CN209126962U - A kind of net bullet formula UAV Intelligent blocking apparatus - Google Patents
A kind of net bullet formula UAV Intelligent blocking apparatus Download PDFInfo
- Publication number
- CN209126962U CN209126962U CN201821959810.XU CN201821959810U CN209126962U CN 209126962 U CN209126962 U CN 209126962U CN 201821959810 U CN201821959810 U CN 201821959810U CN 209126962 U CN209126962 U CN 209126962U
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- CN
- China
- Prior art keywords
- blocking apparatus
- net
- launching tube
- impact block
- holder
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
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- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
The utility model discloses a kind of net bullet formula UAV Intelligent blocking apparatus, the utility model relates to unmanned plane blocking apparatus fields, including unmanned aerial vehicle body, wing and holder, it further include blocking apparatus, the wing is fixedly mounted on the outer surface of unmanned aerial vehicle body, the holder is fixedly mounted on the bottom of unmanned aerial vehicle body, the bottom surface of the holder, which is from left to right fixedly connected sequentially, connecting rod and buffer bar, and the connecting rod and buffer bar are fixedly connected with the upper surface of blocking apparatus respectively；The utility model fixes the position of impact block by electronic range, impact block compresses brute spring, when unmanned plane hovering, rotary platform aims at interceptor, transmitting for intercept net is controlled in the switch of control electronic range, intercept net will wind object after hitting the mark, and achieve the purpose that shoot down.
Description
Technical field
The utility model relates to unmanned plane blocking apparatus fields, more specifically to a kind of net bullet formula UAV Intelligent
Blocking apparatus.
Background technique
In recent years, various civilian consumer level unmanned planes using more and more extensive, bring convenience to production and living.These
Aircraft altitude is low, speed is slow, and radar area is small (so-called " low slow small " aircraft), is difficult to find on ground, is difficult
With control, also become increasingly conspicuous to seriously threatening for highest priority, key area and occasion generation.How to violation unmanned plane
Manage/defence has become a hot issue.Anti- the preferred object of " low slow small " is right before it invades sensitive airspace
It is effectively intercepted.
Unmanned plane blocking apparatus on the market, which does not have, at present is shooting down unmanned plane in the way of air-launched intercept net
Function.
Utility model content
Do not have purpose of the utility model is to solve existing unmanned plane blocking apparatus and is blocked using air-launched
It cuts mode the problem of shooting down unmanned plane function of net, and a kind of net bullet formula UAV Intelligent blocking apparatus proposed.
To achieve the goals above, the utility model adopts the technical scheme that
A kind of net bullet formula UAV Intelligent blocking apparatus, including unmanned aerial vehicle body, wing and holder further include intercepting dress
It sets, the wing is fixedly mounted on the outer surface of unmanned aerial vehicle body, and the holder is fixedly mounted on the bottom of unmanned aerial vehicle body
Portion, the bottom surface of the holder, which is from left to right fixedly connected sequentially, connecting rod and buffer bar, the connecting rod and buffering
Bar is fixedly connected with the upper surface of blocking apparatus respectively.
Preferably, the blocking apparatus includes launching tube, intercept net, impact block and brute spring, the strength bullet
Spring is fixedly connected with right end inside launching tube, and the other end of the brute spring is fixedly connected with impact block, the interception
Net is movably arranged on the inside of launching tube, and middle part is fixedly installed with locating rod, the locating rod difference in the launching tube
Through intercept net and impact block, the impact block upper end is fixedly installed with locking device, and the upper end of the launching tube is fixed
Electronic range is installed, the locking device matches with electronic range, and brute spring can launch intercept net out of launching tube
It goes out.
Preferably, the locking device includes fixed link and block, and bottom end and the impact block of the fixed link are fixed
Connection, the block are fixedly mounted on the upper end of fixed link, and the electronic range includes pedestal and telescopic rod, the pedestal
It is fixedly mounted on the upper surface of launching tube, the telescopic rod is movably arranged on pedestal upper end, the telescopic rod and block phase
Matching, the upper surface of the launching tube are provided with sliding groove, and the outer surface of the fixed link is fixedly installed with bail, described
Bail match with sliding groove, locking device can be limited effect to brute spring, for do ejection intercept net switch.
