Car roof adsorption structure of portable unmanned aerial vehicle reconnaissance, hitting and luring integrated equipment

Abstract

The utility model discloses a portable unmanned aerial vehicle reconnaissance, beating and luring integrated equipment roof adsorption structure which comprises a base and an unmanned aerial vehicle reconnaissance, beating and luring integrated equipment body, an installation cavity is formed in the base, a plurality of ventilation pipes are installed at the bottom of the base in a sealed and penetrating mode, and suction cups are installed at the bottoms of the ventilation pipes. A gas transmission assembly extending to the outer side of the base is installed in the installation cavity, and the upper end of the base is connected with a containing table through a plurality of buffering supporting pieces. The device is reasonable in structural design, the device can be stably adsorbed to a vehicle roof through the gas transmission assembly, the unmanned aerial vehicle reconnaissance, hitting and luring integrated equipment body can be stably fixed to the containing table through the limiting assembly, when a road is bumpy, the buffering supporting piece can play a buffering role, and the safety of the unmanned aerial vehicle is improved. And the phenomena that the unmanned aerial vehicle reconnaissance, hitting and luring integrated equipment body shakes and falls off and internal elements are damaged due to bumpy roads are reduced.

Description

Technical Field

[0001] The utility model relates to the technical field of integrated equipment for drone observation, strike and luring, in particular to a roof adsorption structure of a portable integrated equipment for drone observation, strike and luring. Background Technique

[0002] Existing drones have a wide range of application scenarios and functions. However, for some important places, such as petrochemical production sites, civil aviation airports, and power sites, certain control over the flight of drones is required. However, with the wide application of drones, the phenomenon of unregulated or random flights in important places has gradually increased. Therefore, it is necessary to control them through integrated equipment for drone observation, strike and luring.

[0003] Currently, the integrated equipment for drone observation, strike and luring is usually adsorbed on the roof of a vehicle through an adsorption structure, and the vehicle is used to drive the equipment to move for controlling the drone. However, the adsorption force of the adsorption device is limited. When adsorbed for a long time and the device shakes due to road bumps, the adsorption structure is likely to become loose and fall off the roof, which is not conducive to the observation, strike and luring work. Therefore, we designed a roof adsorption structure of a portable integrated equipment for drone observation, strike and luring to solve the above problems. Summary of the Invention

[0004] The purpose of the utility model is to solve the problems existing in the prior art, and a roof adsorption structure of a portable integrated equipment for drone observation, strike and luring is proposed. Through the setting of the air delivery component, the device can be stably adsorbed on the roof. The setting of the limit component can stably fix the integrated equipment body of the drone observation, strike and luring on the placement table. When the road is bumpy, the buffer support can play a buffering role, reducing the phenomenon that the integrated equipment body of the drone observation, strike and luring shakes and falls off due to road bumps and damage to its internal components.

[0005] To achieve the above purpose, the utility model adopts the following technical scheme:

[0006] A roof adsorption structure of a portable integrated equipment for drone observation, strike and luring, comprising a base and an integrated equipment body of the drone observation, strike and luring. An installation cavity is opened in the base. A plurality of air pipes are hermetically penetrated and installed at the bottom of the base. Suction cups are installed at the bottoms of the plurality of air pipes. An air delivery component extending to the outside of the base is installed in the installation cavity. The upper end of the base is connected with a placement table through a plurality of buffer supports. The integrated equipment body of the drone observation, strike and luring is placed on the upper end of the placement table. A limit component for fixing the integrated equipment body of the drone observation, strike and luring is arranged on the placement table.

[0007] Preferably, the gas transmission component includes a sealing plate that is hermetically and slidably connected in the installation cavity. A threaded rod is rotatably connected to the side wall of the sealing plate. The threaded rod threadedly penetrates the side wall of the base and extends to the outside of the base. A first rotating handle is fixedly connected to the side wall of the threaded rod.

[0008] Preferably, a plurality of through holes that communicate with the installation cavity are hermetically penetrated through the side wall of the base.

[0009] Preferably, the buffer support member includes a sleeve fixedly connected to the upper end of the base. A support column extending to the outside of the sleeve is slidably connected in the sleeve. A plurality of springs are connected between the inner bottom of the support column and the sleeve.

