CN210374792U - Unmanned aerial vehicle interceptor - Google Patents
Unmanned aerial vehicle interceptor Download PDFInfo
- Publication number
- CN210374792U CN210374792U CN201921379746.2U CN201921379746U CN210374792U CN 210374792 U CN210374792 U CN 210374792U CN 201921379746 U CN201921379746 U CN 201921379746U CN 210374792 U CN210374792 U CN 210374792U
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- intercepting
- aerial vehicle
- unmanned aerial
- counterweight
- net
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Abstract
The utility model relates to an unmanned aerial vehicle interceptor discloses a net bullet structure through can withdrawing carries out the interception to unmanned aerial vehicle and catches, reduces the interceptor of the unmanned aerial vehicle escape condition. In the intercepting process, no redundant falling object exists, the closing can be carried out, and the escape possibility is reduced. The intercepting head is characterized in that a traction rope is arranged at one end of the intercepting head, an adjusting sleeve is arranged on the traction rope, the traction rope is formed by twisting four strands of hollow ropes, a lead is arranged in the middle of each hollow rope, the intercepting head is composed of a counterweight flap block, a groove, a wing plate, a connecting sleeve, a convex block, an electromagnetic coil, a fixing ring, an inner arc-shaped groove, a catching net and a connecting seat, the four counterweight flap blocks are combined to form an intercepting head main body, the inner arc-shaped grooves are arranged on the counterweight flap blocks, the inner arc-shaped grooves on the four counterweight flap blocks are combined to form a cylindrical cavity, the intercepting net is contained in the cylindrical cavity in a folding mode, four corners of the intercepting net are connected through the fixing net and the counterweight flap blocks respectively, grooves are formed.
Description
Technical Field
The utility model relates to an unmanned aerial vehicle interceptor relates to one kind and when carrying out the interception to low latitude unmanned aerial vehicle in the city, the unmanned aerial vehicle interceptor of use belongs to the anti-terrorism field of military. In particular to an interceptor which intercepts and captures an unmanned aerial vehicle through a net bomb structure capable of being retracted and reduces the escape condition of the unmanned aerial vehicle.
Background
At present, unmanned aerial vehicle's civilian occasion is more and more, and along with unmanned aerial vehicle's development, make aerial photography technique application in different image propagates, for example, large-scale match live broadcast, the meeting etc., also adopt unmanned aerial vehicle to reconnoiter or the task execution in the military affairs, the same, unmanned aerial vehicle's development has also brought the inconvenience for the aerial public security of society, because above-mentioned civilian unmanned aerial vehicle flight height is low, and is slow in speed, hardly discover through facilities such as radar, need intercept under some extreme occasions, current interception net can only intercept, can not further catch, there is the time difference to unmanned aerial vehicle's control, behind when unmanned aerial vehicle is intercepted, because the distance is indefinite, unexpected situation appears easily.
Publication No. CN105711850A discloses a net-bomb-type anti-unmanned aerial vehicle intelligent interception system, which has the problem that high-altitude falling objects are generated after the interception system is launched, and harm is easily caused to ground personnel.
Publication number CN206755998U discloses an interception system for small unmanned aerial vehicle, including carrying on the interception net that rises to the air through small rocket, this interception net pulls the removal through the unmanned aerial vehicle more than one after rising to the air, the interception net is including the dictyosome in the middle of and the outside frame of dictyosome, the top of frame is provided with a buoyancy mechanism, buoyancy mechanism top has the connecting piece of pulling, and the bottom of interception net is provided with counter weight mechanism, and unmanned aerial vehicle docks with the connecting piece that pulls in the air, and the device pulls the interception through a plurality of unmanned aerial vehicle and removes, lacks the action of catching it, and when being forced to enclose suddenly by the interception unmanned aerial vehicle, easy whole crash.
Publication number CN108088313A discloses an unmanned aerial vehicle interception system, which comprises an early warning system, a control system and an interception device, wherein the interception device comprises a launching bracket, an interception net and a plurality of rocket projectiles, wherein a rocket projectile is placed on a fixed seat, and the plurality of rocket projectiles are respectively connected to the edge of the interception net; the rocket launching bomb comprises a bomb body, a propeller, a fairing arranged at the upper end of the propeller, a parachute arranged in the fairing, a parachute launching device arranged in the fairing and a navigator arranged on the outer wall of the fairing; the early warning system is used for detecting and tracking the position information of the invading unmanned aerial vehicle and transmitting the information to the control system; the control system is used for controlling a propeller in the intercepting device to start and fly to an intercepting target according to the position information of the unmanned aerial vehicle sent by the early warning system and the position information fed back by the navigator in real time.
