CN221300596U - Fixing frame of anti-unmanned aerial vehicle device - Google Patents

Abstract

The utility model discloses a fixing frame of an anti-unmanned aerial vehicle device, which comprises a fixing frame main body, wherein two groups of fixing components used for fixing the device main body are arranged on the surface of the fixing frame main body, and a rotating component which is convenient for the fixing frame main body to rotate is arranged at the bottom of the fixing frame main body; the bottom of the rotating assembly is provided with a lifting module for lifting the fixing frame main body; the bottom of lifting module is provided with the base, the outside of base is provided with a plurality of groups and is used for the lifting means that the mount promoted, the outside of base is provided with a plurality of groups and is used for the moving component that the mount removed, and when fixing, the lifting means extension of mount bottom is fixed the mount, and fixed subassembly presss from both sides tightly fixedly to anti-unmanned aerial vehicle device, when needs remove the mount, shrink the regulation cylinder, makes moving component contact ground, removes, and this structure makes the removal of mount become simple high-efficient.

Description

Fixing frame of anti-unmanned aerial vehicle device

Technical Field

The utility model relates to the field of anti-unmanned aerial vehicle device fixing, in particular to a fixing frame of an anti-unmanned aerial vehicle device.

Background

The anti-unmanned aerial vehicle system, also called unmanned aerial vehicle anti-control system, is a device or system specially used for resisting unmanned aerial vehicle. The unmanned aerial vehicle control system aims to interfere and destroy the operation function or the flight capability of the unmanned aerial vehicle by technical means, realize the driving or the damage of the unmanned aerial vehicle, and the working principle of the unmanned aerial vehicle control system is that the emitted radio signal is utilized to block the communication and the navigation link of the unmanned aerial vehicle so as to ensure that the unmanned aerial vehicle can not keep stable flight capability, or the emitted high-energy laser beam is utilized to destroy the electronic equipment of the unmanned aerial vehicle so as to ensure that the electronic equipment loses the flight capability, so that the purpose of driving or the damage of the unmanned aerial vehicle in a specific area is finally realized;

To this, chinese patent No. CN 211779783U discloses an unmanned aerial vehicle reaction equipment mounting bracket, including the mounting panel, install lifting unit through the screw on the mounting panel top outer wall, lifting unit includes the fixed plate, install first casing through the screw on the fixed plate top outer wall, and the welding has the second casing on the first casing top outer wall, the second casing is link up each other with first casing, first casing bottom inner wall center department installs the lead screw through the bearing, and the top of lead screw passes through the bearing rotation to be connected on second casing top inner wall, lead screw external screw thread connection has this patent of sliding block when using this mounting bracket, the user can pass through the rotation hand wheel for the lead screw drives sliding block and goes up and down in the inside lift of second casing, thereby change unmanned aerial vehicle reaction equipment's height, be favorable to improving the practicality of this mounting bracket, but also can press from both sides tight unmanned aerial vehicle reaction rifle through the effect of spring, avoid unmanned aerial vehicle reaction rifle to drop from splint.

The above-mentioned patent still has some problems when using, and the mount is inconvenient to remove in the use, makes staff's work load increase, makes the result of use of mount worsen, so the mount of anti-unmanned aerial vehicle device that needs now.

Disclosure of utility model

The utility model aims to provide a fixing frame of an anti-unmanned aerial vehicle device, and provides a fixing component and a moving component which are convenient for the fixing frame to move in the using process so as to solve the technical problems in the background art.

In order to achieve the above purpose, the present utility model provides the following technical solutions: the fixing frame of the anti-unmanned aerial vehicle device comprises a fixing frame main body, wherein two groups of fixing components used for fixing the device main body are arranged on the surface of the fixing frame main body, and a rotating component which is convenient for the fixing frame main body to rotate is arranged at the bottom of the fixing frame main body; the bottom of the rotating assembly is provided with a lifting module for lifting the fixing frame main body; the bottom of lifting module is provided with the base, the outside of base is provided with a plurality of groups of lifting unit who is used for the mount to promote, the outside of base is provided with a plurality of groups of removal subassembly that are used for the mount to remove.

Preferably, the fixing assembly comprises a fixing plate arranged in the fixing frame main body, a silica gel pad is arranged at one end of the fixing plate, two groups of first threaded holes are formed in the surfaces of two sides of the fixing frame main body, threaded rods are connected in the first threaded holes in a threaded mode, and the fixing plate is rotatably arranged at one end of each threaded rod.

Preferably, the rotating assembly comprises a rotary table arranged at the bottom of the fixing frame main body, and a damping rotary shaft is arranged in the rotary table.

Preferably, the bottom of carousel is provided with the lift shell, the top fixed mounting of lift shell has the fixed cover, the bottom of lift shell is provided with the mounting box.

Preferably, the lifting module comprises a ball screw arranged in an inner cavity of the lifting shell, a sliding seat is arranged on the outer part of the ball screw, a motor is arranged in the inner cavity of the installation box, the output end of the motor penetrates through the lifting shell and is connected with the ball screw through a key, a plurality of groups of supporting rods are arranged on the top ends of the sliding seat, and lifting seats are arranged on the top ends of the supporting rods.