Preferably, the central part of the intercept net and impact block is provided with location hole, the location hole and positioning
Bar matches, and locating rod can do certain positioning action, and certain deviation occurs when preventing intercept net from launching.
Preferably, be fixedly installed with processor in the unmanned aerial vehicle body, the processor respectively with holder and electricity
Sub bar electrical connection, the angle that processor can control cloud platform rotation are used to adjust the aiming of launching tube, and control electronic range can be controlled
The transmitting of intercept net processed.
Compared with prior art, the utility model provides a kind of net bullet formula UAV Intelligent blocking apparatus, has following
The utility model has the advantages that
(1) in the utility model, unmanned plane mainly includes unmanned aerial vehicle body and wing, and solid in the lower end of unmanned aerial vehicle body
Dingan County fills holder, and the bottom end of holder is fixedly connected with blocking apparatus, and unmanned plane hovering in the sky, and passes through remote control nothing when use
Man-machine adjusting cloud platform rotation, makes blocking apparatus alignment target object, blocking apparatus include launching tube, intercept net, impact block and
Brute spring, in advance by the locking device of mobile impact block upper end, impact block also will and then movement compress brute spring, then to
Intercept net is filled in launching tube, when holder drives launching tube run-home object, remote control electric bar loses electronic range pair
The restriction effect of locking device, intercept net are launched under the action of brute spring, and hit the mark object and is twined using intercept net
Around the rotor of object, achieve the effect that shoot down, certain rush will be will receive in the launching tube in a flash that intercept net is launched
It hits, the buffer bar between holder and launching tube will slow down the impact of a part, and shaking is avoided to cause damages unmanned aerial vehicle body；
(2) in the utility model, by the way that sliding groove is arranged in launching tube upper end, the fixation rod outer surface on locking device is solid
Dingan County is loaded nail, and bail matches with sliding groove, and fixed link is avoided to shake when moving on sliding groove, tight when needing
When locking impact block, the telescopic rod on electronic range can be shunk, moving fixed link is moved to the block in fixed link to stretch
The position of contracting bar, rise telescopic rod block telescopic rod by block, telescopic rod bottom built-in motor and motor work can make
Telescopic rod rises or shrinks, and when the processor control electronic range inside unmanned aerial vehicle body is shunk, block loses telescopic rod
Restriction effect intercept net will be launched away under the action of brute spring, achieve the effect that shoot down object.
Detailed description of the invention
Fig. 1 is the structural schematic diagram of the utility model；
Fig. 2 is the structural schematic diagram of the utility model blocking apparatus；
Fig. 3 is the cross-sectional view of the utility model launching tube；
Fig. 4 is the side view of the utility model launching tube.
Figure label explanation:
1, unmanned aerial vehicle body；2, wing；3, blocking apparatus；4, holder；5, connecting rod；6, buffer bar；7, launching tube；8, fixed
Position bar；9, intercept net；10, impact block；11, brute spring；12, locking device；13, electronic range；14, sliding groove；15, it positions
Hole；16, bail；17, fixed link；18, block；19, pedestal；20, telescopic rod.
Specific embodiment
The following is a combination of the drawings in the embodiments of the present utility model；The technical scheme in the embodiment of the utility model is carried out
Clearly and completely describe；Obviously；The described embodiments are only a part of the embodiments of the utility model；Rather than whole
Embodiment.Based on the embodiments of the present invention；Those of ordinary skill in the art are without making creative work
Every other embodiment obtained；It fall within the protection scope of the utility model.
Embodiment 1: Fig. 1-3, a kind of net bullet formula UAV Intelligent blocking apparatus, including unmanned aerial vehicle body 1, wing are please referred to
2 and holder 4, it further include blocking apparatus 3, wing 2 is fixedly mounted on the outer surface of unmanned aerial vehicle body 1, and holder 4 is fixedly mounted on nothing
The bottom of man-machine fuselage 1, the bottom surface of holder 4, which is from left to right fixedly connected sequentially, connecting rod 5 and buffer bar 6,5 He of connecting rod
Buffer bar 6 is fixedly connected with the upper surface of blocking apparatus 3 respectively.
