CN218124714U - Structure of anti-unmanned aerial vehicle equipment - Google Patents
Structure of anti-unmanned aerial vehicle equipment Download PDFInfo
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- CN218124714U CN218124714U CN202221885810.6U CN202221885810U CN218124714U CN 218124714 U CN218124714 U CN 218124714U CN 202221885810 U CN202221885810 U CN 202221885810U CN 218124714 U CN218124714 U CN 218124714U
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- 238000009434 installation Methods 0.000 claims abstract description 18
- 230000000694 effects Effects 0.000 abstract description 6
- 238000001514 detection method Methods 0.000 abstract description 4
- 238000005516 engineering process Methods 0.000 abstract description 3
- 238000003860 storage Methods 0.000 description 5
- 210000003813 thumb Anatomy 0.000 description 4
- 230000006698 induction Effects 0.000 description 3
- 210000001503 joint Anatomy 0.000 description 3
- 230000006978 adaptation Effects 0.000 description 2
- 230000002411 adverse Effects 0.000 description 2
- 238000003780 insertion Methods 0.000 description 2
- 230000037431 insertion Effects 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 238000003825 pressing Methods 0.000 description 2
- 230000002265 prevention Effects 0.000 description 2
- 241000256103 Simuliidae Species 0.000 description 1
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Abstract
The utility model discloses a structure of anti-unmanned aerial vehicle equipment, relate to the unmanned air vehicle technology field, solve the inconvenient to dismantle of the installation of current anti-unmanned aerial vehicle equipment to and the difficult technical problem of all-round detection, including navigation trapping equipment and support frame, navigation trapping equipment with be equipped with rotating part between the support frame, rotating part includes the revolving stage, the both sides of revolving stage are connected with the side support frame, the top of side support frame is equipped with the upper mounting panel, the upper mounting panel through the locker with navigation trapping equipment fixed connection, the bottom of revolving stage is equipped with the workstation, the inside of workstation is provided with the rotating machine, the output shaft fixed connection of rotating machine the revolving stage, the bottom of workstation is equipped with the lower mounting panel, the lower mounting panel through the locker with support frame fixed connection; the utility model has the advantages of convenient assembly and disassembly, simple and portable performance and good signal detection effect.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field, more specifically are structure technical field who relates to anti-unmanned aerial vehicle equipment.
Background
In recent years, unmanned aerial vehicles have been explosively grown in both military and civilian applications. However, at present, no clear principal department exists in the management and control aspect of the low-altitude unmanned aerial vehicle in China, and related laws and regulations are not perfect, so that all links from production, sale to flight use of the unmanned aerial vehicle are in an out-of-control state. A large number of 'black flies' emerge endlessly, which brings a serious challenge to public safety and important target safety protection.
The technology utilizes the reality that the low-slow small unmanned aerial vehicle usually depends on GNSS (Global Navigation satellite System) to realize Navigation and positioning, and induces the unmanned aerial vehicle to obtain wrong positioning information by transmitting false signals which are the same as or similar to real GNSS signals and have stronger power, thereby realizing effective driving away of the unmanned aerial vehicle or successful decoy. Compared with other management and control technologies, the trap interference can take effect on all low and slow small targets in a certain airspace range at the same time, accurate control on the targets can be achieved, and a good management and control effect is achieved.
The patent with publication number CN213512903U discloses an unmanned aerial vehicle control trapping device, which comprises an interferometer main body, a first mounting plate and a bottom plate, wherein the interferometer main body is mounted on the top surface of the first mounting plate, an adjustable support rod is vertically fixed on the top surface of the bottom plate, a storage box is mounted at the top end of the adjustable support rod, a storage cavity is formed in the storage box, the first mounting plate is slidably mounted in the storage cavity, and an operating assembly for controlling the first mounting plate to move is further distributed in the storage cavity; the utility model discloses an unmanned aerial vehicle control lures equipment, through the receiver that sets up combine the first mounting panel of portable installation, can accomodate the interferometer main part in the accomodate intracavity of receiver and carry out safety protection in idle time, guarantee the subsequent reliable use of interferometer main part, improved the life of interferometer main part greatly; the height of the interference instrument main body can be adjusted, and the application range of the equipment is further improved.
