CN108981473A - A kind of hold-up interception method of pair of rotor wing unmanned aerial vehicle - Google Patents
A kind of hold-up interception method of pair of rotor wing unmanned aerial vehicle Download PDFInfo
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- CN108981473A CN108981473A CN201810846907.8A CN201810846907A CN108981473A CN 108981473 A CN108981473 A CN 108981473A CN 201810846907 A CN201810846907 A CN 201810846907A CN 108981473 A CN108981473 A CN 108981473A
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- airspace
- aerial vehicle
- unmanned aerial
- rotor wing
- wing unmanned
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41H—ARMOUR; ARMOURED TURRETS; ARMOURED OR ARMED VEHICLES; MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL
- F41H11/00—Defence installations; Defence devices
- F41H11/02—Anti-aircraft or anti-guided missile or anti-torpedo defence installations or systems
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- General Engineering & Computer Science (AREA)
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Abstract
The invention discloses the hold-up interception method of a kind of pair of rotor wing unmanned aerial vehicle, setting intercepts airspace, delivers elongated strip lightweight silk ribbon item to intercepting in airspace, fills silk ribbon item and is trapped in intercept in airspace, be wound interception to the rotor wing unmanned aerial vehicle of entrance.The invention has the advantages that at low cost, can the rotor wing unmanned aerial vehicle effectively to aerial small-sized low speed implement to intercept, under effect on environment, and not by electromagnetic interference, easy to operate, putting mode is flexible and varied.
Description
Technical field
The present invention relates to air vehicle technique fields, more particularly, to the Interception Technology of a kind of pair of unmanned plane.
Background technique
With the development and application of modern unmanned plane, flying quality, concealment and the information collecting capacity of unmanned plane are obtained
To the unmanned plane of biggish promotion, especially rotor, integrated level is high, small in size, in the important field such as certain megaevent, meeting
Under conjunction or the state of war, hostile force can use a large amount of rotor wing unmanned aerial vehicle group and carry out to important events or strategic area
Saturation is destroyed or interference.Therefore it needs to come the unmanned plane attacked, especially unmanned aerial vehicle group is effectively intercepted.
The hard Casualty Mode directly hit is generallyd use to the interception mode of unmanned plane, such as using guided missile, shell to nothing
It is man-machine to be shot at interception, but this method is not high for the depletion efficiency of a large amount of rotor wing unmanned aerial vehicle group, and can generate after attacking
A large amount of fragment or residue, be easy to cause collateral damage, constitute significant threat to Friday personnel or Environmental security.According to
On the one hand the soft destruction mode of laser weapon or radio interference is limited to the complexity of entire blocking apparatus, cost is high, makes
With and maintenance can also have difficulties, on the other hand the intercepting system of these soft destruction modes itself is also easy to receive extraneous interference
And intrusion, system reliability is not high, can similarly generate the electromagnetic pollution situation to environment.
Summary of the invention
The object of the present invention is to provide the hold-up interception method of a kind of pair of rotor wing unmanned aerial vehicle, can effectively intercept unmanned plane or nobody
A group of planes, and collateral damage will not be generated, it is also small to environmental disturbances.
The technical solution of the invention is as follows: the hold-up interception method of a kind of pair of rotor wing unmanned aerial vehicle, and setting intercepts airspace, to interception
Deliver elongated strip lightweight silk ribbon item in airspace, fill silk ribbon item and be trapped in interception airspace, to the rotor of entrance nobody
Machine is wound interception.
It, can be with after being detected by radar or optical detection means when rotor wing unmanned aerial vehicle or a group of planes invade our region
Elongate strip lightweight silk ribbon item is delivered in airspace to intercepting, this silk ribbon item, which can be swum in, to be intercepted in airspace, is had longer stagnant
The empty time, under the promotion of rotor air-flow, it is easy to be wrapped on the rotor of rotor wing unmanned aerial vehicle, unmanned plane is made to run out of steam and fall
It falls, there is preferable interception effect to the rotor wing unmanned aerial vehicle intercepted in region is entered, and destructive fragment will not be generated, to ring
Border does not also influence directly, at low cost, can implement effectively to intercept to the rotor wing unmanned aerial vehicle of aerial small-sized low speed.
Further include the steps that prejudging rotor wing unmanned aerial vehicle approach axis and default interception airspace.It is long using the silk ribbon hang time
The characteristics of, airspace can be intercepted with preset in advance, to improve intercepting efficiency and protection effective time.
Include the steps that delivering the silk ribbon into default interception airspace using unmanned plane or the aircraft that downsizes.Delivery side
Just, it and can use the term of validity that stagnant empty aircraft extends interception protection, improve protection effect.
