includes a front shell, a rear shell and a top plate, the top plate is vertically arranged at the top end of the front shell and extends to above the rear shell, and the top plate and the top end of the rear shell form a channel for accommodating the equipment seat.

[0015] Furthermore, a baffle is provided on the bottom surface of the top plate, and the baffle is vertically arranged on the bottom surface of the top plate between the front shell and the rear shell.

[0016] Compared with the prior art, the supporting device for anti-UAV equipment described in the utility model has the following advantages:

[0017] (1) The mounting plate can be raised and lowered in the groove formed by the front shell and the rear shell. The top plate and the baffle plate provided on the front shell can guide the mounting plate to be raised and lowered. When the mounting plate descends, the protrusion on the mounting plate can quickly press the protrusion and press the swing rod to swing. The swing rod pulls the lifting rod to make the suction cup adsorb. When the mounting plate rises, the protrusion moves away from the protrusion to loosen the protrusion. The swing rod resets and swings under the elastic force of the spring, pushing the lifting rod to squeeze the negative pressure space to make it disappear and loosen the suction cup. The operator only needs to press down or lift up the equipment seat connected to the top of the mounting plate to simply and quickly install or remove the anti-UAV equipment.

[0018] (2) The protrusion on the swing rod and the protrusion on the mounting plate can cooperate with each other to press down the other end of the swing rod, so that one end of the swing rod can pull up the raised section of the suction cup bowl through the lifting rod, and the pressing section of the suction cup cover can press the straight section of the suction cup bowl to form a closed negative pressure space between the raised section and the wall surface, so that the suction cup can be quickly and tightly adsorbed on the wall surface. The building height in the power station meets the safety requirements of the power station. The anti-UAV equipment can be installed on the roof or the top of the outer wall of the power station building without damaging the wall surface, and there is no need to evaluate the safety of drilling holes in the power station building;

[0019] (3) A lifting plate is arranged in the sliding groove on the front shell, a dynamic adsorption component is arranged on the lifting plate and is lifted and lowered simultaneously with the lifting plate, a slider is arranged in the slot on the mounting plate, and a dynamic protrusion is arranged on the slider and is lifted and lowered simultaneously with the slider. The dynamic protrusion and the dynamic adsorption component can cooperate with each other, so that a suction cup can be lifted and lowered, and can adapt to the width of various walls and even the anti-UAV equipment can be installed on the eaves. Based on the principle that three points determine a plane, the installation of the anti-UAV equipment is more stable.

[0020] (4) The locking pin on the lifting plate and the locking groove on one side of the sliding groove can cooperate with each other to quickly adjust the position of the lifting plate, and the latch pin on the slider and the slot on one side of the slot can cooperate with each other to quickly adjust the position of the slider. Before installing the anti-UAV equipment, it can be quickly adjusted according to the required installation position. BRIEF DESCRIPTION OF THE DRAWINGS

[0021] The accompanying drawings constituting a part of the present invention are used to provide a further understanding of the present invention. The illustrative embodiments of the present invention and their descriptions are used to explain the present invention and do not constitute an improper limitation on the present invention. In the accompanying drawings:

[0022] Figure 1 A schematic diagram of the structure of a support device for anti-UAV equipment according to an embodiment of the present invention;

[0023] Figure 2 The support device for anti-UAV equipment described in the embodiment of the present invention is along Figure 1 Sectional view along line AA;

[0024] Figure 3 The support device for anti-UAV equipment described in the embodiment of the present invention is along Figure 1 Sectional view along the midline BB;

[0025] Figure 4 A schematic diagram of the structure of the mounting plate according to an embodiment of the present invention;

[0026] Figure 5 A schematic diagram of the structure of the adsorption assembly according to an embodiment of the present invention;

[0027] Figure 6 A schematic structural diagram of another state change of the adsorption component described in the embodiment of the present invention.