[0010] Preferably, the limiting component includes a limiting chute opened at the upper end of the placement table. Two limiting sliders adapted to the limiting chute are slidably connected in the limiting chute. Limiting plates for fixing the integrated UAV reconnaissance, strike and lure equipment body are connected to the upper ends of the two limiting sliders. A double-headed screw rod extending to the outside of the placement table is rotatably connected to the inner side wall of the limiting chute. The double-headed screw rod threadedly penetrates the two limiting sliders. A second rotating handle is fixedly connected to the end of the double-headed screw rod.

[0011] Preferably, the limiting plate is U-shaped, and the limiting plate is connected to the upper end of the limiting slider by screws.

[0012] Compared with the prior art, the beneficial effects of the present utility model are as follows:

[0013] 1. For the roof adsorption structure of the portable integrated UAV reconnaissance, strike and lure equipment, the device can be adsorbed on the roof of the vehicle through the suction cup. Rotating the first rotating handle to rotate the threaded rod can move the sealing plate, and suck the remaining air between the suction cup and the roof into the installation cavity through the air pipe, ensuring the adsorption force of the suction cup on the roof of the vehicle, and thus the device can be stably adsorbed on the roof of the vehicle.

[0014] 2. For the roof adsorption structure of the portable integrated UAV reconnaissance, strike and lure equipment, when the integrated UAV reconnaissance, strike and lure equipment body is placed on the placement table and the two limiting plates are controlled to approach each other, the integrated UAV reconnaissance, strike and lure equipment body can be stably clamped and fixed. When the road is bumpy, the buffer support member can play a buffering role, reducing the phenomenon that the integrated UAV reconnaissance, strike and lure equipment body shakes and falls off due to road bumps and damage to its internal components.

[0015] 3. For the roof adsorption structure of the portable integrated UAV reconnaissance, strike, and lure equipment, reverse rotation of the threaded rod causes the sealing plate to move, pushing the air in the installation cavity into the suction cup through the air pipe, enabling the suction cup to separate from the roof and facilitating the removal of the device. The limit plate is installed on the limit slider by screws, facilitating the disassembly and replacement of the limit plate. Moreover, after the limit plate is removed, the occupied space of the device can be reduced, facilitating the carrying of the device. Description of the Drawings

[0016] Figure 1 Fig. 1 is a schematic structural diagram of the first perspective of the roof adsorption structure of a portable integrated UAV reconnaissance, strike, and lure equipment proposed by the present utility model;

[0017] Figure 2 Fig. 2 is a schematic structural diagram of the second perspective of the roof adsorption structure of a portable integrated UAV reconnaissance, strike, and lure equipment proposed by the present utility model;

[0018] Figure 3 Fig. 3 is a schematic front view structure diagram of the connection of the base, placement table, suction cup, and buffer support member;

[0019] Figure 4 Fig. 4 is a schematic bottom view structure diagram of the connection between the base and the suction cup;

[0020] Figure 5 Fig. 5 is a schematic cross-sectional view structure diagram of the base, placement table, and air delivery component.

[0021] In the figures: 1. Base; 2. Air pipe; 3. Suction cup; 4. Sealing plate; 5. Threaded rod; 6. First rotation handle; 7. Sleeve; 8. Support column; 9. Placement table; 10. Limit chute; 11. Limit slider; 12. Limit plate; 13. Double-headed screw rod; 14. Second rotation handle; 15. UAV reconnaissance, strike, and lure integrated equipment body. Detailed Embodiment

[0022] Next, the technical solutions in the embodiments of the present utility model will be clearly and completely described in conjunction with the accompanying drawings in the embodiments of the present utility model. Obviously, the described embodiments are only a part of the embodiments of the present utility model, rather than all the embodiments.