Including entering interception in rotor wing unmanned aerial vehicle using in the balloon for intercepting the preset silk ribbon item built in several in airspace
The mode of balloon is ignited behind airspace to the step of intercepting airspace delivery silk ribbon.Balloon can also stagnant sky for a long time, setting also side
Just, after silk ribbon items a large amount of built in balloon, when rotor wing unmanned aerial vehicle invades airspace, balloon is ignited by modes such as ground drawstrings,
The silk ribbon item is discharged in default airspace, can also quickly be formed and intercept airspace.
Include the steps that transmitting ignites the shell of built-in silk ribbon item to deliver the silk ribbon into default interception airspace.It throws
It send fast, can quickly be formed and intercept airspace, improve reaction speed.
The shell of the built-in silk ribbon item includes the silk ribbon item that the explosive at middle part is arranged in and is coated on around explosive.Structure
Simply, using the omnidirectional push silk ribbon item of blast wave, covering surface is improved.
The invention has the advantages that at low cost, can the rotor wing unmanned aerial vehicle effectively to aerial small-sized low speed implement to intercept, to environment
Under the influence of, and not by electromagnetic interference, easy to operate, putting mode is flexible and varied.
Detailed description of the invention
Attached drawing 1 is that the embodiment of the present invention intercepts schematic diagram to unmanned plane；
1, rotor wing unmanned aerial vehicle, 2, silk ribbon item, 3, interception airspace.
Specific embodiment
Embodiment:
Refering to fig. 1, the hold-up interception method of a kind of pair of rotor wing unmanned aerial vehicle, comprising the following steps:
1., anticipation 1 approach axis of rotor wing unmanned aerial vehicle, and default intercept airspace 3；
2., to intercept airspace 3 in deliver elongated strip lightweight silk ribbon item 2, make silk ribbon item 2 fill and be trapped in intercept airspace
In 3, interception is wound to the rotor wing unmanned aerial vehicle 1 of entrance.
When rotor wing unmanned aerial vehicle or a group of planes invade our region, can be detected by radar or optical detection means,
Its approach axis is prejudged, and presets intercept airspace 3 in this direction, delivers elongate strip lightweight silk ribbon item 2 in airspace 3 to intercepting,
This light weight of silk ribbon item 2 itself can swim in and intercept in airspace, have the longer hang time, in pushing away for rotor air-flow
Under dynamic, elongate strip structure is also easy to be wrapped on the rotor of rotor wing unmanned aerial vehicle, so that unmanned plane is run out of steam or is balanced and falls,
There is preferable interception effect to the rotor wing unmanned aerial vehicle intercepted in region 3 is entered, and itself will not generate destructive fragment, it is right
Environment does not also influence directly, at low cost, can implement effectively to intercept to the rotor wing unmanned aerial vehicle of aerial small-sized low speed.Utilize silk
The feature of 2 hang time of tape length can intercept airspace 3 with preset in advance, to improve intercepting efficiency and protection effective time.
Further include the steps that delivering the silk ribbon into default interception airspace using unmanned plane or manned vehicle.Nobody
Machine or manned vehicle itself have the longer hang time, thus further extend intercept protection term of validity, and deliver away from
From remote, it is convenient to deliver, and can use stagnant empty aircraft and extend the term of validity for intercepting protection, improves protection effect.
Including entering interception in rotor wing unmanned aerial vehicle using in the balloon for intercepting the preset silk ribbon item built in several in airspace
The mode of balloon is ignited behind airspace to the step of intercepting airspace delivery silk ribbon.Balloon can also stagnant sky for a long time, setting also side
Just, after silk ribbon items a large amount of built in balloon, when rotor wing unmanned aerial vehicle invades airspace, balloon is ignited by modes such as ground drawstrings,
The silk ribbon item is discharged in default airspace, can also quickly be formed and intercept airspace.
Further include the steps that transmitting ignites the shell of built-in silk ribbon item 2 to deliver silk ribbon item 2 into default interception airspace 3.
The shell of the built-in silk ribbon item includes the silk ribbon item that the explosive at middle part is arranged in and is coated on around explosive, is produced using explosive charge
Raw shock wave is pushed the silk ribbon item that surrounding coats open, around to fill biggish interception airspace.This delivery mode,
It can be used for blocking the case where unmanned aerial vehicle group is more evacuated, deliver quick, the biggish interception airspace of Fast Filling, broad covered area.
Above-listed detailed description is illustrating for one of present invention possible embodiments, and the embodiment is not to limit
The scope of the patents of the invention, all equivalence enforcements or change without departing from carried out by the present invention, is intended to be limited solely by the scope of the patents of this case
In.
Claims (6)
1. the hold-up interception method of a kind of pair of rotor wing unmanned aerial vehicle, it is characterised in that: setting intercepts airspace, delivers into interception airspace elongated
Strip lightweight silk ribbon item is filled silk ribbon item and is trapped in intercept in airspace, is wound interception to the rotor wing unmanned aerial vehicle of entrance.