[0028] Explanation of the reference numerals: 1-anti-UAV equipment; 2-front shell; 3-suction cup; 4-sliding groove; 5-locking groove; 6-slot; 7-moving suction cup; 8-lifting plate; 9-locking pin; 10-top plate; 11-bump; 12-bump; 13-moving bump; 14-moving bump; 15-rear shell; 16-groove; 17-mounting plate; 18-baffle; 19-equipment seat; 20-lifting rod; 21-swing rod; 22-spring; 23-latch pin; 24-slider; 25-adjusting groove; 26-slot slot; 27-suction cup cover; 28-straight section; 29-raised section; 30-convex ring; 31-hinge shaft; 32-pressing section; 33-support rod; 34-swing shaft; 35-lifting shaft; 36-negative pressure space. DETAILED DESCRIPTION

[0029] It should be noted that, in the absence of conflict, the embodiments of the present invention and the features in the embodiments can be combined with each other.

[0030] In the description of the present utility model, it should be understood that the terms "center", "longitudinal", "lateral", "up", "down", "front", "back", "left", "right", "vertical", "horizontal", "top", "bottom", "inside", "outside" and the like indicate positions or positional relationships based on the positions or positional relationships shown in the accompanying drawings, and are only for the convenience of describing the present utility model and simplifying the description, rather than indicating or implying that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and therefore cannot be understood as a limitation on the present utility model. In addition, the terms "first", "second", etc. are only used for descriptive purposes, and cannot be understood as indicating or implying relative importance or implicitly indicating the number of technical features indicated. Therefore, features defined as "first", "second", etc. may explicitly or implicitly include one or more of the features. In the description of the present utility model, unless otherwise specified, "multiple" means two or more.

[0031] In the description of the present invention, it should be noted that, unless otherwise clearly specified and limited, the terms "installation", "connection" and "connection" should be understood in a broad sense, for example, it can be a fixed connection, a detachable connection, or an integral connection; it can be a mechanical connection or an electrical connection; it can be a direct connection, or it can be an indirect connection through an intermediate medium, or it can be the internal communication of two components. For ordinary technicians in this field, the specific meanings of the above terms in the present invention can be understood by specific circumstances.

[0032] The present invention will be described in detail below with reference to the accompanying drawings and in combination with embodiments.

[0033] A support device for anti-UAV equipment, such as Figure 1 , 2 As shown, it includes: a housing and a mounting plate 17, the housing includes a front housing 2, a rear housing 15 and a top plate 10, the front housing 2 and the rear housing 15 are arranged in parallel with each other, and the front housing 2 and the rear housing 15 form a groove 16 for accommodating the mounting plate 17, the top plate 10 is vertically arranged on the front housing 2, one end of the top plate 10 is connected to the top end of the front housing 2, the other end of the top plate 10 extends to the top of the rear housing 15, and the other end of the top plate 10 and the top end of the rear housing 15 form a channel for accommodating the device seat 19. Side plates and a bottom plate are respectively arranged on both sides and the bottom surface of the front housing 2 and the rear housing 15, and the front housing 2, the rear housing 15, the side plates, the bottom plate and the top plate 10 together constitute a cube with a device seat channel, and the front housing 2, the rear housing 15, the side plates, the bottom plate and the top plate 10 can be metal plates or hard plastic plates.

[0034] The mounting plate 17 is arranged in the groove 16, and the surface of the mounting plate 17 close to the rear shell 15 can be fitted with the inner surface of the rear shell 15. A baffle 18 is also arranged on the bottom surface of the top plate 10, and the baffle 18 is arranged perpendicular to the top plate 10. The baffle 18 can fit with the surface of the mounting plate 17 close to the front shell 2. The mounting plate 17 rises and falls under the guidance of the rear shell 15 and the baffle 18. The baffle 18 can also prevent dust from entering the groove 16 along the channel when the mounting plate 17 descends. A plurality of protrusions 11 are arranged on the surface of the mounting plate 17 facing the front shell 2. The equipment seat 19 is vertically arranged on the mounting plate 17, one end of the equipment seat 19 is fixedly connected to the top of the mounting plate 17, and the other end of the equipment seat 19 extends from the channel 19 to the outside of the rear shell 15. The equipment seat 19 can rise and fall in the channel to make the mounting plate 17 rise and fall in the groove. The equipment seat 19 is used to install the anti-UAV device 1. The mounting plate 17 can be a metal plate or a hard plastic plate, and the equipment seat 19 can be a metal plate or a hard plastic plate.