[0023] Refer to Figures 1 - 5, a roof adsorption structure for a portable integrated equipment of unmanned aerial vehicle (UAV) for reconnaissance, strike and luring, comprising a base 1 and an integrated equipment body 15 of UAV for reconnaissance, strike and luring. An installation cavity is formed in the base 1. A plurality of ventilation pipes 2 are hermetically penetrated and installed at the bottom of the base 1. Suction cups 3 are installed at the bottoms of the plurality of ventilation pipes 2. The ventilation pipes 2 are arranged to enable the air inside the suction cups 3 and the installation cavity to circulate. An air delivery component extending to the outside of the base 1 is installed in the installation cavity. The air delivery component includes a sealing plate 4 hermetically and slidably connected in the installation cavity. The sealing plate 4 slides in the installation cavity and can suck the air in the suction cups 3 into the installation cavity through the ventilation pipes 2, or input the air in the installation cavity into the suction cups 3 through the ventilation pipes 2. A threaded rod 5 is rotatably connected to the side wall of the sealing plate 4. The threaded rod 5 threadedly penetrates through the side wall of the base 1 and extends to the outside of the base 1. A first rotating handle 6 is fixedly connected to the side wall of the threaded rod 5. The first rotating handle 6 is arranged to facilitate the rotation of the threaded rod 5. When the threaded rod 5 rotates, the sealing plate 4 can slide in the installation cavity under the action of the thread engagement between it and the side wall of the base 1. A plurality of through holes communicating with the installation cavity are hermetically penetrated through the side wall of the base 1. The through holes are arranged to enable the air in the installation cavity on the side of the sealing plate 4 away from the ventilation pipes 2 to be discharged or enter, so that the sealing plate 4 can move stably;

[0024] The upper end of the base 1 is connected with a placement platform 9 through a plurality of buffer supports. The buffer supports include sleeves 7 fixedly connected to the upper end of the base 1. A support column 8 extending to the outside of the sleeve 7 is slidably connected in the sleeve 7. A plurality of springs are connected between the support column 8 and the inner bottom of the sleeve 7. Anti-slip patterns are provided on both the support column 8 and the inner side wall of the sleeve 7 to increase the friction force. The springs can play a buffering role;

[0025] The integrated equipment body 15 of UAV for reconnaissance, strike and luring is placed on the upper end of the placement platform 9. A limiting component for fixing the integrated equipment body 15 of UAV for reconnaissance, strike and luring is arranged on the placement platform 9. The limiting component includes a limiting chute 10 opened on the upper end of the placement platform 9. Two limiting sliders 11 adapted to the limiting chute 10 are slidably connected in the limiting chute 10. Limiting plates 12 for fixing the integrated equipment body 15 of UAV for reconnaissance, strike and luring are connected to the upper ends of the two limiting sliders 11. The limiting plates 12 are U-shaped. The two limiting plates 12 are symmetrically arranged and can clamp and fix the integrated equipment body 15 of UAV for reconnaissance, strike and luring through both sides of it. The limiting plates 12 are connected to the upper ends of the limiting sliders 11 by screws, which is convenient for disassembly and replacement, and can be disassembled to reduce the occupied space of the device and facilitate carrying. A double-headed screw rod 13 extending to the outside of the placement platform 9 is rotatably connected to the inner side wall of the limiting chute 10. The double-headed screw rod 13 threadedly penetrates through the two limiting sliders 11. A second rotating handle 14 is fixedly connected to the end of the double-headed screw rod 13. The second rotating handle 14 is arranged to facilitate the rotation of the double-headed screw rod 13. When the double-headed screw rod 13 rotates, the two limiting sliders 11 can drive the two limiting plates 12 to approach or move away from each other under the action of its thread engagement.

[0026] The functional principle of the present utility model can be described through the following operation modes:

[0027] In the present utility model, when the roof adsorption structure of the portable integrated UAV reconnaissance, strike and lure equipment is in use, the device can be adsorbed on the roof of the vehicle through the suction cup 3. Rotating the first rotating handle 6 makes the threaded rod 5 rotate, and under the action of its thread engagement, the sealing plate 4 can be pulled to move, and the residual air between the suction cup 3 and the roof is inhaled into the installation cavity through the air pipe 2, ensuring the adsorption force of the suction cup 3 on the roof, and then the device can be stably adsorbed on the roof of the vehicle;

