CN206847481U - A kind of accurate emission system for catching unmanned plane - Google Patents
A kind of accurate emission system for catching unmanned plane Download PDFInfo
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- CN206847481U CN206847481U CN201720066964.5U CN201720066964U CN206847481U CN 206847481 U CN206847481 U CN 206847481U CN 201720066964 U CN201720066964 U CN 201720066964U CN 206847481 U CN206847481 U CN 206847481U
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- unmanned plane
- net
- emission system
- netting gear
- rocket
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Abstract
The utility model provides a kind of accurate emission system for catching unmanned plane, the accurate emission system includes base, the netting gear device being arranged on base, annular array type are distributed in the Zhuai Wang mechanisms around netting gear device, and the information detection module being connected with Zhuai Wang mechanisms.The utility model solves prior art during machine is blocked because the net launch angle of dragging for rocket of throwing the net can not be adjusted, thrown the net contradiction between opportunity and acquisition speed so that being difficult to coordination, so as to reduce to moving the capture rate of unmanned plane target and the technical problem of precision.Have the characteristics that intercept speed is fast, hit accuracy rate is high, and angle of throwing the net can be changed according to unmanned plane range information, obtain optimal throw the net speed and flying speed, improve interception and capture rate.
Description
Technical field
The utility model belongs to civilian anti-unmanned plane field, relates more specifically to a kind of accurate transmitting system for catching unmanned plane
System.
Background technology
Background of related of the present utility model is illustrated below, but these explanations might not form this practicality newly
The prior art of type.
With the development of science and technology, civilian unmanned plane starts to miniaturization, simplified, cost degradation development, and rapidly
Applied in commercial market, come into huge numbers of families as emerging rapidly in large numbersBamboo shoots after a spring rain.At present, in afield, in park, street is small
Between lane, the application of rotary wind type unmanned plane is all seen everywhere.But with being surging forward for unmanned plane market, unmanned plane " black to fly " event
Also constantly exposure, not only jeopardizes life and property safety of people, also disturbs public order, or even upsets the event of airplane flight
Also happen occasionally.Therefore, it is necessary to carry out orderly management to civilian unmanned plane, and take effective means catch it is harmful, dangerous can
Doubt unmanned plane.
To administer " black to fly ", people are proposed many technology preventions.Most simple and easy method, it is with transmitting one
Big net, big net are made up of tough and tensile material, can snarl unmanned plane, and unmanned plane can not be flown, finally captures unmanned plane.Country
Department of Intellectual Property disclosed a kind of anti-UAV Intelligent intercepting system of net bullet formula on June 29th, 2016, applied for that artificial Shanghai instrument is resistance to
New material Science and Technology Ltd., the utility model by detection early warning system to come attack invasion unmanned plane carry out early warning, by ground
Or aerial control emission system receives radar signal and sends interception instruction, and target is grabbed by launching intelligent intercept net bullet
Catch, the netting gear that intelligent intercept net bullet is formed by discharging transmitting by high-strength high-modulus polyethylene and the braiding of intelligent conductive fiber, in electricity
Unmanned plane is arrested in the lower interception of directed traction effect that magnetic induction is formed, and by netting palpus winding unmanned plane propeller, loses it
Power, speed slow down, and are wound and arrest.Although the utility model mentioned in the file of announcement with early warning range it is wide, block
Cut that speed is fast, have a wide range of application, hit the features such as high accuracy rate, intelligent and high-efficiency, enemy's unmanned plane can be carried out effectively complete
Orientation, multi-angle interference, intercept, arrest, and according to the model size of unmanned plane in pre-warning signal transmitting can be selected corresponding
The net bullet of netting gear, so that the characteristics of interception result is more preferable, but the transmitting intercept net bullet of throwing the net mentioned in the utility model, it is root
Distance, the velocity information measured during according to transmitting by prior-warning device is prefixed the time of throwing the net, and this kind of mode presence, which can not adjust, throws the net
Rocket drag net launch angle so that be difficult to coordination throw the net contradiction between opportunity and acquisition speed the problem of, so as to reduce to fortune
The capture rate and precision of dynamic unmanned plane target.
