CN210400185U - Launching gun barrel for intercepting net bombs of unmanned aerial vehicle - Google Patents
Launching gun barrel for intercepting net bombs of unmanned aerial vehicle Download PDFInfo
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- CN210400185U CN210400185U CN201921461630.3U CN201921461630U CN210400185U CN 210400185 U CN210400185 U CN 210400185U CN 201921461630 U CN201921461630 U CN 201921461630U CN 210400185 U CN210400185 U CN 210400185U
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Abstract
The utility model discloses a launching barrel of an unmanned aerial vehicle interception net bomb, which comprises a launching barrel, wherein the interception net bomb is arranged in the launching barrel; the driving device drives the intercepting net to eject out of the launching tube and then rotate; the intercepting net bomb comprises an intercepting net, and the edge of the expanded intercepting net is provided with a heavy object block. The utility model discloses can drive the rotatory ejection of interception net bullet, improve the stability of interception net bullet in the motion process, and then promote interception unmanned aerial vehicle's success rate.
Description
Technical Field
The utility model relates to a defense technology field especially relates to an unmanned aerial vehicle intercepts transmission barrel of net bullet.
Background
In recent years, with the emergence of unmanned aerial vehicle companies in the market like bamboo shoots in spring after raining, unmanned aerial vehicles begin to fly into common families and develop into various fields of society, but the problem of black flight of unmanned aerial vehicles also arises, and at present, half of unmanned aerial vehicles in the whole country are in the state of unlicensed black flight. And unmanned aerial vehicle is because its with low costs, and the acquisition channel is extensive, is utilized by illegal very easily, and unmanned aerial vehicle's flying height is low in addition, surveys the plane of reflection for a short time, has caused very big hidden danger for national aerial safety, also endangers civil aviation safety simultaneously.
The flexible rope net interception is an effective means for intercepting the unmanned aerial vehicle at present, and the interception mode of the flexible rope net mainly comprises two modes of net bomb launching interception and manual control unmanned aerial vehicle net throwing interception. When the net bomb is used for launching and intercepting the unmanned aerial vehicle, the motion track of the net bomb after being launched is not easy to control, and the success rate of intercepting the unmanned aerial vehicle is further influenced.
Disclosure of Invention
The purpose of the invention is as follows: in order to overcome the not enough of existence among the prior art, the utility model provides an unmanned aerial vehicle interception net bullet's transmission barrel can drive the rotatory ejection of interception net bullet, improves the stability of interception net bullet in the motion process, and then promotes interception unmanned aerial vehicle's success rate.
The technical scheme is as follows: in order to achieve the purpose, the utility model discloses a launching barrel of the intercepting net bomb of the unmanned aerial vehicle, which comprises a launching barrel, wherein the intercepting net bomb is arranged in the launching barrel; the driving device drives the intercepting net to eject out of the launching tube and then rotate; the intercepting net bomb comprises an intercepting net, and the edge of the expanded intercepting net is provided with a heavy object block.
Furthermore, an elastic compression piece is arranged in the launching tube and used for ejecting the intercepting net.
Furthermore, the intercepting net bullet and the launching tube are circumferentially limited, and the driving device drives the launching tube to rotate and drives the intercepting net bullet to rotate.
Furthermore, a transmission device is arranged in the launching tube, one end of the transmission device is connected with the driving device, and the other end of the transmission device is connected with the intercepting net bullet, so that the intercepting net bullet rotates in the launching tube.
Furthermore, the heavy object blocks are columnar bodies with sector-shaped cross sections, the heavy object blocks at the edges are spliced into a ring shape when the intercepting net is folded, and the intercepting net is positioned in the ring shape.
Furthermore, the intercepting net is circular or regular polygon, and the heavy weight blocks are uniformly arranged on the edge of the intercepting net.
Has the advantages that: the utility model discloses a launching barrel of an unmanned aerial vehicle interception net bullet, a driving device drives the interception net bullet to rotate and expand after being ejected, thereby improving the stability of the interception net bullet in the motion process; the intercepting net is circular or regular polygon, and the edge of the intercepting net after being unfolded is uniformly provided with the heavy object blocks, so that the mass distribution of the intercepting net is uniform, and the stability is better.
Drawings
FIG. 1 is a schematic view of a launching barrel;
fig. 2 is a schematic view of an intercepting net.
Detailed Description
The present invention will be further described with reference to the accompanying drawings.
The launching barrel for intercepting net bombs of the unmanned aerial vehicle as shown in the attached drawings 1-2 comprises a launching barrel 1, wherein intercepting net bombs 3 are arranged in the launching barrel 1, and the intercepting net bombs 3 are launched through the launching barrel 1; the device also comprises a driving device 2, wherein the driving device 2 drives the interception net bullet 3 to eject out of the launching tube 1 and then rotate, and the two modes are divided into two modes, namely that the driving device 2 drives the launching tube 1 and the interception net bullet to rotate together, and the transmission device 7 drives the interception net bullet 3 to rotate; interception net bullet 3 includes interception net 5, works as interception net bullet 3 is close to behind the unmanned aerial vehicle interception net bullet 3 launches interception net 5, the edge after interception net 5 expandes is equipped with heavy object piece 6, can help rotatoryly interception net 5 expandes fast under the centrifugal action, rotatory flight interception net 5 is also more stable relatively.
An elastic compression piece 4 is arranged in the launching tube 1, and the intercepting net bomb 3 is ejected out by the elastic compression piece 4.
The heavy object blocks 6 are columnar bodies with sector-shaped cross sections, the heavy object blocks 6 at the edges are spliced into a ring shape when the intercepting net 5 is folded, so that the folded shape is good in overall stability and not easy to disperse, and the intercepting net 5 is located in the ring shape.