[0035] A plurality of adsorption components are provided on the front housing 2, such as Figure 5As shown, the adsorption assembly includes a suction cup 3, a support rod 33, a swing rod 21, a lifting rod 20 and a spring 22. There can be two adsorption assemblies. The suction cup 3 is arranged on the outer surface of the front shell 2. The two suction cups of the two adsorption assemblies are respectively located on both sides of the center of the outer surface of the front shell 2 near the upper end and are symmetrically arranged. The support rod 33 is arranged on the inner surface of the front shell 2. The middle part of the swing rod 21 is rotatably connected with one end of the support rod 33 through a swing shaft 34. One end of the lifting rod 20 is rotatably connected with the top end of the swing rod 21 through a lifting shaft 35. The other end of the lifting rod 20 passes through the front shell 2 and is connected with the suction cup 3. One end of the spring 22 is connected to the bottom end of the swing rod 21, and the other end of the spring 22 is connected to the inner surface of the front shell 2. A protrusion 12 is also arranged at the bottom end of the swing rod 21. The protrusion 12 is arranged on the side of the swing rod 21 facing the mounting plate 17 and can cooperate with the protrusion 11 on the mounting plate 17.

[0036] When the mounting plate 17 descends in the groove, as shown in FIG. Figure 6 As shown, the protrusion 11 can press the protrusion 12 to make the bottom end of the swing rod 21 swing toward the front shell 2, and the top end of the swing rod 21 swings toward the direction of the rear shell 15 under the action of the support rod 33 and the swing shaft 35 and pulls the lifting rod 20 toward the rear shell 15. At this time, the other end of the lifting rod 20 can tighten the suction cup 3 so that the suction cup 3 can be adsorbed on the wall. When the mounting plate 17 rises, the protrusion 11 leaves the protrusion 12, and the bottom end of the swing rod 21 swings back to the rear shell 15 under the elastic force of the spring 22. The top end of the swing rod 21 swings toward the front shell 15 under the action of the support rod 33 and the swing shaft 35 and pushes the lifting rod 20 to the front shell 2. At this time, the other end of the lifting rod 20 can relax the suction cup 3 to make the suction cup 3 disengage.

[0037] A sliding groove 4 is also provided on the front housing 2. Figure 3 As shown, the sliding groove 4 is provided with a plurality of locking grooves 5, and the plurality of locking grooves 5 are evenly arranged on one side of the sliding groove 4. A lifting assembly is also provided in the sliding groove 4, and the lifting assembly includes a lifting plate 8 and a locking pin 9. The lifting plate 8 can be lifted and lowered under the guidance of the sliding groove 1. The locking pin 9 is slidably arranged on the lifting plate 8 and can cooperate with the locking groove 5 to lock the lifting plate 8. When the locking pin 9 is relatively aligned with the locking groove 5, the locking pin 9 can slide toward the locking groove 5 and insert into the locking groove 5. At this time, the lifting plate 8 is locked. When the locking pin 9 slides out of the locking groove 5, the lifting plate 8 slides and unlocks and can be lifted and lowered in the sliding groove 4. A dynamic adsorption assembly is provided on the lifting plate 8, and the dynamic adsorption assembly can be lifted and lowered together with the lifting plate 8 under the guidance of the sliding groove 4. There can be multiple dynamic adsorption assemblies provided on the lifting plate 8.

[0038] The mounting plate 17 is also provided with a slot 6, such as Figure 3 , 4As shown, the slot 6 is provided with a plurality of slots 26, which are evenly arranged on one side of the slot 6. A slider 24 is also provided in the slot 6, and the slider 24 can be raised and lowered under the guidance of the slot 6. A slidable latch 23 is also provided on the slider 24, and the latch 23 can cooperate with the slot 26 to lock the slider 24. When the latch 23 is aligned with the slot 26, the latch 23 can slide toward the slot 26 and be inserted into the slot 26, and the slider 24 is locked. When the latch 23 slides out of the slot 26, the slider 24 slides to unlock and can be raised and lowered in the slot 6. At least one movable protrusion 13 is provided on the slider 24, and the movable protrusion 13 can be raised and lowered together with the slider 24 under the guidance of the slot 6.

[0039] An adjustment slot 25 is also provided on the rear housing 15 , and the adjustment slot 25 is aligned with the slot 6 . A portion of the latch 23 is located in the adjustment slot 25 and can be raised and lowered in the adjustment slot 25 . The slot 26 into which the latch 23 is inserted can be adjusted through the adjustment slot 25 .