Preferably, the lifting assembly comprises a plurality of groups of fixing blocks arranged on the outer side of the base, an adjusting cylinder is arranged at the bottom end of each fixing block, and a fixing seat is arranged at the bottom end of each adjusting cylinder.

Preferably, the moving assembly comprises a plurality of groups of mounting blocks arranged on the outer side of the base, and the bottom ends of the mounting blocks are rotatably provided with rollers.

Compared with the prior art, the utility model has the beneficial effects that:

1. When fixing the anti-unmanned aerial vehicle device, adjust the cylinder to the extension, fix the mount steady subaerial, fixed subassembly presss from both sides tightly the location to the anti-unmanned aerial vehicle device simultaneously, and the preventing device drops in the use, when needs shift the mount, only need make adjust the cylinder shrink, make gyro wheel contact ground, can promote the mount and remove, let the removal of mount become convenient high-efficient.

2. When the orientation needs to be adjusted by the anti-unmanned aerial vehicle device, the orientation of the anti-unmanned aerial vehicle device can be adjusted by rotating the rotating component, the operation is simple and efficient, the anti-unmanned aerial vehicle device needs to be adjusted to a certain height after being fixed, the fixed component can be driven to lift through the lifting module, lifting work of the anti-unmanned aerial vehicle device is completed, the working effect of the fixing frame is improved, and the fixing frame is convenient and efficient to use.

Drawings

FIG. 1 is a schematic diagram of the structure of the present utility model;

FIG. 2 is a schematic exploded view of a fastening assembly according to the present utility model;

FIG. 3 is a exploded view of the rotary assembly of the present utility model;

FIG. 4 is a schematic cross-sectional view of a lifting module according to the present utility model;

fig. 5 is a schematic view of a base structure of the present utility model.

In the figure: 1. a fixing frame main body; 2. a threaded rod; 3. a fixing plate; 4. a silica gel pad; 5. a turntable; 6. damping the rotating shaft; 7. lifting the shell; 8. a mounting box; 9. a fixed cover; 10. a ball screw; 11. a motor; 12. a slide; 13. a support rod; 14. a lifting seat; 15. a base; 16. a fixed block; 17. adjusting a cylinder; 18. a fixing seat; 19. a mounting block; 20. and a roller.

Detailed Description

The following description of the embodiments of the present utility model will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present utility model, but not all embodiments. All other embodiments, which can be made by those skilled in the art based on the embodiments of the utility model without making any inventive effort, are intended to be within the scope of the utility model.

The present utility model provides: the fixing frame of the anti-unmanned aerial vehicle device comprises a fixing frame main body 1, wherein two groups of fixing components for fixing the device main body are arranged on the surface of the fixing frame main body 1, and a rotating component which is convenient for the fixing frame main body 1 to rotate is arranged at the bottom of the fixing frame main body 1; the bottom of the rotating component is provided with a lifting module for lifting the fixing frame main body 1; the bottom of lifting module is provided with base 15, and the outside of base 15 is provided with a plurality of groups of lifting unit who is used for the mount to promote, and the outside of base 15 is provided with a plurality of groups of moving unit who is used for the mount to remove.

As preferred, fixed subassembly is including installing in the inside fixed plate 3 of mount main part 1, the one end of fixed plate 3 is provided with silica gel pad 4, two sets of first screw holes have been seted up on the both sides surface of mount main part 1, first threaded hole threaded connection has threaded rod 2, the one end at threaded rod 2 is installed in the rotation of fixed plate 3, the mount main part 1 of setting provides the space for the placement of anti-unmanned aerial vehicle device, also provide the position for fixed subassembly's setting, make fixed subassembly's normal work provide the basis, threaded rod 2 and first screw hole collaborative work simultaneously, make the fixed plate 3 of rotating the installation in threaded rod 2 one end tighten up to anti-unmanned aerial vehicle device, and then reach the effect to anti-unmanned aerial vehicle device clamp fastening, the silica gel pad 4 of setting plays and prevents that fixed plate 3 from producing wearing and tearing to anti-unmanned aerial vehicle device's surface, this structure makes anti-unmanned aerial vehicle device work that can be stable.

Further, rotating assembly is including installing in the carousel 5 of mount main part 1 bottom, and the internally mounted of carousel 5 has damping pivot 6, and the carousel 5 and the damping pivot 6 collaborative work of setting for mount main part 1 is rotated, and then accomplishes the orientation to anti-unmanned aerial vehicle and adjusts, makes anti-unmanned aerial vehicle's orientation adjust convenient.

Still further, the lifting shell 7 of carousel 5 bottom, lifting shell 7's top fixed mounting has fixed lid 9, and lifting shell 7's bottom is provided with mounting box 8, and lifting shell 7 of setting provides the space for lifting module's installation, and fixed lid 9 of setting has played spacing effect to lifting module, makes the mount can steady rise, and then makes anti-unmanned aerial vehicle device can steady rise, and this structure makes anti-unmanned aerial vehicle device's fixed height adjust conveniently.