The prior art described above has the following drawbacks: 1. the installation and the disassembly of each part of the trapping device are inconvenient, and the trapping device is not easy to carry; 2. the trapping device cannot rotate and shift, and is difficult to realize 360-degree omnibearing emission of interference signals, so that the effect of navigation trapping is influenced.
SUMMERY OF THE UTILITY MODEL
The utility model aims to provide a: dismantle inconveniently in order to solve current anti-unmanned aerial vehicle equipment fixing to and the all-round technical problem who listens the difficulty, the utility model provides a structure of anti-unmanned aerial vehicle equipment.
The utility model discloses a realize above-mentioned purpose and specifically adopt following technical scheme:
the utility model provides a structure of anti-unmanned aerial vehicle equipment, includes navigation decoy equipment and support frame, the navigation decoy equipment with be equipped with rotating part between the support frame, rotating part includes the revolving stage, the both sides of revolving stage are connected with the side support frame, the top of side support frame is equipped with the mounting panel, go up the mounting panel pass through the locker with navigation decoy equipment fixed connection, the bottom of revolving stage is equipped with the workstation, the inside of workstation is provided with rotates the motor, the output shaft fixed connection who rotates the motor the revolving stage, the bottom of workstation is equipped with down the mounting panel, the mounting panel down pass through the locker with support frame fixed connection.
The use and working process comprises the following steps: during installation, the lower mounting plate of the rotating component is locked with the support frame through the locker, the upper mounting plate of the rotating component is locked with the navigation decoy equipment through the locker, the locking component can be quickly locked through one-step operation of the locker to complete installation of the device, similarly, the device can be disassembled through one-step operation, the structure is simple, the use and the carrying are convenient, other tools are not needed, and the convenience and the practicability of disassembling and installing of the anti-unmanned aerial vehicle equipment are improved; during the use, the inside rotation motor of workstation rotates, drives the revolving stage rotatory, and then realizes the all-round rotation of navigation trapping equipment, helps navigation trapping to launch the sensing signal all-round, realizes functions such as driving away, compelling to land, course induction to unmanned aerial vehicle.
Furthermore, an asymmetric flange is arranged on the upper mounting plate, a groove is formed in the bottom of the navigation decoy device, and the flange is matched with the groove.
Further, the locking device comprises a thumb-turning type locking device and a button type locking device.
Furthermore, the locking devices are symmetrically arranged on two sides of the upper mounting plate and the lower mounting plate.
Furthermore, locking holes matched with the locking device are formed in the bottom of the navigation trapping device and the top of the supporting frame.
Furthermore, a spiral antenna and a GPS antenna are fixedly installed at the top end of the navigation decoy device.
Furthermore, the GPS antenna is installed on the navigation decoy device through a thread, and the spiral antenna is installed on the navigation decoy device through an L-shaped installation seat.
Furthermore, the spiral antenna is vertically installed on one side of the L-shaped installation seat, and the other side of the L-shaped installation seat is fixedly installed on the navigation decoy device through a locker or a bolt.
Furthermore, a positioning block is further arranged at the top end of the navigation trapping device, and a positioning notch matched with the positioning block is formed in the non-geometric central position of the L-shaped mounting seat, which is close to one side of the navigation trapping device.
The utility model has the advantages as follows:
1. the utility model locks the lower mounting plate of the rotating part with the support frame through the locker, locks the upper mounting plate of the rotating part with the navigation trapping device through the locker, can quickly lock the part to complete the installation of the device through one-step operation of the locker, can complete the disassembly of the device through one-step operation, has simple structure, convenient use and carrying, does not need to use other tools, and improves the convenience and the practicability of the disassembly and the installation of the anti-unmanned aerial vehicle device; in addition, the rotating motor inside the workbench rotates to drive the rotary table to rotate, so that the all-directional rotation of the navigation trapping device is realized, the navigation trapping device is facilitated to emit detection signals all-directionally, and the functions of driving away, forced landing, course induction and the like of the unmanned aerial vehicle are realized.
