Rapid erecting and connecting device for unmanned aerial vehicle countering equipment

Abstract

The utility model belongs to the technical field of unmanned aerial vehicle countering equipment, and provides an unmanned aerial vehicle countering equipment rapid erecting and connecting device which comprises a connecting column, a first end of the connecting column is provided with a connecting part matched with a connecting tripod, and a second end of the connecting column extends freely; the connecting ring coaxially sleeves the connecting column and is movably connected with the connecting column; and the locking assembly is arranged on the connecting column and / or the connecting ring and used for locking the connecting ring. The rapid erecting and connecting device for the unmanned aerial vehicle countering equipment is simple in structure, reasonable in design and convenient to operate, and the unmanned aerial vehicle countering equipment can be rapidly erected conveniently.

Description

Technical Field

[0001] The utility model relates to the technical field of unmanned aerial vehicle countermeasure equipment, and in particular to a quick erection connection device for unmanned aerial vehicle countermeasure equipment. Background Art

[0002] Drone countermeasures refer to taking various measures and methods to deal with the security threats posed by drones. With the rapid development of drone technology, drones are being used more and more widely, but this also brings a series of security issues. In order to protect the safety of personnel and critical infrastructure, drone countermeasures have become increasingly important.

[0003] When countering drones, the counter-measure equipment needs to be quickly set up to achieve the best counter-measure effect. However, the connector models and standards of the current counter-measure equipment are not uniform, making it difficult to connect, and the operation of adjusting the connection device is cumbersome. The speed of setting up is slow, resulting in the problem of missing the best counter-measure opportunity. Utility Model Content

[0004] In view of the defects in the prior art, the purpose of the present utility model is to provide a connection device for quickly setting up a UAV countermeasure device, so as to solve the above-mentioned problems existing in the connection device for setting up a UAV countermeasure device in the prior art.

[0005] In order to achieve the above-mentioned purpose, the utility model provides a UAV countermeasure equipment rapid erection connection device, comprising:

[0006] A connecting column, the first end of which is provided with a connecting portion adapted to connect to a tripod, and the second end of which is freely extending;

[0007] A connecting ring, which is coaxially sleeved on the connecting post and movably connected to the connecting post; and

[0008] A locking assembly is arranged on the connecting column and / or the connecting ring and is used to lock the connecting ring.

[0009] Furthermore, the locking assembly comprises:

[0010] A locking groove is provided on the side wall of the connecting column, and a plurality of locking grooves are provided, and the plurality of locking grooves are sequentially spaced apart along the length direction of the connecting column; and

[0011] A locking pin, one end of which is inserted into the connecting ring and slidably connected to the connecting ring, and can make reciprocating linear motion between a first position and a second position, wherein when the locking pin is in the first position, the locking pin is clamped in the locking groove, and when the locking pin is in the second position, the locking pin is located outside the locking groove.

[0012] Furthermore, the locking pin comprises a locking section, a connecting section and an unlocking section which are connected in sequence, wherein the distance between the locking section and the axis of the connecting ring is greater than the distance between the unlocking section and the axis of the connecting ring.

[0013] Furthermore, two locking pins are symmetrically arranged, and the free ends of the unlocking sections of the two locking pins are fixedly connected by a connecting pin.

[0014] Furthermore, the locking assembly further comprises a driving structure, and the driving structure is used to drive the locking pin to perform reciprocating linear motion between the first position and the second position.

[0015] Furthermore, the driving structure comprises:

[0016] A driving button, a first end of which is hinged to the connecting ring, and a second end of which can perform reciprocating linear motion between a third position and a fourth position around its own hinge center line, and the locking pin is drivingly connected to the driving button, wherein when the driving button is in the third position, the locking pin is in the first position, and when the driving button is in the fourth position, the locking pin is in the second position; and

[0017] A torsion spring is arranged at the hinge center of the driving button, and its two ends are respectively hinged to the connecting ring and the driving button, and in a natural state, it has a tendency to move the driving button from the fourth position to the third position.

[0018] Furthermore, it also includes:

[0019] a button seat, the button seat being fixedly connected to the connecting ring; and

[0020] A rotating shaft bolt, wherein the first end of the driving button is hinged to the button seat through the rotating shaft bolt.