It is worth explaining that the lifting module includes the ball screw 10 that sets up in the lift shell 7 inner chamber, the externally mounted of ball screw 10 has slide 12, be provided with motor 11 in the inner chamber of install bin 8, the output of motor 11 runs through lift shell 7 and ball screw 10 key connection, a plurality of sets of bracing pieces 13 are installed to the upper end of slide 12, lifting seat 14 is installed on the top of bracing piece 13, the motor 11 work of setting, drive ball screw 10 and rotate, and then drive the slide 12 on ball screw 10 surface and slide from top to bottom, and then drive bracing piece 13 and reciprocate, and then drive lifting seat 14 and reciprocate, thereby make the anti-unmanned device of fixed completion can adjust from top to bottom, make anti-unmanned device's altitude mixture control convenient.

Specifically, the lifting assembly includes a plurality of fixed blocks 16 of installing in the base 15 outside, the bottom of fixed block 16 is provided with adjusting cylinder 17, the bottom of adjusting cylinder 17 is provided with fixing base 18, adjusting cylinder 17 work of setting, adjust the distance of base 15 and ground, make gyro wheel 20 get contact or leave ground, thereby reach the effect to the removal of mount, the fixed block 16 of setting provides the fulcrum for adjusting cylinder 17 support mount, make the mount can rise or descend, the fixing base 18 of setting contacts ground under the condition of adjusting cylinder 17 extension, make the mount can be fixed, this structure makes the mount remove conveniently.

In addition, remove the subassembly including installing in a plurality of groups installation piece 19 in the base 15 outside, the gyro wheel 20 is installed in the bottom rotation of installation piece 19, and the base 15 of setting provides the position for the installation of gyro wheel 20 and lifting means, makes the mount can steady fixed with remove, and the installation piece 19 of setting provides the space for the installation of gyro wheel 20, makes the mount can fix or remove under lifting means's effect, makes the fixed and removal of mount become simple high-efficient.

Although embodiments of the present utility model have been shown and described, it will be understood by those skilled in the art that various changes, modifications, substitutions and alterations can be made therein without departing from the principles and spirit of the utility model, the scope of which is defined in the appended claims and their equivalents.

Claims (7)

1. The utility model provides a prevent mount of unmanned aerial vehicle device which characterized in that: the device comprises a fixing frame main body (1), wherein two groups of fixing components used for fixing the device main body are arranged on the surface of the fixing frame main body (1), and a rotating component which is convenient for the fixing frame main body (1) to rotate is arranged at the bottom of the fixing frame main body (1);

The bottom of the rotating assembly is provided with a lifting module for lifting the fixing frame main body (1);

The lifting module is characterized in that a base (15) is arranged at the bottom of the lifting module, a plurality of groups of lifting assemblies used for lifting the fixing frame are arranged on the outer side of the base (15), and a plurality of groups of moving assemblies used for moving the fixing frame are arranged on the outer side of the base (15).

2. The mount for an anti-drone assembly of claim 1, wherein: the fixing assembly comprises a fixing plate (3) arranged inside a fixing frame main body (1), a silica gel pad (4) is arranged at one end of the fixing plate (3), two groups of first threaded holes are formed in the surfaces of two sides of the fixing frame main body (1), threaded rods (2) are connected in the first threaded holes in a threaded mode, and the fixing plate (3) is rotatably arranged at one end of each threaded rod (2).

3. The mount for an anti-drone assembly of claim 1, wherein: the rotating assembly comprises a rotating disc (5) arranged at the bottom of the fixing frame main body (1), and a damping rotating shaft (6) is arranged in the rotating disc (5).

4. A mount for an anti-drone assembly as claimed in claim 3, wherein: the bottom of carousel (5) is provided with lift shell (7), the top fixed mounting of lift shell (7) has fixed lid (9), the bottom of lift shell (7) is provided with install bin (8).

5. The mount for an anti-drone assembly of claim 4, wherein: the lifting module comprises a ball screw (10) arranged in an inner cavity of a lifting shell (7), a sliding seat (12) is arranged outside the ball screw (10), a motor (11) is arranged in the inner cavity of a mounting box (8), the output end of the motor (11) penetrates through the lifting shell (7) and is connected with the ball screw (10) in a key manner, a plurality of groups of supporting rods (13) are arranged at the top ends of the sliding seat (12), and lifting seats (14) are arranged at the top ends of the supporting rods (13).

6. The mount for an anti-drone assembly of claim 1, wherein: the lifting assembly comprises a plurality of groups of fixed blocks (16) arranged on the outer side of the base (15), an adjusting cylinder (17) is arranged at the bottom end of each fixed block (16), and a fixing seat (18) is arranged at the bottom end of each adjusting cylinder (17).

7. The mount for an anti-drone assembly of claim 6, wherein: the movable assembly comprises a plurality of groups of mounting blocks (19) arranged on the outer side of the base (15), and rollers (20) are rotatably arranged at the bottom ends of the mounting blocks (19).