2. The utility model discloses a flange asymmetric setting on last mounting panel, when the device installation, with the flange butt joint embedding to the recess in, accomplish the installation, this kind of asymmetric anti-reverse plug structure can effectively avoid the navigation to lure equipment to install with rotating part's butt joint department mistake, fool's a key dress second, simple easy operation and location accuracy.
3. The thumb-turning type locker or the button type locker of the utility model is pre-installed on the upper mounting plate and the lower mounting plate, and the part can be quickly locked only by screwing the knob of the thumb-turning type locker or pressing the button of the button type locker; the GPS antenna is arranged on the navigation trapping device through threads, and the spiral antenna is arranged on the navigation trapping device through an L-shaped mounting seat, so that the navigation trapping device is simple, convenient and easy to operate; when the helical antenna is installed, the positioning notch is aligned to the positioning block at the top end of the navigation trapping device, and the reverse insertion prevention design can effectively prevent adverse effects such as interference and the like caused by reverse installation direction of the helical antenna.
Drawings
Fig. 1 is a schematic structural diagram of the present invention;
fig. 2 is a schematic side view of the present invention;
FIG. 3 is an exploded view of the whole machine of the present invention;
FIG. 4 is a schematic structural view of the rotating member of the present invention;
figure 5 is an enlarged view of the utility model at a in figure 4;
fig. 6 is a schematic view of the installation structure of the navigation decoy device of the present invention;
fig. 7 is a schematic view of the mounting structure of the helical antenna of the present invention;
reference numerals: the mobile navigation system comprises a 1-spiral antenna, a 2-GPS antenna, a 3-navigation decoy device, a 4-rotating part, a 401-upper mounting plate, a 402-side support frame, a 403-rotary table, a 404-workbench, a 405-lower mounting plate, a 406-locker, a 5-support frame, a 6-groove, a 7-flange, an 8-L-shaped mounting seat, a 9-positioning notch and a 10-positioning block.
Detailed Description
In order to make the objects, technical solutions and advantages of the embodiments of the present invention clearer, the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are some, but not all, embodiments of the present invention. The components of embodiments of the present invention, as generally described and illustrated in the figures herein, may be arranged and designed in a wide variety of different configurations.
Thus, the following detailed description of the embodiments of the present invention, presented in the accompanying drawings, is not intended to limit the scope of the invention, as claimed, but is merely representative of selected embodiments of the invention. Based on the embodiments of the present invention, all other embodiments obtained by a person skilled in the art without making creative efforts belong to the protection scope of the present invention.
Example 1
As shown in fig. 1 to 5, a structure of anti-unmanned aerial vehicle device includes a navigation trap device 3 and a support frame 5, a rotating component 4 is arranged between the navigation trap device 3 and the support frame 5, the rotating component 4 includes a rotating table 403, two sides of the rotating table 403 are connected with a side support frame 402, an upper mounting plate 401 is fixedly connected to the top of the side support frame 402, the upper mounting plate 401 is fixedly connected to the navigation trap device 3 through a locker 406, a workbench 404 is arranged at the bottom of the rotating table 403, a rotating motor is arranged inside the workbench 404, an output shaft of the rotating motor is fixedly connected to the rotating table 403, a lower mounting plate 405 is fixedly connected to the bottom of the workbench 404, and the lower mounting plate 405 is fixedly connected to the support frame 5 through the locker 406.