[0021] Furthermore, a sliding hole is provided on one side of the second end of the driving button facing the axis of the connecting ring, the length direction of the sliding hole extends along the length direction of the driving button, and the connecting pin is movably inserted in the sliding hole.

[0022] Furthermore, it also includes a limiting bolt, which is arranged at the first end of the driving button and is used to limit the driving button.

[0023] Furthermore, the connecting column is cylindrical, the locking groove is annular, and the inner wall of the locking groove is provided with a limiting wall that cooperates with the locking pin.

[0024] Beneficial effects of the utility model:

[0025] The UAV countermeasure equipment quick erection connection device provided by the utility model has a simple structure and a reasonable design. The connecting ring can be moved to a target position by releasing the lock on the connecting ring through the locking component. The connecting ring can be fixed in the target position by locking the connecting ring through the locking component. The UAV countermeasure equipment is quick to erect and is easy to operate. BRIEF DESCRIPTION OF THE DRAWINGS

[0026] In order to more clearly illustrate the specific implementation of the utility model or the technical solution in the prior art, the following is a brief introduction to the drawings required for the specific implementation or the prior art description. In all the drawings, similar elements or parts are generally identified by similar reference numerals. In the drawings, each element or part is not necessarily drawn according to the actual scale.

[0027] Figure 1 A three-dimensional view of a quick installation connection device for a drone countermeasure device provided in one embodiment of the utility model;

[0028] Figure 2 for Figure 1 An enlarged view of section A is shown;

[0029] Figure 3 for Figure 1 An exploded perspective view of a quick erection connection device for a drone countermeasure device is shown;

[0030] Figure 4 for Figure 3 An enlarged view of section B is shown;

[0031] Figure 5 for Figure 1 A cross-sectional view of a quick-erection connection device for drone countermeasure equipment is shown.

[0032] Reference numerals:

[0033] 100, connecting column; 110, connecting part; 200, connecting ring; 310, locking groove; 311, limiting wall; 320, locking pin; 321, locking section; 322, connecting section; 323, unlocking section; 330, connecting pin; 340, driving button; 341, sliding hole; 350, torsion spring; 360, button seat; 370, rotating shaft bolt; 380, connecting bolt; 390, limiting bolt. DETAILED DESCRIPTION

[0034] The following embodiments of the technical solution of the utility model are described in detail in conjunction with the accompanying drawings. The following embodiments are only used to more clearly illustrate the technical solution of the utility model, and are therefore only used as examples, and cannot be used to limit the protection scope of the utility model.

[0035] It should be noted that, unless otherwise specified, the technical terms or scientific terms used in this application should have the common meanings understood by technicians in the field to which the utility model belongs.

[0036] In the description of the present application, it should be understood that the terms "center", "longitudinal", "lateral", "length", "width", "thickness", "up", "down", "front", "back", "left", "right", "vertical", "horizontal", "top", "bottom", "inside", "outside", "clockwise", "counterclockwise", "axial", "radial", "circumferential" and the like indicate orientations or positional relationships based on the orientations or positional relationships shown in the accompanying drawings, and are only for the convenience of describing the present invention and simplifying the description, and do not indicate or imply that the referred device or element must have a specific orientation, be constructed and operated in a specific orientation, and therefore should not be understood as a limitation on the present invention.

[0037] In addition, the terms "first", "second", etc. are used for descriptive purposes only and cannot be understood as indicating or implying relative importance or implicitly indicating the number of technical features indicated. In the description of the present utility model, the meaning of "plurality" is more than two, unless otherwise clearly and specifically limited.

[0038] In this application, unless otherwise clearly specified and limited, the terms "installed", "connected", "connected", "fixed" and the like 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 an indirect connection through an intermediate medium, it can be the internal connection of two elements or the interaction relationship between two elements. For ordinary technicians in this field, the specific meanings of the above terms in this utility model can be understood according to specific circumstances.

[0039] In the present application, unless otherwise clearly specified and limited, a first feature being “above” or “below” a second feature may mean that the first and second features are in direct contact, or the first and second features are in indirect contact through an intermediate medium. Moreover, a first feature being “above”, “above”, and “above” a second feature may mean that the first feature is directly above or obliquely above the second feature, or simply means that the first feature is higher in level than the second feature. A first feature being “below”, “below”, and “below” a second feature may mean that the first feature is directly below or obliquely below the second feature, or simply means that the first feature is lower in level than the second feature.

