CN108016618A - A kind of ammunition emitter and system - Google Patents
A kind of ammunition emitter and system Download PDFInfo
- Publication number
- CN108016618A CN108016618A CN201711453960.3A CN201711453960A CN108016618A CN 108016618 A CN108016618 A CN 108016618A CN 201711453960 A CN201711453960 A CN 201711453960A CN 108016618 A CN108016618 A CN 108016618A
- Authority
- CN
- China
- Prior art keywords
- ammunition
- installing plate
- emitter
- aerial vehicle
- unmanned aerial
- 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.)
- Pending
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D1/00—Dropping, ejecting, releasing, or receiving articles, liquids, or the like, in flight
- B64D1/02—Dropping, ejecting, or releasing articles
- B64D1/04—Dropping, ejecting, or releasing articles the articles being explosive, e.g. bombs
- B64D1/06—Bomb releasing; Bombs doors
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41F—APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
- F41F1/00—Launching apparatus for projecting projectiles or missiles from barrels, e.g. cannons; Harpoon guns
Abstract
The present invention relates to unmanned air vehicle technique field, there is provided a kind of ammunition emitter and system.A kind of ammunition emitter, including it is fixed on unmanned aerial vehicle platform, the ammunition emitter includes installing plate, upper the setting trigger mechanism and cartridge of the installing plate, and the cartridge is used to load ammunition, and the trigger mechanism is used to control transmitting ammunition；Side of the installing plate away from cartridge passes through a bindiny mechanism and the angled connection of unmanned aerial vehicle platform.The ammunition emitter can be stablized, launch ammunition exactly.The present invention also provides a kind of ammunition emission system, including above-mentioned ammunition emitter.
Description
Technical field
The present invention relates to unmanned air vehicle technique field, more particularly to a kind of ammunition emitter and system.
Background technology
Increasingly mature with unmanned air vehicle technique, unmanned plane is widely used in the field such as military, police and civilian,
Such as surveying and drawing, security monitoring, fire-fighting and military investigation etc..Wherein, unmanned plane is in police sides such as police detecting, Airborne Search
The application in face achieves good effect, also therefore receives more and more attention.Social security is important one of police work
Ring, at some in special circumstances, it is necessary to be kept order using ammunitions such as tear bombnoun, pinking bullet, aerosol bombs.At present, based on nobody
The ammunition of machine platform is mostly directly anchored to below unmanned plane, there is projection stability, accuracy is not high the shortcomings that.
The content of the invention
It is an object of the invention to provide a kind of ammunition emitter and system, can stablize, launch ammunition exactly.
In order to solve the above technical problems, invention uses technical solution as described below.A kind of ammunition emitter, including its
It is fixed on unmanned aerial vehicle platform, the ammunition emitter includes installing plate, the upper setting trigger mechanism of the installing plate
And cartridge, the cartridge are used to load ammunition, the trigger mechanism is used to control transmitting ammunition；The installing plate is away from bullet
The side of cartridge case by a bindiny mechanism and the angled connection of unmanned aerial vehicle platform, and the installing plate and the unmanned aerial vehicle platform it
Between angle be less than or equal to 90 °.
Preferably, the bindiny mechanism is section hollow frame triangular in shape, and the installing plate is put down with the unmanned plane
Angle between platform is fixed.
Preferably, the angle between the installing plate and the unmanned aerial vehicle platform is 15-70 °.
Preferably, the trigger mechanism is arranged in the bindiny mechanism.
Preferably, the first swinging mounting and the second swinging mounting that the bindiny mechanism connects including shaft, described first
Swinging mounting is fixedly connected with unmanned aerial vehicle platform, and second swinging mounting is fixedly connected with installing plate, the installing plate and institute
The angle stated between unmanned aerial vehicle platform adjusts.
Preferably, the cartridge is hung on the installing plate by suspending assembly.
Preferably, the suspending assembly includes clip.
Preferably, the installing plate is equipped with image collecting device.
The present invention also provides a kind of ammunition emission system, including above-mentioned ammunition emitter, unmanned plane and terminal control
Device, the terminal control mechanism are connected with the ammunition emitter, UAV Communication.
Preferably, when the installing plate of the ammunition emitter is equipped with image collecting device, the terminal control dress
Put including an image processing unit.