During installation, the lower mounting plate 405 of the rotating component 4 is locked with the support frame 5 through the locker 406, the upper mounting plate 401 of the rotating component 4 is locked with the navigation trapping device 3 through the locker 406, the locker 406 can quickly lock the components to complete the installation of the device through one-step operation, similarly, the device can be disassembled through one-step operation, the structure is simple, the use and the carrying are convenient, other tools are not needed, compared with the traditional bolt fastening, the device is quicker and more efficient, and the convenience and the practicability of disassembling and installing the anti-unmanned aerial vehicle device are improved; when the unmanned aerial vehicle driving device is used, the rotating motor in the workbench 404 rotates to drive the rotary table 403 to rotate, so that the all-directional rotation of the navigation trapping device 3 is realized, the navigation trapping device is facilitated to emit detection signals all-directionally, and the functions of driving away, forced landing, course induction and the like of the unmanned aerial vehicle are realized.
Example 2
As shown in fig. 6, based on embodiment 1, the utility model provides a structure of anti-unmanned aerial vehicle equipment, go up and be provided with an asymmetric flange 7 on the mounting panel 401, the navigation is deceived the equipment 3 bottom and is provided with a recess 6, flange 7 with recess 6 looks adaptation.
The flange 7 is asymmetrically arranged on the upper mounting plate 401, when the device is mounted, the flange 7 is butt-jointed and embedded into the groove 6 to complete mounting, and the asymmetric anti-reverse-plugging structure can effectively avoid that the navigation trapping device 3 is wrongly mounted at the butt joint part of the rotating component 4, so that the device is simple and easy to operate and is accurate in positioning.
Example 3
As shown in fig. 3, fig. 4 and fig. 5, based on embodiment 1, the utility model provides a structure of anti-unmanned aerial vehicle equipment, locker 406 symmetry sets up go up mounting panel 401 with the both sides of lower mounting panel 405, navigation lures deception equipment 3 bottom with all be equipped with in the top of support frame 5 with locker 406 matched with locking hole.
Preferably, the locking device 406 comprises a rotary thumb type locking device and a button type locking device, the rotary thumb type locking device and the button type locking device are commercially available, the rotary thumb type locking device comprises a knob, a spring, a shaft, a pin and a body with an ON/OFF mark, and a cam sleeve matched with the rotary thumb type locking device is arranged in the locking hole. The button type locker comprises a button, a wedge block, a ball, a spring and a body, wherein a sleeve which is matched with the button locker and is provided with an inner conical surface is arranged in the locking hole. The thumb-turn or button type lockers are pre-installed on the upper mounting plate 401 and the lower mounting plate 405, and the components can be quickly locked by only screwing the knob of the thumb-turn or pressing the button of the button type locker.
Example 4
As shown in fig. 3 and 7, based on embodiment 1, the utility model provides a structure of anti-unmanned aerial vehicle equipment, the top fixed mounting of navigation trapping apparatus 3 has helical antenna 1 and GPS antenna 2, GPS antenna 2 is installed through the screw thread from the area on the navigation trapping apparatus 3, helical antenna 1 is installed through L shape mount pad 8 on the navigation trapping apparatus 3, helical antenna 1 installs perpendicularly on one side of L shape mount pad 8, the another side of L shape mount pad 8 is passed through locker 406 or bolt fixed mounting and is in on the navigation trapping apparatus 3. Preferably, the spiral antenna 1 is installed on the navigation decoy device 3 through a button type locker 406.
The GPS antenna 2 is arranged on the navigation trapping device 3 through threads, and the spiral antenna 1 is arranged on the navigation trapping device 3 through the L-shaped mounting seat 8, so that the navigation trapping device is simple, convenient and easy to operate.
Example 5
As shown in fig. 7, based on embodiment 4, the utility model provides a structure of anti-unmanned aerial vehicle equipment, the top of navigation decoy equipment 3 still is equipped with locating piece 10, L shape mount pad 8 is close to the non-geometric centre position on one side of navigation decoy equipment 3 is provided with locating notch 9 of locating piece 10 looks adaptation.