The content of the invention
To solve prior art during machine is blocked because the net launch angle of dragging for rocket of throwing the net can not be adjusted, so that
It is difficult to coordination to throw the net contradiction between opportunity and acquisition speed, so as to reduce capture rate and precision to moving unmanned plane target
Technical problem, the utility model provide it is a kind of catch unmanned plane accurate emission system.
According in a preferred embodiment of the present utility model, a kind of unmanned plane that catches provided by the utility model
Accurate emission system includes base, and the netting gear device being arranged on base, annular array type is distributed in dragging around netting gear device
Net mechanism, and the information detection module being connected with Zhuai Wang mechanisms；Netting gear device, for placing and launching netting gear；Zhuai Wang mechanisms
For providing target range information according to information detection module, adjust automatically well optimal launch angle, when Zhuai Wang mechanisms are sent
Drive the netting gear in netting gear device to open, make netting gear diameter equal with the time required to flying distance the time required to opening completely, it is real
Now to the accurate and quick seizure of UAV targets；Information detection module be used for by the distance of the UAV targets of acquisition, position,
The information such as speed draw the optimal launch angle of adjustment Zhuai Wang mechanisms with being calculated.
Preferably, above-mentioned netting gear device is by net cylinder, the dictyosome composition being arranged inside net cylinder.
Preferably, above-mentioned Zhuai Wang mechanisms are by launching tube, and rocket and the controller composition being arranged in launching tube；Drag net
Mechanism lights uniform rocket, extracts dictyosome, fly to unmanned plane by adjusting the optimal launch angle of rocket.
Preferably, above- mentioned information detecting module is made up of optical sight and millimeter wave frequency modulated(FM) radar.
Preferably, the optical axis of above-mentioned optical sight and millimetre-wave radar antenna beam central coaxial.
Preferably, the scope of above-mentioned rocket launching angle is 0-90 °.
Preferably, the above-mentioned launching tube containing rocket is provided with multiple, and is uniformly distributed in around net cylinder, to realize angle
Adjustable, synchronized transmissions.
Preferably, above-mentioned dictyosome is worked out using nylon yarn or high-strength high-modulus polyethylene fiber or carbon fibre material.
Preferably, be provided with above-mentioned dictyosome net must, net must by thread nylon yarn or high-strength high-modulus polyethylene fiber or
Carbon fibre material is worked out.
Preferably, the rocket in above-mentioned launching tube is 4 or more than 4.
The specific advantages below of the utility model：
1st, the utility model obtains unmanned plane distance by the millimeter wave frequency modulated(FM) radar in information acquisition module and speed is believed
Breath, distance and velocity information further according to the unmanned plane got adjust angle of throwing the net, so that emitter of throwing the net obtains most
Good throw the net speed and flying speed, so as to improve the interception of emitter and capture rate.
2nd, the utility model is again by equipped with optical sight, making its optical axis and millimetre-wave radar antenna beam center same
Axle, user's run-home can be helped in horizon range, make the antenna run-home unmanned plane of millimeter wave frequency modulated(FM) radar, realized
Precisely catch.
3rd, the utility model after 6 uniform rockets are lighted, is passed through by dragging net institutional adjustment well optimal launch angle
The rocket of transmitting extracts dictyosome, and 6 rockets form optimal speed of throwing the net and fly to unmanned plane simultaneously with flight optimization speed, with
Dictyosome just opens completely when unmanned plane meets, and takes full advantage of the flying speed of rocket, greatly improves the efficiency of capture, both
Suitable for static target, it is applied to moving target again.
4th, the dictyosome in the utility model is worked out using nylon yarn, is in regular hexagon after opening completely, is set on dictyosome
Net palpus is put, unmanned plane propeller can be wound, unmanned plane is run out of steam, speed slows down, and has and efficiently winding target can be achieved
The advantages of unmanned plane.