[0040] The dynamic adsorption component has the same structure as the adsorption component, except that the dynamic adsorption component can be raised and lowered on the front housing 2 under the guidance of the slide groove 4 and the lifting plate 8. The suction cup that can be adsorbed on the wall on the corresponding dynamic adsorption component is the dynamic suction cup 7, and the part that can cooperate with the dynamic protrusion 13 is the dynamic protrusion 14. The positions of the multiple slots 26 on the slot 6 can correspond to the positions of the multiple locking slots 5 on the slide groove 4. When the latch 23 and the locking pin 9 are respectively inserted into the corresponding slots 26 and the locking slot 5, the dynamic protrusion 14 can cooperate with the dynamic protrusion 13. When the lifting plate 17 descends to make the protrusion 11 press the protrusion 12, the dynamic protrusion 14 can also press the dynamic protrusion 13 at the same time. At this time, the dynamic suction cup 7 of the dynamic adsorption component can be adsorbed on the wall at the same time as the suction cup 3 of the adsorption component.

[0041] Before installing the support device of the anti-UAV equipment, the locking groove 5 into which the locking pin 9 is inserted can be adjusted on the outer side of the front shell 2 and the latch 23 can be adjusted in the adjustment groove 25 to be inserted into the corresponding slot 26 so that the movable protrusion 13 and the movable protrusion 14 can cooperate with each other.

[0042] The suction cup 3 includes a suction cup cover 27 and a suction cup bowl. The suction cup cover 27 is provided with a clamping section 32. The suction cup bowl includes a straight section 28 and a raised section 29. One end of the suction cup cover 27 is connected to the outer surface of the front shell 2. The clamping section 32 is in contact with the straight section 28 and can press the straight section 28 against the wall when the suction cup is adsorbed. A convex ring 30 is also provided on the raised section 29. The straight section 28, the raised section 29 and the convex ring 30 are integrally formed to form a suction cup bowl. The suction cup bowl is a flexible suction cup and can be made of rubber or silicone. The other end of the lifting rod 20 is connected to the convex ring 30 through a hinge shaft 31.

[0043] When the lifting rod 20 is pulled by the swing rod 21 and moves to the rear housing 15, the lifting rod 20 can pull the convex ring 30 to move toward the rear housing 15 through the hinge shaft 31. At this time, the raised section 29 is pulled by the convex ring 31 and bulges in the direction of the rear housing 15. A negative pressure space 36 is generated between the raised section 29 and the wall. The suction cup 3 is firmly adsorbed on the wall under the action of the negative pressure space 36. The pressing section 32 presses the straight section 28 tightly against the wall, ensuring that the airtightness of the negative pressure space 36 will not be destroyed, resulting in the suction cup adsorption failure. When the swing rod 21 is reset and swung under the action of the spring 22, the lifting rod 20 is pushed by the swing rod 21 and moves toward the front housing. The lifting rod 20 can relax the raised section 29 that is raised toward the rear housing 15. At this time, the raised section 29 is attached to the wall, the negative pressure space disappears, and the suction cup is out of the adsorption state. Since the suction cup is made of a flexible material, the raised section 29 can be lifted by the lifting rod 20 by its own elastic deformation to rise into the cavity formed by the suction cup cover 27 or to fit against the wall.

[0044] One installation method of this embodiment is: first install the anti-UAV device on the device seat, then adjust the position of the latch and the locking pin according to the installation position so that the two can cooperate with each other to determine the position of the dynamic suction cup, then stick the front shell to the wall surface where the installation is required, press the device seat downward to drive the installation plate down so that the suction cup can be adsorbed on the wall surface to complete the installation of the anti-UAV device. When the anti-UAV device is disassembled and moved, the device seat is lifted up to drive the installation plate up to make the suction cup out of the adsorption state, so as to remove the anti-UAV device.