When the helical antenna 1 is installed, the positioning notch 9 is aligned to the positioning block 10 at the top end of the navigation decoy equipment 3, and the reverse insertion prevention design can effectively prevent adverse effects such as interference and the like caused by reverse installation direction of the helical antenna 1.
Claims (9)
1. The utility model provides a structure against unmanned aerial vehicle equipment, lures deceiving equipment (3) and support frame (5) including the navigation, its characterized in that: navigation lures deceiving equipment (3) with be equipped with rotating part (4) between support frame (5), rotating part (4) include revolving stage (403), the both sides of revolving stage (403) are connected with side support frame (402), the top of side support frame (402) is equipped with mounting panel (401), go up mounting panel (401) through locker (406) with navigation lures deceiving equipment (3) fixed connection, the bottom of revolving stage (403) is equipped with workstation (404), the inside of workstation (404) is provided with the rotation motor, the output shaft fixed connection of rotation motor revolving stage (403), the bottom of workstation (404) is equipped with down mounting panel (405), down mounting panel (405) through locker (406) with support frame (5) fixed connection.
2. The structure of an anti-drone device according to claim 1, characterized in that: an asymmetric flange (7) is arranged on the upper mounting plate (401), a groove (6) is formed in the bottom of the navigation decoy device (3), and the flange (7) is matched with the groove (6).
3. Structure of an anti-drone device according to claim 1, characterized in that: the locking device (406) comprises a thumb-turning type locking device and a button type locking device.
4. Structure of an anti-drone device according to claim 1, characterized in that: the locking devices (406) are symmetrically arranged on two sides of the upper mounting plate (401) and the lower mounting plate (405).
5. An anti-drone device structure according to claim 4, characterized in that: locking holes matched with the locking device (406) are formed in the bottom of the navigation trapping device (3) and the top of the support frame (5).
6. The structure of an anti-drone device according to claim 1, characterized in that: the top end of the navigation decoy device (3) is fixedly provided with a spiral antenna (1) and a GPS antenna (2).
7. The structure of an anti-drone device according to claim 6, characterized in that: the GPS antenna (2) is installed on the navigation decoy device (3) through threads, and the spiral antenna (1) is installed on the navigation decoy device (3) through an L-shaped installation seat (8).
8. The structure of an anti-drone device according to claim 7, characterized in that: the spiral antenna (1) is vertically arranged on one side of the L-shaped mounting seat (8), and the other side of the L-shaped mounting seat (8) is fixedly arranged on the navigation decoy device (3) through a locker (406) or a bolt.
9. Structure of an anti-drone device according to claim 8, characterized in that: the top end of the navigation trapping device (3) is further provided with a positioning block (10), and a positioning notch (9) matched with the positioning block (10) is formed in the non-geometric central position of the L-shaped mounting seat (8) close to one side of the navigation trapping device (3).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202221885810.6U CN218124714U (en) | 2022-07-21 | 2022-07-21 | Structure of anti-unmanned aerial vehicle equipment |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202221885810.6U CN218124714U (en) | 2022-07-21 | 2022-07-21 | Structure of anti-unmanned aerial vehicle equipment |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN218124714U true CN218124714U (en) | 2022-12-23 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202221885810.6U Active CN218124714U (en) | 2022-07-21 | 2022-07-21 | Structure of anti-unmanned aerial vehicle equipment |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN218124714U (en) |
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2022
- 2022-07-21 CN CN202221885810.6U patent/CN218124714U/en active Active
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| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CP01 | Change in the name or title of a patent holder |
Address after: No.205, 2nd floor, building 2, No.88 Keyuan South Road, high tech Zone, Chengdu, Sichuan 610000 Patentee after: Sichuan Qingcheng Rongchuang Technology Co.,Ltd. Address before: No.205, 2nd floor, building 2, No.88 Keyuan South Road, high tech Zone, Chengdu, Sichuan 610000 Patentee before: Chengdu Qingcheng Rongchuang Information Technology Co.,Ltd. |
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| CP01 | Change in the name or title of a patent holder |