Brief description of the drawings
By that will become and the specific embodiment part provided, feature and advantage of the present utility model referring to the drawings
It is easier to understand, in the accompanying drawings：
Fig. 1 is the stereogram of emitter of being thrown the net in the utility model；
Fig. 2 is the structural representation of emitter of being thrown the net in the utility model；
Fig. 3 is the top view of emitter of being thrown the net in the utility model；
Fig. 4 is deployed condition schematic diagram of being thrown the net in the utility model.
Description of reference numerals：
Base 1；Netting gear device 2, net cylinder 201, dictyosome 202, net palpus 212；Zhuai Wang mechanisms 3, launching tube 301, rocket 302,
Controller 303；Information detection module 4.
Embodiment
Illustrative embodiments of the present utility model are described in detail with reference to the accompanying drawings.To illustrative embodiments
Description merely for the sake of demonstration purpose, and be definitely not to the utility model and its application or the limitation of usage.
Referring to shown in Fig. 1-Fig. 4, the accurate emission system provided by the utility model for catching unmanned plane includes base 1, if
The netting gear device 2 being placed on base 1, annular array type are distributed in the Zhuai Wang mechanisms 3 around netting gear device 2, and with dragging net machine
The information detection module 4 that structure 3 connects；Unmanned plane distance and speed are obtained by the millimeter wave frequency modulated(FM) radar in information detection module 4
Information is spent, the distance and velocity information further according to the unmanned plane got adjust angle of throwing the net, and obtain netting gear device 2 optimal
Speed of throwing the net and flying speed, just open, then pass through completely when the dictyosome in netting gear device 2 is meeting with UAV targets
Net palpus 212 on dictyosome 202 and dictyosome 202 winds unmanned plane propellers, it is run out of steam, speed slows down, and realizes to nobody
The winding of machine is arrested.Interception and the capture rate of emitter are improved simultaneously.Concrete structure and operation principle are as follows：
Target information is provided according to information acquisition module 4, information acquisition module 4 by the distance of unmanned plane in horizon range and
Velocity information, optimization calculating is carried out, draw the launch angle (scope of launch angle is 0-90 °) of adjustment rocket 302, so as to
Obtain optimal throw the net speed and flying speed；Information detection module 4 is mainly by optical sight 401 and millimeter wave frequency modulated(FM) radar
402 compositions, especially by optical sight 401 and millimeter wave frequency modulated(FM) radar 402 by the distance of the UAV targets of acquisition, position
Put, the information such as speed with being calculated, to obtain precision data, the optical axis of optical sight with millimetre-wave radar antenna beam
The heart is coaxial.After the good 302 optimal launch angle of rocket of system adjust automatically, drive dictyosome 202 to open when rocket 302 is sent, make
The diameter of dictyosome 202 open completely the time required to flying distance required time it is equal, realize to UAV targets it is accurate with it is fast
Speed is caught.
The netting gear device 2 mentioned in above-mentioned, the device is specifically by net cylinder 201, the dictyosome 202 being arranged inside net cylinder 201
Composition, for placing and launching netting gear, wherein dictyosome 202 uses high-strength high-modulus polyethylene fiber or carbon fibre material or nylon yarn
Work out, preferred nylon establishment, is specifically worked out by foldable nylon yarn, be placed in net cylinder in order in the technical program
In 201；It is in regular hexagon after dictyosome 202 opens completely, net palpus 212 is set on dictyosome 202, unmanned plane spiral can be wound
Oar, unmanned plane is set to run out of steam, speed slows down, so as to realize the purpose of efficiently winding UAV targets.Zhuai Wang mechanisms 3 are by sending out
Shooting cylinder 301, and the rocket 302 and controller 303 that are arranged in launching tube 301 form, and the rocket 302 in the application is more
It is individual, preferably 6, exemplified by 6 rockets are set, 6 launching tubes 301 containing rocket 302 are adjusted by controller 303 and most preferably sent out
Firing angle degree.When lighting 6 uniform rockets 302, dictyosome 202 is extracted by operation by this 6 rockets 302, flies to unmanned plane.