[0040] like Figure 1-5 As shown, the utility model provides a rapid installation connection device for UAV countermeasure equipment, including a connecting column 100, a connecting ring 200 and a locking assembly.

[0041] The first end of the connecting column 100 is provided with a connecting portion 110 adapted to connect to a tripod, and the second end is freely extended. The connecting ring 200 is coaxially sleeved on the connecting column 100 and movably connected to the connecting column 100, and the connecting ring 200 can slide in and out from the second end of the connecting column 100. The locking assembly is provided on the connecting column 100 and / or the connecting ring 200, and the locking assembly is used to lock the connecting ring 200.

[0042] When in use, the first end of the connecting column 100 is fixedly connected to the connecting tripod, the connecting ring 200 is fixedly connected to the countermeasure device, and then the connecting ring 200 is sleeved on the connecting column 100 from the second end of the connecting column 100. At the same time, the locking assembly for the connecting ring 200 is released, so that the connecting ring 200 can move along the length direction of the connecting column 100. After the connecting ring 200 is moved to the target position, the connecting ring 200 is locked by the locking assembly, thereby achieving the purpose of locking the connecting ring 200 at the target position, and further achieving the purpose of locking the countermeasure device at the target position.

[0043] The drone countermeasure equipment quick installation connection device provided in this embodiment has a simple structure and a reasonable design, is convenient for quick installation of the drone countermeasure equipment, and is easy to operate.

[0044] In one embodiment, the locking assembly includes a locking slot 310 and a locking pin 320 .

[0045] The locking groove 310 is provided on the side wall of the connecting column 100, and a plurality of locking grooves 310 are provided, and the plurality of locking grooves 310 are sequentially spaced along the length direction of the connecting column 100. One end of the locking pin 320 is inserted into the connecting ring 200 and is slidably connected to the connecting ring 200, and the locking pin 320 can reciprocate between a first position and a second position. When the locking pin 320 is in the first position, the locking pin 320 is clamped in the locking groove 310, and when the locking pin 320 is in the second position, the locking pin 320 is located outside the locking groove 310.

[0046] During use, when it is necessary to lock the connecting ring 200, the locking pin 320 is placed in the first position so that the locking pin 320 is located in the locking groove 310, thereby achieving the purpose of locking the connecting ring 200. When it is necessary to unlock the connecting ring 200, the locking pin 320 is placed in the second position so that the locking pin 320 is located outside the locking groove 310, thereby achieving the purpose of unlocking the connecting ring 200.

[0047] The locking assembly of the drone countermeasure equipment quick erection connection device provided in this embodiment has a simple structure and a reasonable design. The purpose of locking or unlocking the connecting ring 200 can be achieved by placing the locking pin 320 in the first position or the second position, and the operation is convenient.

[0048] In one embodiment, the locking pin 320 includes a locking segment 321, a connecting segment 322 and an unlocking segment 323 connected in sequence, wherein the distance between the locking segment 321 and the axis of the connecting ring 200 is greater than the distance between the unlocking segment 323 and the axis of the connecting ring 200. Specifically, when the locking pin 320 is in the first position, the locking segment 321 corresponds to the locking groove 310. Since the distance between the locking segment 321 and the axis of the connecting ring 200 is relatively close, the locking segment 321 will be stuck in the locking groove 310, thereby achieving the purpose of locking the connecting ring 200. When the locking pin 320 is in the second position, the unlocking segment 323 corresponds to the locking groove 310. Since the distance between the unlocking segment 323 and the axis of the connecting ring 200 is relatively far, the unlocking segment 323 will be located outside the locking groove 310, thereby achieving the purpose of unlocking the connecting ring 200.

[0049] The locking pin 320 of the locking assembly of the UAV countermeasure equipment quick erection connection device provided in this embodiment has a simple structure and a reasonable design, and there is no need for the locking pin 320 to perform reciprocating linear motion along the radial direction of the connecting ring 200, thereby making the structure of the UAV countermeasure equipment quick erection connection device more compact.