[0028] Place the UAV reconnaissance, strike and lure integrated equipment body 15 on the placement table 9. Rotating the second rotating handle 14 makes the double-headed screw rod 13 rotate, and under the action of its thread engagement, the two limit sliders 11 drive the two limit plates 12 to approach each other, so that the two limit plates 12 jointly act to stably clamp and fix the UAV reconnaissance, strike and lure integrated equipment body 15;

[0029] When the vehicle is driving and the reconnaissance, strike and lure work is carried out in the chassis of the UAV reconnaissance, strike and lure integrated equipment body 15, when the road is bumpy, the support column 8 slides in the sleeve 7, and cooperating with the spring can play a buffering role for the placement table 9 and the UAV reconnaissance, strike and lure integrated equipment body 15, reducing the detachment of the base 1 from the roof of the vehicle caused by the shaking of the UAV reconnaissance, strike and lure integrated equipment body 15 due to road bumps, and reducing the damage of the internal components of the UAV reconnaissance, strike and lure integrated equipment body 15 caused by shaking.

[0030] The above is only the preferred specific embodiment of the present utility model, but the protection scope of the present utility model is not limited thereto. Any person skilled in the art within the technical scope disclosed by the present utility model, according to the technical solution and the inventive concept of the present utility model, makes equivalent substitutions or changes, and all should be covered by the protection scope of the present utility model.

Claims

1. A portable UAV reconnaissance, strike and decoy integrated equipment roof adsorption structure, comprising a base (1) and a UAV reconnaissance, strike and decoy integrated equipment body (15), characterized in that: The base (1) is provided with an installation cavity, a plurality of ventilation pipes (2) are installed through the bottom of the base (1), and a suction cup (3) is installed at the bottom of each of the ventilation pipes (2). A gas transmission component extending to the outside of the base (1) is installed in the installation cavity. The upper end of the base (1) is connected to a placement table (9) through a plurality of buffer support members. The unmanned aerial vehicle reconnaissance, strike and decoy integrated equipment body (15) is placed on the upper end of the placement table (9). A limit assembly for fixing the unmanned aerial vehicle reconnaissance, strike and decoy integrated equipment body (15) is provided on the placement table (9).

2. The roof adsorption structure of a portable UAV integrated reconnaissance and decoy equipment according to claim 1 is characterized in that: The gas delivery assembly comprises a sealing plate (4) sealingly and slidably connected in the installation cavity, the side wall of the sealing plate (4) is rotatably connected to a threaded rod (5), the threaded rod (5) threads penetrate the side wall of the base (1) and extend to the outside of the base (1), and the side wall of the threaded rod (5) is fixedly connected to a first rotating handle (6).

3. The roof adsorption structure of a portable UAV integrated reconnaissance and decoy equipment according to claim 2 is characterized in that: The side wall of the base (1) is sealed and penetrated by a plurality of through holes which are in communication with the installation cavity.

4. The roof adsorption structure of a portable UAV integrated reconnaissance and decoy equipment according to claim 1 is characterized in that: The buffer support member comprises a sleeve (7) fixedly connected to the upper end of the base (1), a support column (8) extending to the outside of the sleeve (7) being slidably connected therein, and a plurality of springs being connected between the support column (8) and the inner bottom of the sleeve (7).

5. The roof adsorption structure of a portable UAV integrated reconnaissance and decoy equipment according to claim 1 is characterized in that: The limiting component comprises a limiting slide groove (10) provided at the upper end of the placement platform (9), wherein two limiting sliders (11) adapted thereto are slidably connected in the limiting slide groove (10), and the upper ends of the two limiting sliders (11) are both connected to limiting plates (12) for fixing the UAV reconnaissance, strike and decoy integrated equipment body (15), and the inner side wall of the limiting slide groove (10) is rotatably connected to a double-headed screw (13) extending to the outside of the placement platform (9), and the double-headed screw (13) is threadedly passed through the two limiting sliders (11), and the end of the double-headed screw (13) is fixedly connected to a second rotating handle (14).

6. The roof adsorption structure of a portable UAV integrated reconnaissance and decoy equipment according to claim 5 is characterized in that: The limiting plate (12) is U-shaped, and the limiting plate (12) is connected to the upper end of the limiting slider (11) by means of screws.

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