The method that 302 optimal launch angle of rocket adjusts in the utility model is as follows：First by information acquisition module 4
Optical sight and millimeter wave frequency modulated(FM) radar detect emission system and the distance of UAV targets, and system is according to UAV targets
Speed, coordinate position and apart from the accurate regulation optimal launch angle of rocket：When apart from it is remote when, launch angle diminishes；Distance is near
When, launch angle becomes big.Its setting principle is：The diameter of dictyosome 202 opens required time and flying distance required time phase completely
Deng.If distance is R, a diameter of d of dictyosome, optimal emission angle theta may be configured as：θ=arctg (d/2R).Light 6 launching tubes 301
Interior mouse 302, mouse 302 are flown with 80~330m/s speed towards 6 uniform different preceding line directions, extract dictyosome
202, target unmanned plane, and complete process of throwing the net；Diameter is about that 6m (can be selected and set according to demand after dictyosome 202 opens
Meter), then maximum miss distance 3m；Detector rf frequency 35GHz, triangular modulation signal, frequency deviation 500MHz, modulation period
10us。
Although the utility model is described with reference to illustrative embodiments, but it is to be understood that the utility model
The embodiment be described in detail and shown in text is not limited to, in the feelings without departing from claims limited range
Under condition, those skilled in the art can make various improvement or modification to the illustrative embodiments.
Claims (10)
- A kind of 1. accurate emission system for catching unmanned plane, it is characterised in that：The precisely emission system includes base (1), if The netting gear device (2) being placed on base (1), annular array type are distributed in the Zhuai Wang mechanisms (3) around netting gear device (2), and The information detection module (4) being connected with Zhuai Wang mechanisms (3)；The netting gear device (2), for placing and launching netting gear；It is described to drag Net mechanism (3), for providing target range information according to information detection module (4), adjust automatically well optimal launch angle, dragging Drive the netting gear in netting gear device (2) to open when net mechanism (3) is sent, make netting gear diameter open completely the time required to flight away from It is equal from required time, realize the accurate and quick seizure to UAV targets；Described information detecting module (4), for that will obtain The information such as the distance of the UAV targets taken, position, speed draw the optimal transmitting of adjustment Zhuai Wang mechanisms (3) with being calculated Angle.
- 2. the accurate emission system according to claim 1 for catching unmanned plane, it is characterised in that：The netting gear device (2) By net cylinder (201), internal dictyosome (202) composition of net cylinder (201) is arranged at.
- 3. the accurate emission system according to claim 2 for catching unmanned plane, it is characterised in that：The Zhuai Wang mechanisms (3) By launching tube (301), and rocket (302) and controller (303) composition being arranged in launching tube (301)；It is described to drag net machine Structure (3) lights uniform rocket (302), extracts dictyosome (202), fly to nobody by adjusting rocket (302) optimal launch angle Machine.
- 4. the accurate emission system according to claim 3 for catching unmanned plane, it is characterised in that：Described information detecting module (4) it is made up of optical sight (401) and millimeter wave frequency modulated(FM) radar (402).
- 5. the accurate emission system according to claim 4 for catching unmanned plane, it is characterised in that：The optical sight (401) optical axis and millimetre-wave radar (402) antenna beam central coaxial.
- 6. the accurate emission system according to claim 5 for catching unmanned plane, it is characterised in that：Rocket (302) hair The scope of firing angle degree is 0-90 °.
- 7. the accurate emission system according to claim 6 for catching unmanned plane, it is characterised in that：It is described to include rocket (302) launching tube (301) including is provided with multiple, and is uniformly distributed in net cylinder（201）Around, with realize adjustable angle, Synchronized transmissions.
- 8. the accurate emission system of the seizure unmanned plane according to claim 2 or 7, it is characterised in that：The dictyosome (202) Worked out using nylon yarn or high-strength high-modulus polyethylene fiber or carbon fibre material.