[0045] The working principle of this embodiment is: according to the installation position, first adjust the locking groove where the locking pin is inserted on the outside of the front shell to position the lifting plate to fix the position of the dynamic suction cup, and at the same time adjust the slot where the pin is inserted in the adjustment groove to position the dynamic protrusion so that it can cooperate with the dynamic protrusion. When the equipment seat is pressed down to drive the mounting plate to descend, the protrusion and the dynamic protrusion can respectively descend and press the protrusion and the dynamic protrusion at the same time. At this time, the swing rod swings to pull the lifting rod to move toward the rear shell, and the lifting rod pulls the bulge to the rear shell and forms a negative pressure space with the wall to complete the adsorption. When disassembling the anti-UAV equipment, lift the equipment seat to drive the mounting plate to rise, and the protrusion and the dynamic protrusion are removed from the protrusion and the dynamic protrusion respectively. The swing rod resets and swings under the action of the spring and pushes the lifting rod to move to the front shell. At this time, the lifting rod relaxes the protrusion, and the protrusion fits the wall, the negative pressure space disappears, and the suction cup is out of the adsorption state.

[0046] The effects of the above scheme are described below:

[0047] The mounting plate can be raised and lowered in the groove formed by the front shell and the rear shell, and the top plate and the baffle can guide the lifting and lowering of the mounting plate. When the mounting plate descends, the convex block can quickly press the convex block and make the suction cup adsorbed on the wall. When the mounting plate rises, the convex block can loosen the convex block. The swing plate is reset under the elastic force of the spring and pushes the lifting rod to squeeze the bulge section so that the negative pressure space disappears and the suction cup is loosened. The operator only needs to press down or lift up the equipment seat connected to the top of the mounting plate to simply and quickly install or remove the anti-UAV equipment; the convex block on the mounting plate can be aligned with the convex block on the swing rod The two parts cooperate with each other to make the swing rod swing and pull up the raised section of the suction cup bowl by rotating the lifting rod connected to one end of the swing rod. After the raised section is raised, it can form a negative pressure space with the wall so that the suction cup can be adsorbed on the wall. The pressing section of the suction cup cover can press the straight section of the suction cup bowl to ensure that the airtightness of the negative pressure space will not be destroyed, resulting in the failure of the suction cup adsorption. The suction cup adsorbs the wall quickly and firmly. The building height in the power station meets the safety requirements of the power station. The anti-UAV equipment can be installed on the roof or the top of the outer wall of the power station building without damaging the wall. It is easy to operate and There is no need to evaluate the safety of drilling holes in the power station building; a lifting plate is arranged in the sliding groove on the front shell, a dynamic adsorption component that is lifted and lowered simultaneously with the lifting plate is arranged on the lifting plate, a slider is arranged in the slot on the mounting plate, and a dynamic protrusion that is lifted and lowered simultaneously with the slider is arranged on the slider, the dynamic protrusion and the dynamic adsorption component can cooperate with each other, so that the dynamic suction cup can be lifted and lowered, and can adapt to the width of various walls and even install the anti-UAV equipment on the eaves, and based on the principle of three points determining a plane, the installation of the anti-UAV equipment is more stable; the locking pin and the locking groove can cooperate with each other to quickly adjust the position of the lifting plate, the latch and the slot can cooperate with each other to quickly adjust the position of the slider, and before the anti-UAV equipment is installed, it can be quickly adjusted according to the position to be installed to ensure that the position of the lifting plate and the slider can cooperate with each other so that the dynamic suction cup can be smoothly adsorbed on the wall; the pressing section on the suction cup cover can press the straight section of the suction cup bowl on the wall, so that when the raised section is pulled up, the airtightness of the negative pressure space formed between the raised section and the wall is ensured, and the suction cup will not fail due to air leakage in the negative pressure space, so that the installation of the anti-UAV equipment is more stable.

[0048] The above description is only a preferred embodiment of the present invention and is not intended to limit the present invention. Any modifications, equivalent substitutions, improvements, etc. made within the spirit and principles of the present invention should be included in the protection scope of the present invention.