The beneficial effects of the present invention are：
The present invention provides a kind of ammunition emitter, its installing plate is angled by a bindiny mechanism and unmanned aerial vehicle platform
Connection, first, is attached by bindiny mechanism, can effectively improve the stability of ammunition transmitting；Secondly, installing plate and unmanned plane
It is angled between platform to be fixedly connected, it can realize certain launch angle, can guarantee that the stability of ammunition transmitting, moreover it is possible to improve bullet
The accuracy of medicine transmitting.
Present invention also offers a kind of ammunition emitter, including above-mentioned ammunition emitter, therefore with ammunition hair
The advantages of stability and higher accuracy for penetrating；In addition, the transmitting using terminal control mechanism energy remote control ammunition.
Brief description of the drawings
Fig. 1 is the dimensional structure diagram of the ammunition emitter provided in the present invention.
Fig. 2 is the schematic front view of the ammunition emitter provided in some currently preferred embodiments of the present invention.
Fig. 3 is the structure block diagram of the ammunition emission system provided in the present invention.
Embodiment
To make those of ordinary skill in the art that the purpose, technical scheme and advantage of invention be more clearly understood, below
Invention is further elaborated in conjunction with the accompanying drawings and embodiments.
First embodiment
As shown in Figure 1, a kind of ammunition emitter, it is fixed on unmanned aerial vehicle platform, the ammunition emitter
Including installing plate 2, upper the setting trigger mechanism 3 and cartridge 7 of the installing plate 2, the cartridge 7 are used to load ammunition, institute
State trigger mechanism 3 be used for control transmitting ammunition；The side of the installing plate 2 away from cartridge 7 passes through a bindiny mechanism 1 and nobody
The angled connection of machine platform, and the angle between the installing plate 2 and the unmanned aerial vehicle platform is less than or equal to 90 °.It is appreciated that
The ammunition can be tear bombnoun, pinking bullet, aerosol bomb etc..
Ammunition emitter provided by the present invention, its installing plate 2 are angled by a bindiny mechanism 1 and unmanned aerial vehicle platform
It is fixedly connected, first, is attached by bindiny mechanism 1, the stability of ammunition transmitting can be effectively improved, it is possible to understand that unmanned plane
In the air during flight, stability is poor, and relatively stable emission state can be provided using bindiny mechanism 1.Secondly, installing plate 2 with
Angled connection between unmanned aerial vehicle platform, can realize certain launch angle, can guarantee that the stability of ammunition transmitting, moreover it is possible to improve
The accuracy of ammunition transmitting.It is appreciated that if ammunition horizontal emission, from the distance to land is transmitted to than ramp-launched
Distance, and the resistance bigger being subject to, so as to influence the stability and accuracy of ammunition transmitting；And if tilted to realize
Transmitting, so as to control unmanned plane more to influence the stability that ammunition is launched on the contrary into line tilt.Therefore, connected by setting
Mechanism 1, can just to realize certain launch angle under smooth flight or resting state in unmanned plane.
In certain embodiments, the angle between the installing plate 2 and the unmanned aerial vehicle platform is fixed, the bindiny mechanism
1 section is triangular in shape, and the both sides of same angle are connected with installing plate 2, unmanned aerial vehicle platform respectively.It is preferable real at some
Apply in example, the bindiny mechanism 1 is hollow frame, and the trigger mechanism 3 is arranged in the bindiny mechanism 1, so can be to hair
Penetrate mechanism 3 and form certain protection, extend the service life of the ammunition emitter.Certainly, the trigger mechanism 3 can also
It is directly arranged on installing plate 2, specifically, the trigger mechanism 3 can be microcontroller.
Preferably, the angle between the installing plate 2 and the unmanned aerial vehicle platform is 15-70 °, preferably described installation
Angle between plate 2 and the unmanned aerial vehicle platform is 15-60 °, in some specific embodiments, the angle be 15 °, 30 ° or
45°。
In some preferred embodiments, as shown in Fig. 2, the angle between the installing plate 2 and the unmanned aerial vehicle platform
It is adjustable.The first swinging mounting 11 ' and the second swinging mounting 12 ' that the bindiny mechanism 1 ' connects including shaft, described first
Swinging mounting 11 ' is fixedly connected with unmanned aerial vehicle platform, and second swinging mounting 12 ' is fixedly connected with installing plate 2.So also
It is that the second swinging mounting 12 ' can be rotated around the first swinging mounting 11 ', namely as shown in arrow R in figure, is rotated, so that
Drive installing plate 2 and cartridge 7 to be rotated, realize certain launch angle, and launch angle is adjustable.Specifically, can
To be by setting steering engine to be adjusted.
Preferably, the cartridge 7 is hung on the installing plate 2 by suspending assembly 4.It is further, it is described to hang
Hanging component 4 includes clip, and cartridge 7 can be fixed well using clip, and easy to disassemble is replaced.The clip includes
Along the first clip 41 and the second clip 42 with being arranged in parallel in 2 vertical direction of installing plate, more ammunitions can be loaded.It is preferred that
Ground, is detachably connected between 41 and second clip 42 of the first clip, specifically, can be first clip 41 and second
Clip 42 is connected by a connecting plate 43, and 41 and second clip 42 of the first clip is connected with connecting plate by screw
Connect.
In some preferred embodiments, the installing plate 2 is equipped with image collecting device 5, utilizes the image collector
Putting 5 can be aimed at, and increase the accuracy of transmitting, and described image harvester 5 can be that shooting is first-class.
Second embodiment
As shown in figure 3, a kind of ammunition emission system, including ammunition emitter 10, unmanned plane 20 and terminal control mechanism
30, the ammunition emitter 10 is the ammunition emitter provided in first embodiment.The terminal control mechanism 30
Communicated to connect with the ammunition emitter 10, unmanned plane 20.It is appreciated that the ammunition emitter 10 is installed on unmanned plane
On 20, the terminal control mechanism 30 can be the console positioned at ground, therefore can realize at a distance to 20 He of unmanned plane
The control of ammunition emitter 10, so as to accurately launch ammunition.It is appreciated that when the installing plate of the ammunition emitter 10
When angle between 2 and unmanned aerial vehicle platform is adjustable, the terminal control mechanism 30 can be carried out with remote control bindiny mechanism 1 '
The adjustment of angle.
It is further, when the installing plate 2 of the ammunition emitter 10 is equipped with image collecting device 5, the end
End control device 30 includes an image processing unit.The image namely collected using image collecting device 5 is handled
Analysis, so that launch site can accurately be aimed at.It is preferred that positioning is set in unmanned plane 20 and/or ammunition emitter 10
Device, terminal control mechanism 30 can obtain 10 present position of unmanned plane 20 and/or ammunition emitter by locator at any time, so that
Can preferably it be controlled.
Claims (10)
1. a kind of ammunition emitter, it is fixed on unmanned aerial vehicle platform, and the ammunition emitter includes installing plate, institute
Upper the setting trigger mechanism and cartridge of installing plate are stated, the cartridge is used to load ammunition, and the trigger mechanism is used to control
Launch ammunition；It is characterized in that：Side of the installing plate away from cartridge is in angle by a bindiny mechanism and unmanned aerial vehicle platform
Degree connection, and the angle between the installing plate and the unmanned aerial vehicle platform is less than or equal to 90 °.
2. ammunition emitter as claimed in claim 1, it is characterised in that：The bindiny mechanism is section sky triangular in shape
Heart framework, the angle between the installing plate and the unmanned aerial vehicle platform are fixed.
3. ammunition emitter as claimed in claim 2, it is characterised in that：Between the installing plate and the unmanned aerial vehicle platform
Angle be 15-70 °.
4. ammunition emitter as claimed in claim 2, it is characterised in that：The trigger mechanism is arranged at the bindiny mechanism
It is interior.
5. ammunition emitter as claimed in claim 1, it is characterised in that：The bindiny mechanism includes the first of shaft connection
Swinging mounting and the second swinging mounting, first swinging mounting are fixedly connected with unmanned aerial vehicle platform, second swinging mounting
It is fixedly connected with installing plate, the angle between the installing plate and the unmanned aerial vehicle platform adjusts.
6. ammunition emitter as claimed in claim 1, it is characterised in that：The cartridge is hung in institute by suspending assembly
State on installing plate.
7. ammunition emitter as claimed in claim 6, it is characterised in that：The suspending assembly includes clip.
8. such as the ammunition emitter described in claim any one of 1-7, it is characterised in that：The installing plate is equipped with image
Harvester.
A kind of 9. ammunition emission system, it is characterised in that：Including ammunition emitter as described in claim 1, unmanned plane
And terminal control mechanism, the terminal control mechanism are connected with the ammunition emitter, UAV Communication.
10. ammunition emission system as claimed in claim 9, it is characterised in that：When on the installing plate of the ammunition emitter
During equipped with image collecting device, the terminal control mechanism includes an image processing unit.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711453960.3A CN108016618A (en) | 2017-12-28 | 2017-12-28 | A kind of ammunition emitter and system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711453960.3A CN108016618A (en) | 2017-12-28 | 2017-12-28 | A kind of ammunition emitter and system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108016618A true CN108016618A (en) | 2018-05-11 |
Family
ID=62072181
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201711453960.3A Pending CN108016618A (en) | 2017-12-28 | 2017-12-28 | A kind of ammunition emitter and system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108016618A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108775837A (en) * | 2018-06-08 | 2018-11-09 | 中国人民解放军济南军区72465部队 | It is loaded percussion system based on the matched collection of intelligent image |
| CN112631156A (en) * | 2020-11-09 | 2021-04-09 | 西安昆仑工业（集团）有限责任公司 | Ammunition firing control circuit |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104027909A (en) * | 2014-06-11 | 2014-09-10 | 江苏数字鹰科技发展有限公司 | Police fire-fighting unmanned aerial vehicle for high-rise building |
| CN104590562A (en) * | 2015-02-12 | 2015-05-06 | 马鞍山市赛迪智能科技有限公司 | Anti-collision fixed-point unmanned aerial vehicle for fire control |
| US20160370136A1 (en) * | 2013-11-07 | 2016-12-22 | Bae Systems Bofors Ab | Management system and method for sorting mixed ammunition types |
| CN206007850U (en) * | 2016-06-24 | 2017-03-15 | 河南沃野智能科技有限公司 | Air-to-surface missile fire extinguisher |
| CN206297734U (en) * | 2016-12-20 | 2017-07-04 | 北方天途航空技术发展（北京）有限公司 | The hanging structure and unmanned plane and fire-extinguishing of a kind of fire extinguisher bomb launching tube |
| CN107444641A (en) * | 2017-08-16 | 2017-12-08 | 广东容祺智能科技有限公司 | A kind of launched by airplane system with vision collimation |
| CN208102352U (en) * | 2017-12-28 | 2018-11-16 | 深圳城际快机科技有限公司 | A kind of ammunition emitter and system |
-
2017
- 2017-12-28 CN CN201711453960.3A patent/CN108016618A/en active Pending
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20160370136A1 (en) * | 2013-11-07 | 2016-12-22 | Bae Systems Bofors Ab | Management system and method for sorting mixed ammunition types |
| CN104027909A (en) * | 2014-06-11 | 2014-09-10 | 江苏数字鹰科技发展有限公司 | Police fire-fighting unmanned aerial vehicle for high-rise building |
| CN104590562A (en) * | 2015-02-12 | 2015-05-06 | 马鞍山市赛迪智能科技有限公司 | Anti-collision fixed-point unmanned aerial vehicle for fire control |
| CN206007850U (en) * | 2016-06-24 | 2017-03-15 | 河南沃野智能科技有限公司 | Air-to-surface missile fire extinguisher |
| CN206297734U (en) * | 2016-12-20 | 2017-07-04 | 北方天途航空技术发展（北京）有限公司 | The hanging structure and unmanned plane and fire-extinguishing of a kind of fire extinguisher bomb launching tube |
| CN107444641A (en) * | 2017-08-16 | 2017-12-08 | 广东容祺智能科技有限公司 | A kind of launched by airplane system with vision collimation |
| CN208102352U (en) * | 2017-12-28 | 2018-11-16 | 深圳城际快机科技有限公司 | A kind of ammunition emitter and system |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108775837A (en) * | 2018-06-08 | 2018-11-09 | 中国人民解放军济南军区72465部队 | It is loaded percussion system based on the matched collection of intelligent image |
| CN108775837B (en) * | 2018-06-08 | 2019-07-16 | 中国人民解放军济南军区72465部队 | It is loaded percussion system based on the matched collection of intelligent image |
| CN112631156A (en) * | 2020-11-09 | 2021-04-09 | 西安昆仑工业（集团）有限责任公司 | Ammunition firing control circuit |
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