- 9. the accurate emission system according to claim 8 for catching unmanned plane, it is characterised in that：On the dictyosome (202) Set net must (212), the net must by thread nylon yarn or high-strength high-modulus polyethylene fiber or carbon fibre material establishment and Into.
- 10. the accurate emission system according to claim 9 for catching unmanned plane, it is characterised in that：The launching tube (301) Quantity containing rocket (302) is 4 or more than 4.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720066964.5U CN206847481U (en) | 2017-01-18 | 2017-01-18 | A kind of accurate emission system for catching unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720066964.5U CN206847481U (en) | 2017-01-18 | 2017-01-18 | A kind of accurate emission system for catching unmanned plane |
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| Publication Number | Publication Date |
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| CN206847481U true CN206847481U (en) | 2018-01-05 |
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ID=60790466
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| CN201720066964.5U Active CN206847481U (en) | 2017-01-18 | 2017-01-18 | A kind of accurate emission system for catching unmanned plane |
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Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108534603A (en) * | 2018-04-16 | 2018-09-14 | 无锡北方湖光光电有限公司 | Laser ranging night sight, anti-unmanned plane catch rifle and its application method with net |
| CN110849219A (en) * | 2019-12-03 | 2020-02-28 | 日照金慧科技信息咨询有限公司 | Improve unmanned aerial vehicle trapper of catching effect |
| RU2745590C1 (en) * | 2020-04-03 | 2021-03-29 | Федеральное государственное унитарное предприятие "Российский федеральный ядерный центр - Всероссийский научно-исследовательский институт технической физики имени академика Е.И. Забабахина" | Method for capture of air target with a net |
| CN112829908A (en) * | 2019-11-25 | 2021-05-25 | 福永干夫 | Torpedo defense system |
| CN113587730A (en) * | 2021-08-30 | 2021-11-02 | 航宇救生装备有限公司 | Umbrella net storage bag for unmanned aerial vehicle net capture |
| CN114153223A (en) * | 2021-09-22 | 2022-03-08 | 航天科工微电子系统研究院有限公司 | Net type capturing system and method for clustered unmanned aerial vehicle |
| CN114413685A (en) * | 2022-02-24 | 2022-04-29 | 北京化工大学 | Black unmanned aerial vehicle trapping apparatus that flies |
-
2017
- 2017-01-18 CN CN201720066964.5U patent/CN206847481U/en active Active
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108534603A (en) * | 2018-04-16 | 2018-09-14 | 无锡北方湖光光电有限公司 | Laser ranging night sight, anti-unmanned plane catch rifle and its application method with net |
| CN112829908A (en) * | 2019-11-25 | 2021-05-25 | 福永干夫 | Torpedo defense system |
| CN110849219A (en) * | 2019-12-03 | 2020-02-28 | 日照金慧科技信息咨询有限公司 | Improve unmanned aerial vehicle trapper of catching effect |
| RU2745590C1 (en) * | 2020-04-03 | 2021-03-29 | Федеральное государственное унитарное предприятие "Российский федеральный ядерный центр - Всероссийский научно-исследовательский институт технической физики имени академика Е.И. Забабахина" | Method for capture of air target with a net |
| CN113587730A (en) * | 2021-08-30 | 2021-11-02 | 航宇救生装备有限公司 | Umbrella net storage bag for unmanned aerial vehicle net capture |
| CN113587730B (en) * | 2021-08-30 | 2022-11-25 | 航宇救生装备有限公司 | Umbrella net storage bag for unmanned aerial vehicle net capture |
| CN114153223A (en) * | 2021-09-22 | 2022-03-08 | 航天科工微电子系统研究院有限公司 | Net type capturing system and method for clustered unmanned aerial vehicle |
| CN114413685A (en) * | 2022-02-24 | 2022-04-29 | 北京化工大学 | Black unmanned aerial vehicle trapping apparatus that flies |
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