Claims

1. A support device for anti-UAV equipment, characterized in that: The invention comprises: a shell and a mounting plate (17); a groove (16) for accommodating the mounting plate (17) is provided in the shell, and the mounting plate (17) can be raised and lowered in the groove; a plurality of adsorption components are provided on the shell, and a plurality of protrusions (11) are provided on the mounting plate (17); the adsorption components comprise a suction cup (3), a support rod (33), a swing rod (21), a lifting rod (20) and a spring (22); the suction cup (3) is provided on the outer surface of the shell, the support rod (33) is provided on the inner surface of the shell, the middle part of the swing rod (21) is rotatably connected to one end of the support rod (33), one end of the lifting rod (20) is rotatably connected to the top end of the swing rod (21), the other end of the lifting rod (20) passes through the shell and is connected to the suction cup (3), and the spring (22) One end of the spring (22) is connected to the bottom end of the swing rod (21), and the other end of the spring (22) is connected to the inner surface of the shell. A protrusion (12) that can cooperate with the protrusion (11) is also provided at the bottom end of the swing rod (21). When the mounting plate (17) descends, the protrusion (11) can press the protrusion (12) to make the swing rod (21) swing and pull the lifting rod (20) to move into the shell. At this time, the other end of the lifting rod (20) can tighten the suction cup (3) so that the suction cup (3) can be adsorbed on the wall. When the mounting plate (17) rises, the protrusion (11) leaves the protrusion (12), and the swing rod (21) resets and swings under the elastic force of the spring (22). At this time, the lifting rod (20) moves out of the shell and relaxes the suction cup (3) so that the suction cup (3) is separated from the adsorption. The shell is also provided with a lifting component, and at least one adsorption component is arranged on the lifting component; the mounting plate (17) is also provided with a movable protrusion (13) that can be lifted and lowered, and the movable protrusion (13) can cooperate with the lifting component so that the suction cup on the lifting component can be adsorbed on the wall surface.

2. A support device for anti-UAV equipment according to claim 1, characterized in that: The suction cup comprises a suction cup cover (27) and a suction cup bowl. The lifting rod (20) is connected to the center of the suction cup bowl. The lifting rod (20) can tighten the suction cup bowl to generate a negative pressure space (36) between the suction cup bowl and the wall.

3. The supporting device for anti-UAV equipment according to claim 1, characterized in that: The housing is also provided with a sliding groove (4), the lifting assembly is arranged in the sliding groove (4) in a liftable manner, the sliding groove (4) is provided with a plurality of locking grooves (5), and the plurality of locking grooves (5) are evenly arranged on one side of the sliding groove (4).

4. The supporting device for anti-UAV equipment according to claim 1, characterized in that: The mounting plate (17) is also provided with a slot (6), a slider (24) is provided in the slot (6), the movable protrusion (13) is arranged on the slider (24), the slot (6) is provided with a plurality of slots (26), and the plurality of slots (26) are evenly arranged on one side of the slot (6).

5. The supporting device for anti-UAV equipment according to claim 3, characterized in that: The lifting assembly comprises a lifting plate (8) and a locking pin (9). The locking pin (9) is slidably arranged on the lifting plate (8) and can cooperate with the locking groove (5) to lock the lifting plate (8).

6. The supporting device for anti-UAV equipment according to claim 4, characterized in that: The slider (24) is provided with a latch (23), and the latch (23) can be inserted into the slot (26) to lock the slider (24).

7. The supporting device for anti-UAV equipment according to claim 2, characterized in that: The suction cup cover (27) is provided with a pressing section (32), and the suction cup bowl includes a straight section (28) and a raised section (29). The pressing section (32) can press the straight section (28) against the wall surface, and the lifting rod (20) is connected to the center of the raised section (29) and can lift the center of the raised section (29) to generate a negative pressure space (36) between the raised section (29) and the wall surface.

8. The supporting device for anti-UAV equipment according to claim 1, characterized in that: The top of the mounting plate (17) is also provided with a device seat (19), which is vertically arranged on the mounting plate (17), and one end of the device seat (19) is fixedly connected to the top of the mounting plate (17).

9. A support device for anti-UAV equipment according to claim 8, characterized in that: The shell comprises a front shell (2), a rear shell (15) and a top plate (10); the front shell (2) and the rear shell (15) are arranged in parallel with each other at an interval; the top plate (10) is vertically arranged at the top end of the front shell (2) and extends to the top of the rear shell (15); the top plate (10) and the top end of the rear shell (15) form a channel for accommodating the device seat (19).

10. A support device for anti-UAV equipment according to claim 9, characterized in that: A baffle (18) is also provided on the bottom surface of the top plate (10), and the baffle (18) is vertically arranged on the bottom surface of the top plate (10) between the front shell (2) and the rear shell (15).

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