2. the hold-up interception method of a kind of pair of rotor wing unmanned aerial vehicle according to claim 1, it is characterised in that: further include anticipation rotor
Unmanned plane approach axis and default the step of intercepting airspace.
3. the hold-up interception method of a kind of pair of rotor wing unmanned aerial vehicle according to claim 2, it is characterised in that: including using unmanned plane
Or manned vehicle mode to intercept airspace in deliver the silk ribbon the step of.
4. the hold-up interception method of a kind of pair of rotor wing unmanned aerial vehicle according to claim 2, it is characterised in that: intercepted including using
The balloon of several preset built-in silk ribbon items of airspace, ignited after rotor wing unmanned aerial vehicle enters and intercepts airspace the mode of balloon to
Intercept the step of silk ribbon is delivered in airspace.
5. the hold-up interception method of a kind of pair of rotor wing unmanned aerial vehicle according to claim 2, it is characterised in that: including using to interception
The step of shell mode that built-in silk ribbon item is ignited in transmitting in airspace delivers the silk ribbon.
6. the hold-up interception method of a kind of pair of rotor wing unmanned aerial vehicle according to claim 5, it is characterised in that: the built-in silk ribbon item
Shell include the silk ribbon item that the explosive at middle part is set and is coated on around explosive.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810846907.8A CN108981473A (en) | 2018-07-27 | 2018-07-27 | A kind of hold-up interception method of pair of rotor wing unmanned aerial vehicle |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810846907.8A CN108981473A (en) | 2018-07-27 | 2018-07-27 | A kind of hold-up interception method of pair of rotor wing unmanned aerial vehicle |
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| Publication Number | Publication Date |
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| CN108981473A true CN108981473A (en) | 2018-12-11 |
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| CN201810846907.8A Pending CN108981473A (en) | 2018-07-27 | 2018-07-27 | A kind of hold-up interception method of pair of rotor wing unmanned aerial vehicle |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2020208330A1 (en) * | 2019-04-11 | 2020-10-15 | The Secretary Of State For Defence Dstl | Entanglement device and method of use |
| CN114812280A (en) * | 2022-05-24 | 2022-07-29 | 刘加凯 | A fixed-point air-explosive anti-rotor UAV fiber bomb system |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102384702A (en) * | 2010-08-30 | 2012-03-21 | 北京理工大学 | Method for intercepting aircrafts without collateral damage in unmanned way |
| CN205352204U (en) * | 2016-02-25 | 2016-06-29 | 谢琼芳 | A intercepting device for aircraft interception |
| CN205602150U (en) * | 2016-01-30 | 2016-09-28 | 上海仪耐新材料科技有限公司 | Anti - unmanned aerial vehicle of net bullet formula intelligence interception system |
| CN107054678A (en) * | 2017-01-18 | 2017-08-18 | 芜湖博高光电科技股份有限公司 | A kind of vehicle-mounted anti-unmanned plane net bullet intercepting system |
| CN206755998U (en) * | 2017-03-29 | 2017-12-15 | 深圳中翼特种装备制造有限公司 | A kind of intercepting system for SUAV |
| CN108088313A (en) * | 2017-11-20 | 2018-05-29 | 华南农业大学 | A kind of unmanned plane intercepting system |
| CN207540428U (en) * | 2017-11-20 | 2018-06-26 | 华南农业大学 | A kind of unmanned plane blocking apparatus |
-
2018
- 2018-07-27 CN CN201810846907.8A patent/CN108981473A/en active Pending
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102384702A (en) * | 2010-08-30 | 2012-03-21 | 北京理工大学 | Method for intercepting aircrafts without collateral damage in unmanned way |
| CN205602150U (en) * | 2016-01-30 | 2016-09-28 | 上海仪耐新材料科技有限公司 | Anti - unmanned aerial vehicle of net bullet formula intelligence interception system |
| CN205352204U (en) * | 2016-02-25 | 2016-06-29 | 谢琼芳 | A intercepting device for aircraft interception |
| CN107054678A (en) * | 2017-01-18 | 2017-08-18 | 芜湖博高光电科技股份有限公司 | A kind of vehicle-mounted anti-unmanned plane net bullet intercepting system |
| CN206755998U (en) * | 2017-03-29 | 2017-12-15 | 深圳中翼特种装备制造有限公司 | A kind of intercepting system for SUAV |
| CN108088313A (en) * | 2017-11-20 | 2018-05-29 | 华南农业大学 | A kind of unmanned plane intercepting system |
| CN207540428U (en) * | 2017-11-20 | 2018-06-26 | 华南农业大学 | A kind of unmanned plane blocking apparatus |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2020208330A1 (en) * | 2019-04-11 | 2020-10-15 | The Secretary Of State For Defence Dstl | Entanglement device and method of use |
| CN114812280A (en) * | 2022-05-24 | 2022-07-29 | 刘加凯 | A fixed-point air-explosive anti-rotor UAV fiber bomb system |
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Application publication date: 20181211 |