Blocking apparatus 3 includes launching tube 7, intercept net 9, impact block 10 and brute spring 11, brute spring 11 and launching tube 7
Internal right end is fixedly connected, and the other end of brute spring 11 is fixedly connected with impact block 10, and intercept net 9 is movably arranged on launching tube
7 inside, the interior middle part of launching tube 7 are fixedly installed with locating rod 8, and locating rod 8 extends through intercept net 9 and impact block 10, impact
10 upper end of block is fixedly installed with locking device 12, and the upper end of launching tube 7 is fixedly installed with electronic range 13, locking device 12 and electronics
Bar 13 matches.
In the utility model, unmanned plane mainly includes unmanned aerial vehicle body 1 and wing 2, and solid in the lower end of unmanned aerial vehicle body 1
Dingan County fills holder 4, and the bottom end of holder 4 is fixedly connected with blocking apparatus 3, when use unmanned plane hovering in the sky, and by distant
Control unmanned plane and adjust holder 4 and rotate, make 3 alignment target object of blocking apparatus, blocking apparatus 3 include launching tube 7, intercept net 9,
Impact block 10 and brute spring 11, in advance by the locking device 12 of mobile 10 upper end of impact block, impact block 10 also will be moved and then
Brute spring 11 is compressed, then fills intercept net 9 into launching tube 7, when holder 4 drives 7 run-home object of launching tube,
Remote control electric bar 13 makes electronic range 13 lose the restriction effect to locking device 12, and intercept net 9 is under the action of brute spring 11
Launch, the rotor of hit the mark object and the utilization winding object of intercept net 9 achievees the effect that shoot down, emit in intercept net 9
The launching tube in a flash 7 gone out will have certain impact, and the buffer bar 6 between holder 4 and launching tube 7 will slow down one
The impact divided avoids shaking from causing damages unmanned aerial vehicle body 1.
Embodiment 2: referring to Fig. 4, the 1 different place in basis is that locking device 12 includes solid in conjunction with the embodiments
The bottom end of fixed pole 17 and block 18, fixed link 17 is fixedly connected with impact block 10, and block 18 is fixedly mounted on the upper of fixed link 17
End, electronic range 13 include pedestal 19 and telescopic rod 20, and pedestal 19 is fixedly mounted on the upper surface of launching tube 7,20 activity of telescopic rod
It is mounted on 19 upper end of pedestal, telescopic rod 20 matches with block 18, and the upper surface of launching tube 7 is provided with sliding groove 14, fixed link
17 outer surface is fixedly installed with bail 16, and bail 16 matches with sliding groove 14.
The central part of intercept net 9 and impact block 10 is provided with location hole 15, and location hole 15 matches with locating rod 8.
Processor is fixedly installed in unmanned aerial vehicle body 1, processor is electrically connected with holder 4 and electronic range 13 respectively.
In the utility model, by the way that sliding groove 14 is arranged in 7 upper end of launching tube, 17 appearance of fixed link on locking device 12
Bail 16 is fixedly mounted in face, and bail 16 matches with sliding groove 14, avoids hair when moving on sliding groove 14 of fixed link 17
It is raw to shake, when needing tight lock impact block 10, the telescopic rod 20 on electronic range 13 can be shunk, mobile fixed link 17 makes
Block 18 in fixed link 17 is moved to the position of telescopic rod 20, blocks telescopic rod 20 by block 18 rising telescopic rod 20,
20 bottom built-in motor of telescopic rod and motor work can make the rise of telescopic rod 20 or shrink, the place inside unmanned aerial vehicle body 1
When managing the device control contraction of electronic range 13, the restriction effect that block 18 loses telescopic rod 20 will be in the effect of brute spring 11
It is lower to launch away intercept net 9, achieve the effect that shoot down object.
It is described above；The only preferable specific embodiment of the utility model；But the protection scope of the utility model is not
It is confined to this；Anyone skilled in the art is within the technical scope disclosed by the utility model；It is practical according to this
Novel technical solution and its improvement design is subject to equivalent substitution or change；It should all cover in the protection scope of the utility model
It is interior.In addition, one word of " comprising " is not excluded for other elements or step, "one" word before the component is not excluded for including " multiple " be somebody's turn to do
Element.The multiple multiple elements stated in claim to a product can also by an element by software or hardware come real
It is existing.The first, the second equal words are used to indicate names, and are not indicated any particular order.