Disclosure of Invention
In order to improve the situation, the utility model relates to an unmanned aerial vehicle interceptor provides one kind and carries out the interception through the net bullet structure that can withdraw and catch unmanned aerial vehicle, reduces the interceptor of the unmanned aerial vehicle escape condition. In the intercepting process, no redundant falling object exists, the closing can be carried out, and the escape possibility is reduced.
The utility model relates to an unmanned aerial vehicle interceptor is realized like this: the utility model relates to an unmanned aerial vehicle interceptor, which comprises a blocking head, an adjusting sleeve and a traction rope, wherein one end of the blocking head is provided with the traction rope, the adjusting sleeve is sleeved on the traction rope, the traction rope is formed by twisting four strands of hollow ropes, the middle part of the hollow ropes is provided with a lead, the blocking head is composed of a counterweight flap block, a groove, a wing plate, a connecting sleeve, a convex block, an electromagnetic coil, a fixing ring, an inner arc-shaped groove, a catching net and a connecting seat, the four counterweight flap blocks are combined to form a blocking head main body, the counterweight flap block is provided with the inner arc-shaped groove, the inner arc-shaped grooves on the four counterweight flap blocks are combined to form a cylindrical cavity, the blocking net is folded and accommodated in the cylindrical cavity, four corners of the blocking net are respectively connected through the fixing net and the counterweight flap block, the groove is arranged on the convex block, the four counterweight flap blocks are correspondingly spliced through the groove, the connecting seat is provided with a connecting sleeve, the connecting sleeves are respectively connected with the hollow rope correspondingly, the electromagnetic coils are arranged on the counterweight clack block and are correspondingly connected with the hollow rope through leads in the connecting sleeves, the electromagnetic coils are distributed relatively, and the outer side wall of the counterweight clack block is provided with a wing plate.
Has the beneficial effects.
Firstly, the low-altitude unmanned aerial vehicle can be intercepted and captured.
Secondly, simple structure, can used repeatedly.
And in the intercepting process, no redundant falling object exists, the closing can be carried out, and the escape possibility is reduced.
Drawings
Figure 1 the utility model relates to a three-dimensional structure chart of unmanned aerial vehicle interceptor.
Figure 2 the utility model relates to a three-dimensional structure chart of unmanned aerial vehicle interceptor counter weight lamella piece.
Fig. 3 the utility model relates to a structural schematic diagram of unmanned aerial vehicle interceptor.
Figure 4 the utility model relates to a three-dimensional structure chart when unmanned aerial vehicle interceptor uses.
In the attached drawings
Wherein the parts are: the adjustable type hydraulic pressure balance weight device comprises a blocking frustum 1, an adjusting sleeve 2, a traction rope 3, a balance weight petal block 4, a groove 5, a wing plate 6, a connecting sleeve 7, a convex block 8, an electromagnetic coil 9, a fixing ring 10, an inner arc-shaped groove 11, a catching net 12 and a connecting seat 13.
The specific implementation mode is as follows:
the utility model relates to an unmanned aerial vehicle interceptor, including blocking 1, adjusting sleeve 2 and traction rope 3, blocking 1 one end is provided with traction rope 3, adjusting sleeve 2 is nested on traction rope 3, traction rope 3 is twisted together by four strands of hollow rope, the middle part of hollow rope is provided with a lead, blocking 1 is composed of counterweight flap block 4, groove 5, wing plate 6, adapter sleeve 7, lug 8, solenoid 9, fixing ring 10, inner arc-shaped groove 11, catching net 12 and connecting seat 13, four counterweight flap blocks 4 are combined to form blocking 1 main body, counterweight flap block 4 is provided with inner arc-shaped groove 11, inner arc-shaped grooves 11 on four counterweight flap blocks 4 are combined to form a cylindrical cavity, the blocking net is accommodated in the cylindrical cavity in a folding manner, four corners of blocking net are connected with counterweight flap block 4 through the fixing net respectively, and counterweight flap block 4 is provided with groove 5, on counter weight lamella piece 4, four was arranged in to lug 8 correspond the amalgamation through recess 5 and lug 8 between the counter weight lamella piece 4, on counter weight lamella piece 4 was arranged in to connecting seat 13, connecting seat 13 overhead has adapter sleeve 7, and adapter sleeve 7 corresponds respectively and is connected with the cavity rope, and on solenoid 9 arranged counter weight lamella piece 4, and correspond the connection through the wire in adapter sleeve 7 and the cavity rope, relative distribution between a plurality of solenoid 9 has put pterygoid lamina 6 on the 4 lateral walls of counter weight lamella piece.