The intercepting net 5 is circular or regular polygon, and a plurality of the heavy object blocks 6 are uniformly arranged on the edge of the intercepting net 5, so that the mass of the intercepting net 5 and the mass of the heavy object blocks 6 are uniformly distributed, and the intercepting net 5 is more stable during rotating flight in the air.
The intercepting net bullets 3 are circumferentially limited with the launching tube 1, the driving device 2 drives the launching tube 1 to rotate and drives the intercepting net bullets 3 to rotate, so that the intercepting net bullets 3 rotate after being ejected.
The launching tube 1 is internally provided with a transmission device 7, one end of the transmission device 7 is connected with the driving device 2, and the other end of the transmission device 7 is connected with the intercepting net bullet 3, so that the intercepting net bullet 3 rotates in the launching tube 1, and the intercepting net bullet 3 rotates after being ejected.
The utility model mainly utilizes the principle that the rotating shaft of an object always points to a fixed direction in the high-speed rotation process, and adds the driving device 2 in the existing net bomb launching cavity, so that the interception net bomb 3 has a rotating initial speed after launching, thereby improving the stability of the interception net bomb 3 in the flying process; meanwhile, the heavy object blocks 6 are uniformly distributed on the edge of the interception net 5 in the interception net bomb 3, so that the interception net 5 can be rapidly unfolded and moves more stably.
The above description is only a preferred embodiment of the present invention, and it should be noted that: for those skilled in the art, without departing from the principle of the present invention, several improvements and modifications can be made, and these improvements and modifications should also be considered as the protection scope of the present invention.
Claims (6)
1. The utility model provides an unmanned aerial vehicle intercepts transmission barrel of net bullet which characterized in that: the device comprises a launching tube (1), wherein an intercepting net bomb (3) is arranged in the launching tube (1); the device further comprises a driving device (2), and the driving device (2) drives the interception net bomb (3) to be ejected out of the launching tube (1) and then to rotate; the intercepting net bomb (3) comprises an intercepting net (5), and a heavy object block (6) is arranged at the edge of the expanded intercepting net (5).
2. The launch barrel of an unmanned aerial vehicle interception net bomb according to claim 1, characterized in that: an elastic compression piece (4) is arranged in the launching tube (1), and the intercepting net bomb (3) is ejected out by the elastic compression piece (4).
3. The launch barrel of an unmanned aerial vehicle interception net bomb according to claim 1, characterized in that: the intercepting net bomb (3) and the launching tube (1) are circumferentially limited, and the driving device (2) drives the launching tube (1) to rotate and drives the intercepting net bomb (3) to rotate.
4. The launch barrel of an unmanned aerial vehicle interception net bomb according to claim 1, characterized in that: a transmission device (7) is arranged in the launching tube (1), one end of the transmission device (7) is connected with the driving device (2), the other end of the transmission device (7) is connected with the intercepting net bullet (3), and the intercepting net bullet (3) is enabled to rotate in the launching tube (1).
5. The launch barrel of an unmanned aerial vehicle interception net bomb according to claim 1, characterized in that: the heavy object blocks (6) are columnar bodies with sector-shaped cross sections, the heavy object blocks (6) on the edges are spliced into a ring shape when the intercepting net (5) is folded, and the intercepting net (5) is located in the ring shape.
6. The launch barrel of an unmanned aerial vehicle interception net bomb according to claim 5, characterized in that: the intercepting net (5) is circular or regular polygon, and the plurality of heavy object blocks (6) are uniformly arranged on the edge of the intercepting net (5).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921461630.3U CN210400185U (en) | 2019-09-04 | 2019-09-04 | Launching gun barrel for intercepting net bombs of unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921461630.3U CN210400185U (en) | 2019-09-04 | 2019-09-04 | Launching gun barrel for intercepting net bombs of unmanned aerial vehicle |
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| CN210400185U true CN210400185U (en) | 2020-04-24 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201921461630.3U Active CN210400185U (en) | 2019-09-04 | 2019-09-04 | Launching gun barrel for intercepting net bombs of unmanned aerial vehicle |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110455126A (en) * | 2019-09-04 | 2019-11-15 | 中交遥感天域科技江苏有限公司 | A kind of launching gun barrel and its working method of unmanned plane intercept net bullet |
-
2019
- 2019-09-04 CN CN201921461630.3U patent/CN210400185U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110455126A (en) * | 2019-09-04 | 2019-11-15 | 中交遥感天域科技江苏有限公司 | A kind of launching gun barrel and its working method of unmanned plane intercept net bullet |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| PE01 | Entry into force of the registration of the contract for pledge of patent right |
Denomination of utility model: A gun barrel for UAV intercepting net bomb Effective date of registration: 20210122 Granted publication date: 20200424 Pledgee: Wuxi Branch of Bank of Beijing Co.,Ltd. Pledgor: CHINA COMMUNICATIONS REMOTE SENSING TIANYU TECHNOLOGY JIANGSU Co.,Ltd. Registration number: Y2021320010028 |
|
| PE01 | Entry into force of the registration of the contract for pledge of patent right | ||
| PC01 | Cancellation of the registration of the contract for pledge of patent right |
Granted publication date: 20200424 Pledgee: Wuxi Branch of Bank of Beijing Co.,Ltd. Pledgor: CHINA COMMUNICATIONS REMOTE SENSING TIANYU TECHNOLOGY JIANGSU Co.,Ltd. Registration number: Y2021320010028 |
|
| PC01 | Cancellation of the registration of the contract for pledge of patent right |