[0050] In one embodiment, two locking pins 320 are symmetrically provided, and the free ends of the unlocking sections 323 of the two locking pins 320 are fixedly connected by a connecting pin 330. By providing two locking pins 320, the purpose of enhancing the locking effect is achieved. Preferably, the two locking pins 320 and the connecting pin 330 are integrally formed.

[0051] In one embodiment, the locking assembly further includes a driving structure for driving the locking pin 320 to perform reciprocating linear motion between the first position and the second position.

[0052] Specifically, the driving structure includes a driving button 340 and a torsion spring 350 .

[0053] The first end of the driving button 340 is hinged to the connecting ring 200, and the second end can reciprocate linearly between the third position and the fourth position around its own hinge center line. The locking pin 320 is transmission-connected to the driving button 340. Specifically, a sliding hole 341 is provided on the side of the second end of the driving button 340 facing the axis of the connecting ring 200. The length direction of the sliding hole 341 extends along the length direction of the driving button 340, and the connecting pin 330 is movably inserted in the sliding hole 341. When the driving button 340 is in the third position, the locking pin 320 is in the first position, and when the driving button 340 is in the fourth position, the locking pin 320 is in the second position.

[0054] The torsion spring 350 is arranged at the hinge center of the driving button 340. Both ends of the torsion spring 350 are respectively hinged to the connecting ring 200 and the driving button 340. In a natural state, it has a tendency to move the driving button 340 from the fourth position to the third position.

[0055] When in use, in a natural state, under the action of the torsion spring 350, the torsion spring 350 keeps the driving button 340 in the third position, thereby keeping the locking pin 320 in the first position through the driving button 340. When it is necessary to release the lock of the connecting ring 200, the driving button 340 is pressed to drive the driving button 340 from the third position to the fourth position, thereby driving the locking pin 320 from the first position to the second position through the driving button 340, thereby achieving the purpose of releasing the lock of the connecting ring 200.

[0056] After the connecting ring 200 is moved to a suitable position, the driving button 340 is released, and under the elastic force of the torsion spring 350, the driving button 340 is driven from the fourth position to the third position, thereby driving the locking pin 320 to the first position through the driving button 340, thereby achieving the purpose of locking the connecting ring 200.

[0057] The driving structure of the locking component of the UAV countermeasure equipment quick erection connection device provided in this embodiment has a simple structure and a reasonable design. The connecting ring 200 can be unlocked by pressing the driving button 340, and the connecting ring 200 can be locked by stopping pressing the driving button 340. The operation is simple.

[0058] In one embodiment, a button seat 360 and a rotating shaft bolt 370 are also included.

[0059] The button seat 360 is fixedly connected to the connecting ring 200, specifically, the button seat 360 is fixedly connected to the connecting ring 200 via a connecting bolt 380. The first end of the driving button 340 is hinged to the button seat 360 via a rotating shaft bolt 370. The torsion spring 350 is sleeved on the rotating shaft bolt 370.

[0060] In this embodiment, the button seat 360 and the rotating shaft bolt 370 are provided to facilitate the assembly of the driving button 340 and the torsion spring 350 .

[0061] In one embodiment, a limiting bolt 390 is further included, and the limiting bolt 390 is arranged at the first end of the driving button 340. The limiting bolt 390 is used to limit the driving button 340, so that under the action of the elastic force of the torsion spring 350, when the torsion spring 350 moves the driving button 340 from the fourth position to the third position, when the driving button 340 moves to the third position, the limiting bolt 390 conflicts with the connecting ring 200 or the button seat 360, so that the driving button 340 cannot continue to rotate.

[0062] In one embodiment, the connecting column 100 is cylindrical, the locking groove 310 is annular, and the inner wall of the locking groove 310 is provided with a limiting wall 311 that matches the locking pin 320. When the locking pin 320 is located in the locking groove 310, the locking pin 320 conflicts with the limiting wall 311, thereby achieving the purpose of locking the rotation of the connecting ring 200.

[0063] In the specification of the present utility model, a lot of specific details are described. However, it is understood that the embodiments of the present utility model can be practiced without these specific details. In some examples, well-known methods, structures and techniques are not shown in detail so as not to obscure the understanding of this specification.