Claims (5)
1. a kind of net bullet formula UAV Intelligent blocking apparatus, including unmanned aerial vehicle body (1), wing (2) and holder (4), feature
It is: further includes blocking apparatus (3), the wing (2) is fixedly mounted on the outer surface of unmanned aerial vehicle body (1), the cloud
Platform (4) is fixedly mounted on the bottom of unmanned aerial vehicle body (1), and the bottom surface of the holder (4) is from left to right fixedly connected sequentially
There are connecting rod (5) and buffer bar (6), the connecting rod (5) and buffer bar (6) are solid with the upper surface of blocking apparatus (3) respectively
Fixed connection.
2. a kind of net bullet formula UAV Intelligent blocking apparatus according to claim 1, it is characterised in that: the interception dress
Setting (3) includes launching tube (7), intercept net (9), impact block (10) and brute spring (11), the brute spring (11) and hair
The internal right end of shooting cylinder (7) is fixedly connected, and the other end of the brute spring (11) is fixedly connected with impact block (10), described
Intercept net (9) is movably arranged on the inside of launching tube (7), and middle part is fixedly installed with locating rod (8) in the launching tube (7),
The locating rod (8) extends through intercept net (9) and impact block (10), and the impact block (10) upper end is fixedly installed with tightly
Locking device (12), the upper end of the launching tube (7) are fixedly installed with electronic range (13), the locking device (12) and electronics
Bar (13) matches.
3. a kind of net bullet formula UAV Intelligent blocking apparatus according to claim 2, it is characterised in that: the tight lock dress
Setting (12) includes fixed link (17) and block (18), and the bottom end of the fixed link (17) is fixedly connected with impact block (10), institute
The block (18) stated is fixedly mounted on the upper end of fixed link (17), and the electronic range (13) includes pedestal (19) and telescopic rod
(20), the pedestal (19) is fixedly mounted on the upper surface of launching tube (7), and the telescopic rod (20) is movably arranged on pedestal
(19) upper end, the telescopic rod (20) match with block (18), and the upper surface of the launching tube (7) is provided with sliding groove
(14), the outer surface of the fixed link (17) is fixedly installed with bail (16), the bail (16) and sliding groove (14) phase
Matching.
4. a kind of net bullet formula UAV Intelligent blocking apparatus according to claim 2, it is characterised in that: the intercept net
(9) it is provided with location hole (15) with the central part of impact block (10), the location hole (15) matches with locating rod (8).
5. a kind of net bullet formula UAV Intelligent blocking apparatus according to claim 1, it is characterised in that: the unmanned plane
It is fixedly installed with processor in fuselage (1), the processor is electrically connected with holder (4) and electronic range (13) respectively.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821959810.XU CN209126962U (en) | 2018-11-27 | 2018-11-27 | A kind of net bullet formula UAV Intelligent blocking apparatus |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821959810.XU CN209126962U (en) | 2018-11-27 | 2018-11-27 | A kind of net bullet formula UAV Intelligent blocking apparatus |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209126962U true CN209126962U (en) | 2019-07-19 |
Family
ID=67246812
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821959810.XU Expired - Fee Related CN209126962U (en) | 2018-11-27 | 2018-11-27 | A kind of net bullet formula UAV Intelligent blocking apparatus |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN209126962U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111272019A (en) * | 2020-03-27 | 2020-06-12 | 牛三库 | Intelligent elastic net |
| CN114671028A (en) * | 2022-05-30 | 2022-06-28 | 西安杰出科技有限公司 | Police is with catching unmanned aerial vehicle |
-
2018
- 2018-11-27 CN CN201821959810.XU patent/CN209126962U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111272019A (en) * | 2020-03-27 | 2020-06-12 | 牛三库 | Intelligent elastic net |
| CN114671028A (en) * | 2022-05-30 | 2022-06-28 | 西安杰出科技有限公司 | Police is with catching unmanned aerial vehicle |
| CN114671028B (en) * | 2022-05-30 | 2022-11-18 | 南京拓恒无人系统研究院有限公司 | Police catching unmanned aerial vehicle |
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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: 20190719 Termination date: 20191127 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |