CN205098467U - Arms unmanned aerial vehicle - Google Patents

Arms unmanned aerial vehicle Download PDF

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Publication number
CN205098467U
CN205098467U CN201520814971.XU CN201520814971U CN205098467U CN 205098467 U CN205098467 U CN 205098467U CN 201520814971 U CN201520814971 U CN 201520814971U CN 205098467 U CN205098467 U CN 205098467U
Authority
CN
China
Prior art keywords
rotor
aerial vehicle
unmanned aerial
electromagnetism
main part
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.)
Expired - Fee Related
Application number
CN201520814971.XU
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Chinese (zh)
Inventor
黄耀辉
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
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Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to CN201520814971.XU priority Critical patent/CN205098467U/en
Application granted granted Critical
Publication of CN205098467U publication Critical patent/CN205098467U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The utility model provides an arms unmanned aerial vehicle, including unmanned aerial vehicle main part and magnetic artillery main part, the unmanned aerial vehicle main part on be provided with the mounting platform, install the magnetic artillery main part on the mounting platform, the magnetic artillery main part includes electromagnetism barrel and sight, the electromagnetism barrel be two, be provided with the sight between two electromagnetism barrels, be provided with electromagnetic launcher in the left side of sight, the right side is provided with the battery, the utility model discloses a rotary rod is connected with dismantling of mounting platform, can dwindle holistic volume, reduces the space area who takies, and rotor mast is the rectangle, has made things convenient for to set up solar panel on rotor mast, increases unmanned aerial vehicle's flight time, guarantees safe coming and going, the solution of installation electromagnetism arms leads to the unable use of traditional firearms weapon problem on ordinary unmanned aerial vehicle owing to unmanned aerial vehicle's stability and the recoil's of traditional firearms problem on unmanned aerial vehicle, the possibility of unmanned aerial vehicle as the attack plane has been realized like this.

Description

A kind of armed drones
Technical field
The utility model relates to a kind of armed drones.
Background technology
Along with the progress of society, the development of science and technology, the technology of unmanned plane is more and more ripe, civilian unmanned plane of taking photo by plane is more and more universal, but go no further with in UAV flight's weapon people's police always, because the problem of the stability of unmanned plane and the Backlash of traditional firearms cannot solve always, cause traditional firearms weapon cannot be used on common unmanned plane.Along with the development of science and technology, unmanned plane stability is become better and better, and the Backlash problem of traditional firearms still cannot solve, and the appearance of electromagnetism firearms solves this problem.Electromagnetism firearm recoil is then very little, can not have any impact, unmanned plane and electromagnetism firearms are tied the difficult problem thoroughly solving common UAV flight's weapon mutually time electromagnetism firearms start to the stable of unmanned plane.
Utility model content
Problem to be solved in the utility model is to provide a kind of armed drones.
For solving the problems of the technologies described above, the technical solution adopted in the utility model is: a kind of armed drones, comprise unmanned plane main body and magnetic artillery main body, it is characterized in that: described unmanned plane main body is provided with erecting stage, erecting stage is provided with magnetic artillery main body, magnetic artillery main body comprises electromagnetism gun tube and back sight, described electromagnetism gun tube is two, between two electromagnetism gun tubes, be provided with back sight, the left side of back sight is provided with electromagnetic launcher, and right side is provided with battery.
Further, described erecting stage is provided with rotor bar, rotor bar one end is arranged on erecting stage, and the other end is provided with rotor.
Further, described erecting stage is arranged four rotor bars, each rotor bar structure is identical.
Further, described rotor is divided into rotor and lower rotor, and described upper rotor is arranged on rotor bar upper end, and lower rotor is arranged on the lower end of rotor bar.
Further, described rotor bar and erecting stage removably connect.
Further, described upper rotor and lower rotor are coaxially arranged on rotor bar.
Further, described unmanned plane is provided with camera.
Further, described rotor bar is rectangle, and rotor bar upper surface is provided with solar panels.
The advantage that the utility model has and beneficial effect are: removably connecting of revolving bar and erecting stage, overall volume can be reduced, reduce the spatial area taken, rotor bar is rectangle, facilitate and solar panels are set on rotor bar, increase the flight time of unmanned plane, ensure coming and going of safety; Unmanned plane is installed electromagnetism firearms and solves problem due to the stability of unmanned plane and the Backlash of traditional firearms, cause traditional firearms weapon cannot be used in problem on common unmanned plane; Achieve the possibility of unmanned plane as attack plane like this.
Accompanying drawing explanation
Fig. 1 is the utility model structural representation;
Fig. 2 is magnetic artillery agent structure schematic diagram in Fig. 1.
Fig. 3 is unmanned plane agent structure schematic diagram in Fig. 1.
In figure: 1, battery, 2, rotor bar, 3, rotor, 4, back sight, 5, electromagnetism gun tube, 6, camera, 7, erecting stage, 8, electromagnetic launcher.
Detailed description of the invention
Below in conjunction with accompanying drawing, specific embodiment of the utility model is elaborated.
As shown in Figure 1, Figure 2, Figure 3 shows, a kind of armed drones, comprise unmanned plane main body and magnetic artillery main body, unmanned plane main body is provided with erecting stage 7, erecting stage 7 is provided with magnetic artillery main body, magnetic artillery main body comprises electromagnetism gun tube 5 and back sight 4, described electromagnetism gun tube 5 is two, between two electromagnetism gun tubes 5, be provided with back sight 4, the left side of back sight 4 is provided with electromagnetic launcher 8, right side is provided with battery 1.
Erecting stage 7 is provided with rotor bar 2, rotor bar 2 one end is arranged on erecting stage 7, and the other end is provided with rotor 3; Erecting stage 7 is arranged four rotor bars 2, each rotor bar 2 structure is identical; Rotor 3 is divided into rotor and lower rotor, and upper rotor is arranged on rotor bar 2 upper end, and lower rotor is arranged on the lower end of rotor bar 2; Rotor bar 2 and erecting stage 7 removably connect.
Upper rotor and lower rotor are coaxially arranged on rotor bar 2; Unmanned plane is provided with camera 6; Rotor bar 2 is rectangle, and rotor bar 2 upper surface is provided with solar panels.
Removably connecting of revolving bar of the present utility model and erecting stage 7, can reduce overall volume, reduces the spatial area taken, rotor bar 2 is rectangles, facilitate and solar panels are set on rotor bar 2, increase the flight time of unmanned plane, ensure coming and going of safety; Unmanned plane is installed electromagnetism firearms and solves problem due to the stability of unmanned plane and the Backlash of traditional firearms, cause traditional firearms weapon cannot be used in problem on common unmanned plane; Achieve the possibility of unmanned plane as attack plane like this.
Above an embodiment of the present utility model has been described in detail, but described content being only preferred embodiment of the present utility model, can not being considered to for limiting practical range of the present utility model.All equalizations done according to the utility model application range change and improve, and all should still belong within patent covering scope of the present utility model.

Claims (8)

1. an armed drones, comprise unmanned plane main body and magnetic artillery main body, it is characterized in that: described unmanned plane main body is provided with erecting stage (7), erecting stage (7) is provided with magnetic artillery main body, magnetic artillery main body comprises electromagnetism gun tube (5) and back sight (4), described electromagnetism gun tube (5) is two, back sight (4) is provided with between two electromagnetism gun tubes (5), the left side of back sight (4) is provided with electromagnetic launcher (8), and right side is provided with battery (1).
2. a kind of armed drones according to claim 1, it is characterized in that: described erecting stage (7) is provided with rotor bar (2), rotor bar (2) one end is arranged on erecting stage (7), and the other end is provided with rotor (3).
3. a kind of armed drones according to claim 2, is characterized in that: described erecting stage (7) is arranged four rotor bars (2), and each rotor bar (2) structure is identical.
4. a kind of armed drones according to claim 3, it is characterized in that: described rotor (3) is divided into rotor and lower rotor, described upper rotor is arranged on rotor bar (2) upper end, and lower rotor is arranged on the lower end of rotor bar (2).
5. a kind of armed drones according to claim 4, is characterized in that: described rotor bar (2) and erecting stage (7) removably connect.
6. a kind of armed drones according to claim 5, is characterized in that: described upper rotor and lower rotor are coaxially arranged on rotor bar (2).
7. a kind of armed drones according to claim 6, is characterized in that: described unmanned plane is provided with camera (6).
8. a kind of armed drones according to claim 7, is characterized in that: described rotor bar (2) is rectangle, and rotor bar (2) upper surface is provided with solar panels.
CN201520814971.XU 2015-10-20 2015-10-20 Arms unmanned aerial vehicle Expired - Fee Related CN205098467U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201520814971.XU CN205098467U (en) 2015-10-20 2015-10-20 Arms unmanned aerial vehicle

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201520814971.XU CN205098467U (en) 2015-10-20 2015-10-20 Arms unmanned aerial vehicle

Publications (1)

Publication Number Publication Date
CN205098467U true CN205098467U (en) 2016-03-23

Family

ID=55514268

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201520814971.XU Expired - Fee Related CN205098467U (en) 2015-10-20 2015-10-20 Arms unmanned aerial vehicle

Country Status (1)

Country Link
CN (1) CN205098467U (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106477047A (en) * 2016-11-23 2017-03-08 深圳市轻准科技有限公司 A kind of aerial howitzer launch craft
CN108327897A (en) * 2018-03-09 2018-07-27 深圳市轻准科技有限公司 Equip with arms unmanned helicopter
CN108341060A (en) * 2018-04-17 2018-07-31 深圳市轻准科技有限公司 Deflectable transmitting ammunition unmanned plane

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106477047A (en) * 2016-11-23 2017-03-08 深圳市轻准科技有限公司 A kind of aerial howitzer launch craft
CN108327897A (en) * 2018-03-09 2018-07-27 深圳市轻准科技有限公司 Equip with arms unmanned helicopter
CN108341060A (en) * 2018-04-17 2018-07-31 深圳市轻准科技有限公司 Deflectable transmitting ammunition unmanned plane

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Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20160323

Termination date: 20161020

CF01 Termination of patent right due to non-payment of annual fee