[0064] Finally, it should be noted that the above embodiments are only used to illustrate the technical solution of the utility model, rather than to limit it. Although the utility model has been described in detail with reference to the aforementioned embodiments, those skilled in the art should understand that they can still modify the technical solutions described in the aforementioned embodiments, or replace some or all of the technical features therein by equivalents. These modifications or replacements do not make the essence of the corresponding technical solutions deviate from the scope of the technical solutions of the embodiments of the utility model, and they should all be included in the scope of the claims and specification of the utility model.

Claims

1. A quick installation and connection device for drone countermeasure equipment, characterized in that: include: A connecting column (100), a first end of which is provided with a connecting portion (110) adapted to be connected to a tripod, and a second end of which is freely extending; A connecting ring (200) is coaxially sleeved on the connecting post (100) and movably connected to the connecting post (100); as well as A locking assembly is arranged on the connecting column (100) and / or the connecting ring (200) and is used to lock the connecting ring (200).

2. The UAV countermeasure equipment rapid erection connection device according to claim 1, characterized in that: The locking assembly comprises: A locking groove (310) is provided on the side wall of the connecting column (100), and a plurality of the locking grooves (310) are provided, and the plurality of the locking grooves (310) are sequentially spaced apart along the length direction of the connecting column (100); and A locking pin (320), one end of which is inserted into the connecting ring (200) and is slidably connected to the connecting ring (200), and can perform reciprocating linear motion between a first position and a second position, wherein when the locking pin (320) is in the first position, the locking pin (320) is clamped in the locking groove (310), and when the locking pin (320) is in the second position, the locking pin (320) is located outside the locking groove (310).

3. The UAV countermeasure equipment rapid erection connection device according to claim 2, characterized in that: The locking pin (320) comprises a locking section (321), a connecting section (322) and an unlocking section (323) which are connected in sequence, wherein the distance between the locking section (321) and the axis of the connecting ring (200) is greater than the distance between the unlocking section (323) and the axis of the connecting ring (200).

4. The UAV countermeasure equipment rapid erection connection device according to claim 3, characterized in that: Two locking pins (320) are symmetrically arranged, and the free ends of the unlocking sections (323) of the two locking pins (320) are fixedly connected via a connecting pin (330).

5. The UAV countermeasure equipment rapid erection connection device according to claim 4, characterized in that: The locking assembly further comprises a driving structure, wherein the driving structure is used to drive the locking pin (320) to perform reciprocating linear motion between the first position and the second position.

6. The UAV countermeasure equipment rapid erection connection device according to claim 5, characterized in that: The driving structure comprises: a driving button (340), the first end of which is hinged to the connecting ring (200), and the second end of which can perform reciprocating linear motion between a third position and a fourth position around its own hinge center line, the locking pin (320) being transmission-connected to the driving button (340), wherein when the driving button (340) is in the third position, the locking pin (320) is in the first position, and when the driving button (340) is in the fourth position, the locking pin (320) is in the second position; and A torsion spring (350) is arranged at the hinge center of the driving button (340), and its two ends are respectively hinged to the connecting ring (200) and the driving button (340), and in a natural state, it has a tendency to move the driving button (340) from the fourth position to the third position.

7. The UAV countermeasure equipment rapid erection connection device according to claim 6, characterized in that: Also includes: A button seat (360), wherein the button seat (360) is fixedly connected to the connecting ring (200); as well as A rotating shaft bolt (370), wherein the first end of the driving button (340) is hingedly connected to the button seat (360) via the rotating shaft bolt (370).

8. The UAV countermeasure equipment rapid erection connection device according to claim 6 or 7, characterized in that: A sliding hole (341) is provided on a side of the second end of the driving button (340) facing the axis of the connecting ring (200), the length direction of the sliding hole (341) extends along the length direction of the driving button (340), and the connecting pin (330) is movably inserted in the sliding hole (341).

9. The UAV countermeasure equipment rapid erection connection device according to claim 6 or 7, characterized in that: It also includes a limiting bolt (390), which is arranged on the first end of the driving button (340) and is used to limit the driving button (340).

10. The UAV countermeasure equipment rapid erection connection device according to any one of claims 3 to 7, characterized in that: The connecting column (100) is cylindrical, the locking groove (310) is annular, and the inner wall of the locking groove (310) is provided with a limiting wall (311) that matches the locking pin (320).

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