When the unmanned aerial vehicle is used, the plurality of counterweight petals 4 are combined to form the interception frustum 1 in the initial state, the traction rope 3 is coiled on the traction wire coil, the lead in the traction rope 3 is electrified but not electrified, when the traction rope is electrified, the magnetic field directions among the plurality of electromagnetic coils 9 are opposite to form repulsion, when interception is needed, the interception frustum 1 is placed in an ejection gun, the interception frustum 1 is ejected to the unmanned aerial vehicle to be intercepted through the ejection gun, when the unmanned aerial vehicle is close to, the guidance is electrified, the electromagnetic coils 9 are electrified to generate magnetism, the electromagnetic coils 9 are opposite to generate the same magnetic poles and repel the plurality of counterweight petals 4, the counterweight petals 4 are respectively ejected to the periphery, the counterweight petals 4 are expanded to spread the interception net, the unmanned aerial vehicle is intercepted and wrapped to form interception capture, then three of the guidance is powered off, one electromagnetic coil 9 is electrified to attract the plurality of counterweight petals 4, the interception net is sealed, and simultaneously, retrieve traction rope 3, catch the recovery to unmanned aerial vehicle, it is great as the unmanned aerial vehicle that needs were caught, and the interception net spreads out the area grow, through adjusting the distance of adjusting sleeve 2 on traction rope 3, changes the distance that counter weight lamella 4 expands outward, reaches the purpose of carrying out the interception to unmanned aerial vehicle.
The above embodiments are the preferred embodiments of the present invention, and are not intended to limit the scope of the present invention. Any person skilled in the art can make some modifications without departing from the scope of the invention, i.e. all equivalent modifications made according to the invention are intended to be covered by the scope of the invention. It should also be noted that, unless otherwise specifically stated or limited, the terms "disposed on," "mounted on," "connected to" and "connected to" are to be construed broadly and may include, for example, a fixed connection such as a crimped connection, a riveted connection, a pinned connection, an adhesive connection, a welded connection, a removable connection such as a threaded connection, a snap connection, a hinged connection, an integral connection, an electrical connection, a direct connection, an indirect connection through an intermediate medium, and a communication between two elements. The specific meaning of the above terms in the present invention can be understood in specific cases to those skilled in the art.
Claims (3)
1. The utility model provides an unmanned aerial vehicle interceptor, characterized by: the intercepting device comprises an intercepting head, an adjusting sleeve and a traction rope, wherein the traction rope is arranged at one end of an intercepting head, the adjusting sleeve is arranged on the traction rope, the traction rope is formed by twisting four strands of hollow ropes, a lead is arranged in the middle of each hollow rope, the intercepting head consists of a counterweight flap block, a groove, a wing plate, a connecting sleeve, a convex block, an electromagnetic coil, a fixing ring, an inner arc-shaped groove, a catching net and a connecting seat, the four counterweight flap blocks are combined to form an intercepting head main body, the inner arc-shaped groove is arranged on each counterweight flap block, the inner arc-shaped grooves on the four counterweight flap blocks are combined to form a cylindrical cavity, the intercepting net is folded and accommodated in the cylindrical cavity, four corners of the intercepting net are respectively connected with the counterweight flap blocks through the fixing net, the connecting seat is arranged on each counterweight flap block, the connecting seat is provided with the connecting sleeve, the connecting sleeves are respectively correspondingly connected with, the plurality of electromagnetic coils are distributed relatively.
2. The unmanned aerial vehicle interceptor of claim 1, wherein the counterweight petal is provided with a groove, the projection is disposed on the counterweight petal, and the four counterweight petals are correspondingly spliced by the groove and the projection.
3. An unmanned aerial vehicle interceptor of claim 1 or 2 wherein a wing panel is disposed on the outer sidewall of the counterweight flap.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921379746.2U CN210374792U (en) | 2019-08-23 | 2019-08-23 | Unmanned aerial vehicle interceptor |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921379746.2U CN210374792U (en) | 2019-08-23 | 2019-08-23 | Unmanned aerial vehicle interceptor |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN210374792U true CN210374792U (en) | 2020-04-21 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201921379746.2U Expired - Fee Related CN210374792U (en) | 2019-08-23 | 2019-08-23 | Unmanned aerial vehicle interceptor |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN210374792U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN116379841A (en) * | 2023-03-20 | 2023-07-04 | 中国人民武装警察部队指挥学院 | Capturing type anti-unmanned aerial vehicle interception system and application method thereof |
-
2019
- 2019-08-23 CN CN201921379746.2U patent/CN210374792U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN116379841A (en) * | 2023-03-20 | 2023-07-04 | 中国人民武装警察部队指挥学院 | Capturing type anti-unmanned aerial vehicle interception system and application method thereof |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20200421 Termination date: 20200823 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |