Full-band directional unmanned aerial vehicle control equipment

Abstract

The utility model discloses full-band directional unmanned aerial vehicle control equipment which comprises a hollow column, the top of the hollow column is provided with a hollow column in a penetrating mode, the hollow column is connected with the hollow column in a sliding mode, the hollow column is provided with a lifting mechanism, the top of the hollow column is provided with an unmanned aerial vehicle control instrument, and the bottom of the unmanned aerial vehicle control instrument is fixedly connected with a connecting block. The top of the hollow column is inserted into the connecting block, a plug pin slidably connected with the connecting block is arranged on the connecting block in a penetrating mode, the outer wall of the plug pin is sleeved with a spring, the two ends of the spring are fixedly connected with the connecting block and the plug pin respectively, an inserting groove is formed in the hollow column, and the plug pin is inserted into the inserting groove. The bottom of the hollow column is fixedly connected with a base. The height of the unmanned aerial vehicle control equipment can be adjusted through the lifting mechanism, so that the signal transmitting and receiving quality of the unmanned aerial vehicle control equipment is good; and through cooperation of the inserted pins and the insertion grooves, the unmanned aerial vehicle control equipment can be rapidly disassembled and assembled, and operation is easy.

Description

Technical Field

[0001] The utility model relates to the technical field of unmanned aerial vehicle (UAV) control equipment, and in particular to a full-band directional UAV control equipment. Background Art

[0002] The rapid development of the drone industry has brought convenience to various industries, but it has also brought unprecedented difficulty to drone management. With the widespread use of drones, many potential safety issues caused by "illegal flying" of aircraft have emerged, so drone control equipment is needed.

[0003] In order to ensure the safety of the destination, existing drone control equipment is usually installed on the roof of the destination. The existing drone control equipment is fixed at a fixed height. When the drone control equipment is low, the information it transmits and receives is blocked, resulting in poor information quality. In addition, the existing drone control equipment is usually fixed in place. When the drone control equipment is damaged or needs to be regularly inspected and maintained, it is inconvenient for the staff to quickly disassemble and remove the drone control equipment. In order to solve the above problems, this application proposes a full-band directional drone control device. Utility Model Content

[0004] The purpose of the utility model is to solve the shortcomings of the existing technology and propose a full-band directional drone control device, which can adjust the height of the drone control device through a lifting mechanism to improve the signal transmission and reception quality; by setting the combination of pins and slots, the drone control device can be quickly disassembled and assembled, and the operation is simple.

[0005] In order to achieve the above purpose, the present invention adopts the following technical solutions:

[0006] A full-band directional drone control device comprises a hollow column, wherein a hollow column is provided on the top of the hollow column and is slidably connected to the hollow column, a lifting mechanism is provided on the hollow column, a drone controller is provided on the top of the hollow column, and a connecting block is fixedly connected to the bottom of the drone controller, the top of the hollow column is inserted into the connecting block, a latch is provided on the connecting block and is slidably connected to the connecting block, a spring is provided on the outer wall of the latch, and the two ends of the spring are respectively fixedly connected to the connecting block and the latch, a slot is provided on the hollow column, and the latch is inserted into the slot, and the bottom of the hollow column is fixedly connected to the base, and a signal receiving module, a signal analysis module, a control module, a signal transmitting module and a signal amplification module are provided in the drone controller.

[0007] Preferably, the lifting mechanism includes a T-shaped rod passing through the hollow column and rotatably connected thereto, the end of the T-shaped rod is fixedly connected to a driving bevel gear, the driving bevel gear is engaged with a driven bevel gear, and the driven bevel gear is provided with a threaded rod coaxially fixedly connected thereto, the bottom of the threaded rod is rotatably connected to the inner bottom of the hollow column, and the threaded rod is threadedly connected to the hollow column.

[0008] Preferably, an anti-slip block is fixedly connected to the outer wall of the hollow column, the anti-slip block is located in the hollow column and slidably connected to the inner wall thereof, and the cross section of the anti-slip block is rectangular.

[0009] Preferably, the outer wall of the threaded rod is provided with an external thread, the hollow column is provided with a groove, and the inner wall of the groove is provided with an internal thread matching the external thread.

[0010] Preferably, a mounting groove is provided at the bottom of the connecting block, and the top of the hollow column is inserted into the mounting groove.

[0011] Preferably, a plurality of through holes are formed through the base, and the positions of the plurality of through holes are distributed at equal intervals.

[0012] Preferably, the signal receiving module is electrically connected to the signal analyzing module, the signal analyzing module is electrically connected to the control module, the control module is electrically connected to the signal transmitting module, and the signal transmitting module is electrically connected to the signal amplifying module.

[0013] Compared with the prior art, the present invention has the following beneficial effects:

[0014] 1. The staff holds the T-shaped rod and rotates it to drive the active bevel gear, driven bevel gear, and threaded rod to rotate, so that the hollow column and the UAV controller can be raised and lowered. The height of the UAV controller can be adjusted to an appropriate height, and the subsequent signal transmission and reception effects are better.

[0015] 2. The staff holds the pin and moves it away from the connecting block. The movement of the pin drives the spring to stretch until the pin is out of the slot. The connecting block can be pulled out from the hollow column, realizing the disassembly of the drone controller. The operation is simple and the drone controller can be quickly disassembled and assembled to realize the maintenance of the drone controller.

[0016] In summary, the height of the drone control equipment can be adjusted through the lifting mechanism to optimize the signal transmission and reception quality; by setting the combination of pins and slots, the drone control equipment can be quickly disassembled and assembled, and the operation is simple. BRIEF DESCRIPTION OF THE DRAWINGS

[0017] Figure 1 This is a first structural diagram of a full-band directional UAV control device proposed in the utility model;

[0018] Figure 2 This is a second structural diagram of a full-band directional UAV control device proposed in the utility model;

[0019] Figure 3 This is a first cross-sectional schematic diagram of a full-band directional UAV control device proposed in the present invention;

[0020] Figure 4 This is a second cross-sectional schematic diagram of a full-band directional UAV control device proposed in the present invention;

[0021] Figure 5 This is a system diagram of a full-band directional drone control device proposed in this utility model.

[0022] In the figure: 1 hollow column, 2 hollow column, 3 T-shaped rod, 4 driving bevel gear, 5 driven bevel gear, 6 threaded rod, 7 connecting block, 8 UAV controller, 9 pin, 10 spring, 11 slot, 12 base, 13 signal receiving module, 14 signal analysis module, 15 control module, 16 signal transmitting module, 17 signal amplification module. DETAILED DESCRIPTION

[0023] The technical solutions in the embodiments of the present invention will be described clearly and completely below in conjunction with the drawings in the embodiments of the present invention. Obviously, the described embodiments are only part of the embodiments of the present invention, rather than all the embodiments.

[0024] Reference Figure 1-Figure 5 The top of the hollow column 1 is provided with a hollow column 2 which is slidably connected to it. The outer wall of the hollow column 2 is fixedly connected with an anti-falling block, which is located in the hollow column 1 and is slidably connected to its inner wall. The cross section of the anti-falling block is rectangular, which can limit the hollow column 2 to make it lift and move. A lifting mechanism is provided on the hollow column 1. The lifting mechanism includes a T-shaped rod 3 that penetrates the hollow column 1 and is rotatably connected to it. The end of the T-shaped rod 3 is fixedly connected to an active bevel gear 4, which meshes with a driven bevel gear 5. The driven bevel gear 5 is provided with a threaded rod 6 coaxially fixedly connected to it. The bottom of the threaded rod 6 is rotatably connected to the inner bottom of the hollow column 1, and the threaded rod 6 is threadedly connected to the hollow column 2. The outer wall of the threaded rod 6 is provided with an external thread, and a groove is opened on the hollow column 2. The inner wall of the groove is provided with an internal thread matching the external thread. The height of the drone controller 8 can be adjusted by the lifting mechanism, which has a good effect on the transmission and reception of subsequent signals.

[0025] A drone controller 8 is provided on the top of the hollow column 2. The drone controller 8 interferes with the drone's navigation and communication systems by emitting full-frequency radio waves of matching frequencies, forcing it to land or return to the take-off point. The drone controller 8 is installed with a high-gain directional antenna, which can transmit signals and accurately strike the drone; a connecting block 7 is fixedly connected to the bottom of the drone controller 8, and the top of the hollow column 2 is inserted into the connecting block 7. A mounting groove is provided at the bottom of the connecting block 7, and the top of the hollow column 2 is inserted into the mounting groove. A pin 9 is provided on the connecting block 7 for sliding connection therewith, and a spring 10 is provided on the outer wall of the pin 9. The two ends of the spring 10 are respectively fixedly connected to the connecting block 7 and the pin 9. A slot 11 is provided on the hollow column 2, and the pin 9 is inserted into the slot 11. By inserting the pin 9 into the slot 11 or pulling out the pin 9, the drone controller 8 can be quickly installed and disassembled, and the drone controller 8 can be quickly repaired.

[0026] The bottom of the hollow column 1 is fixedly connected to a base 12, and a plurality of through holes are opened through the base 12. The positions of the plurality of through holes are distributed at equal intervals. The device can be installed and fixed by the cooperation of bolts and through holes. A signal receiving module 13, a signal analysis module 14, a control module 15, a signal transmitting module 16 and a signal amplifying module 17 are provided in the drone control instrument 8. The signal receiving module 13 is electrically connected to the signal analysis module 14, the signal analysis module 14 is electrically connected to the control module 15, the control module 15 is electrically connected to the signal transmitting module 16, and the signal transmitting module 16 is electrically connected to the signal amplifying module 17. The signal receiving module 13 can receive wireless signals in the environment in real time, including signals from drones; The signal analysis module 14 can demodulate, analyze and identify the received wireless signals to determine the location and working frequency band of the UAV; the control module 15 can control the system to decide whether to interfere with the UAV, as well as the type and strength of the interference signal based on the signal analysis results; the signal transmission module 16 can generate an interference signal with the same working frequency band as the UAV, and transmit it through a high-gain directional antenna to accurately strike the UAV. The signal transmission module 16 can cover all frequency bands commonly used by UAVs, including 2.4GHz, 5.8GHz, etc., to achieve comprehensive interference; the signal amplification module 17 can amplify the generated interference signal to improve the interference effect and ensure that the signal can cover the target UAV.

[0027] In the present invention, the base 12 can be installed on the ground or roof by the cooperation of bolts and through holes, completing the installation and fixation of the device; the staff holds the T-bar 3 and rotates it to drive the active bevel gear 4, the driven bevel gear 5, and the threaded rod 6 to rotate, so that the hollow column 2 and the drone controller 8 are raised and lowered, and the height of the drone controller 8 can be adjusted to an appropriate height, so that the subsequent signal transmission and reception effects are good; the signal receiving module 13 can receive wireless signals in the environment in real time, including the signals of the drone; the signal analysis module 14 can demodulate, analyze and identify the received wireless signals to determine the position and working frequency band of the drone; the control module 15 can control the system to decide whether to interfere with the drone according to the signal analysis results, as well as the type and strength of the interfered signal; the signal transmitting module 1 6 can generate an interference signal with the same working frequency band as the drone, and transmit it through a high-gain directional antenna to accurately strike the drone, and the signal transmission module 16 can cover all frequency bands commonly used by drones, including 2.4GHz, 5.8GHz, etc., to achieve comprehensive interference; the generated interference signal can be amplified by the signal amplification module 17 to improve the interference effect and ensure that the signal can cover the target drone; when the drone controller 8 needs to be repaired, the staff holds the pin 9 and moves it away from the connecting block 7. The movement of the pin 9 drives the spring 10 to stretch until the pin 9 is disengaged from the slot 11, and the connecting block 7 can be pulled out from the hollow column 2, realizing the disassembly of the drone controller 8. The operation is simple, and the drone controller 8 can be quickly disassembled and assembled to realize the maintenance of the drone controller 8.

[0028] The utility model solves the problem that the drone control equipment in the prior art is fixed in height by setting a lifting mechanism, a pin and a slot. When the drone control equipment is low, the information it transmits and receives is blocked, resulting in poor information quality. In addition, the existing drone control equipment is usually fixed in place. When the drone control equipment is damaged or needs to be regularly inspected and maintained, it is inconvenient for the staff to quickly disassemble and remove the drone control equipment.

Claims

1. A full-band directional drone control device, comprising a hollow column (1), characterized in that: The top of the hollow column (1) is penetrated by a hollow column (2) connected to the hollow column in a sliding manner. The hollow column (1) is provided with a lifting mechanism. The top of the hollow column (2) is provided with a UAV controller (8). The bottom of the UAV controller (8) is fixedly connected with a connecting block (7). The top of the hollow column (2) is inserted into the connecting block (7). The connecting block (7) is penetrated by a latch (9) connected to the connecting block in a sliding manner. The outer wall of the latch (9) is provided with a spring (10). The two ends of the spring (10) are respectively fixedly connected to the connecting block (7) and the latch (9). The hollow column (2) is provided with a slot (11). The latch (9) is inserted into the slot (11). The bottom of the hollow column (1) is fixedly connected with a base (12). The UAV controller (8) is provided with a signal receiving module (13), a signal analysis module (14), a control module (15), a signal transmitting module (16) and a signal amplification module (17).

2. The full-band directional drone control device according to claim 1, characterized in that: The lifting mechanism comprises a T-shaped rod (3) passing through the hollow column (1) and being rotatably connected thereto; the end of the T-shaped rod (3) is fixedly connected to a driving bevel gear (4); the driving bevel gear (4) is meshed with a driven bevel gear (5); a threaded rod (6) passing through the driven bevel gear (5) and being coaxially fixedly connected thereto is provided; the bottom of the threaded rod (6) is rotatably connected to the inner bottom of the hollow column (1); and the threaded rod (6) is threadedly connected to the hollow column (2).

3. The full-band directional drone control device according to claim 1, characterized in that: An anti-slip block is fixedly connected to the outer wall of the hollow column (2); the anti-slip block is located inside the hollow column (1) and is slidably connected to the inner wall thereof; and the cross section of the anti-slip block is rectangular.

4. The full-band directional drone control device according to claim 2, characterized in that: The outer wall of the threaded rod (6) is provided with an external thread, the hollow column (2) is provided with a groove, and the inner wall of the groove is provided with an internal thread matching the external thread.

5. The full-band directional drone control device according to claim 1, characterized in that: The bottom of the connecting block (7) is provided with a mounting groove, and the top of the hollow column (2) is inserted into the mounting groove.

6. The full-band directional drone control device according to claim 1, characterized in that: The base (12) is provided with a plurality of through holes, and the positions of the plurality of through holes are distributed at equal intervals.

7. The full-band directional drone control device according to claim 1, characterized in that: The signal receiving module (13) is electrically connected to the signal analysis module (14), the signal analysis module (14) is electrically connected to the control module (15), the control module (15) is electrically connected to the signal transmitting module (16), and the signal transmitting module (16) is electrically connected to the signal amplifying module (17).

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