CN208102352U - A kind of ammunition emitter and system - Google Patents

A kind of ammunition emitter and system Download PDF

Info

Publication number
CN208102352U
CN208102352U CN201721886419.7U CN201721886419U CN208102352U CN 208102352 U CN208102352 U CN 208102352U CN 201721886419 U CN201721886419 U CN 201721886419U CN 208102352 U CN208102352 U CN 208102352U
Authority
CN
China
Prior art keywords
ammunition
mounting 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.)
Expired - Fee Related
Application number
CN201721886419.7U
Other languages
Chinese (zh)
Inventor
刘永军
廖俊杰
陈冠勇
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.)
Shenzhen Intercity Express Technology Co Ltd
Original Assignee
Shenzhen Intercity Express Technology Co Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Shenzhen Intercity Express Technology Co Ltd filed Critical Shenzhen Intercity Express Technology Co Ltd
Priority to CN201721886419.7U priority Critical patent/CN208102352U/en
Application granted granted Critical
Publication of CN208102352U publication Critical patent/CN208102352U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Landscapes

  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)

Abstract

The utility model relates to air vehicle technique field, a kind of ammunition emitter and system are provided.A kind of ammunition emitter, including it is fixed on unmanned aerial vehicle platform, the ammunition emitter includes mounting plate, the upper setting trigger mechanism and cartridge of the mounting plate, and the cartridge is for loading ammunition, and the trigger mechanism is for controlling transmitting ammunition;Side of the mounting plate far from cartridge passes through a bindiny mechanism and the angled connection of unmanned aerial vehicle platform.The ammunition emitter can be stablized, accurately emit ammunition.The utility model also provides a kind of ammunition emission system, including above-mentioned ammunition emitter.

Description

A kind of ammunition emitter and system
Technical field
The utility model relates to air vehicle technique field more particularly to a kind of ammunition emitter and systems.
Background technique
Increasingly mature with unmanned air vehicle technique, unmanned plane is widely used in the fields 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 needs to keep order using ammunitions such as tear bombnoun, pinking bullet, aerosol bombs in some special circumstances.Currently, being based on nobody The ammunition of machine platform is mostly directly anchored to below unmanned plane, haves the shortcomings that projection stability, accuracy is not high.
Utility model content
The purpose of this utility model is to provide a kind of ammunition emitter and systems, can stablize, accurately emit ammunition.
In order to solve the above technical problems, utility model uses technical solution as described below.A kind of ammunition emitter, packet It includes it to be fixed on unmanned aerial vehicle platform, the ammunition emitter includes mounting plate, the upper setting transmitting of the mounting plate Mechanism and cartridge, the cartridge is for loading ammunition, and the trigger mechanism is for controlling transmitting ammunition;The mounting plate is remote From the side of cartridge by a bindiny mechanism and the angled connection of unmanned aerial vehicle platform, and the mounting plate and the unmanned plane are flat Angle between platform is less than or equal to 90 °.
Preferably, the bindiny mechanism is section hollow frame triangular in shape, and the mounting plate and the unmanned plane are flat Angle between platform is fixed.
Preferably, the angle between the mounting plate and the unmanned aerial vehicle platform is 15-70 °.
Preferably, the trigger mechanism is set in the bindiny mechanism.
Preferably, the bindiny mechanism include shaft connection the first rotating bracket and the second rotating bracket, described first Rotating bracket is fixedly connected with unmanned aerial vehicle platform, and second rotating bracket is fixedly connected with mounting plate, the mounting plate and institute The angle stated between unmanned aerial vehicle platform is adjustable.
Preferably, the cartridge is hung on the mounting plate by suspending assembly.
Preferably, the suspending assembly includes clip.
Preferably, the mounting plate is equipped with image collecting device.
The utility model also provides a kind of ammunition emission system, including above-mentioned ammunition emitter, unmanned plane and terminal Control device, the terminal control mechanism are connect with the ammunition emitter, UAV Communication.
Preferably, when the mounting plate of the ammunition emitter is equipped with image collecting device, the terminal control dress It sets including an image processing unit.
The beneficial effects of the utility model are:
The utility model provides a kind of ammunition emitter, and mounting plate is in unmanned aerial vehicle platform by a bindiny mechanism Angle connection can effectively improve the stability of ammunition transmitting firstly, being attached by bindiny mechanism;Secondly, mounting plate and nothing It is angled between man-machine platform to be fixedly connected, it is able to achieve certain launch angle, can guarantee the stability of ammunition transmitting, moreover it is possible to mention The accuracy of high ammunition transmitting.
The utility model additionally provides a kind of ammunition emitter, including above-mentioned ammunition emitter, therefore has bullet The stability and the higher advantage of accuracy of medicine transmitting;In addition, can remotely control the transmitting of ammunition using terminal control mechanism.
Detailed description of the invention
Fig. 1 is the schematic perspective view of ammunition emitter provided in the utility model.
Fig. 2 is the schematic front view of ammunition emitter provided in some preferred embodiments of the utility model.
Fig. 3 is the structure block diagram of ammunition emission system provided in the utility model.
Specific embodiment
To make those skilled in the art that the purposes, technical schemes and advantages of utility model be more clearly understood, Utility model is further elaborated below in conjunction with drawings and examples.
First embodiment
As shown in Figure 1, a kind of ammunition emitter, is fixed on unmanned aerial vehicle platform, the ammunition emitter Including mounting plate 2, the upper setting trigger mechanism 3 and cartridge 7 of the mounting plate 2, the cartridge 7 is for loading ammunition, institute State trigger mechanism 3 for control transmitting ammunition;Side of the mounting plate 2 far from cartridge 7 passes through a bindiny mechanism 1 and nobody The angled connection of machine platform, and the angle between the mounting 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 utility model, mounting plate 2 are in unmanned aerial vehicle platform by a bindiny mechanism 1 Angle is fixedly connected, firstly, being attached by bindiny mechanism 1, can effectively improve the stability of ammunition transmitting, it is possible to understand that nothing When man-machine flight in the sky, stability is poor, can provide relatively stable emission state using bindiny mechanism 1.Secondly, mounting plate It is angled between 2 and unmanned aerial vehicle platform to be fixedly connected, it is able to achieve certain launch angle, can guarantee the stability of ammunition transmitting, The accuracy of ammunition transmitting can also be improved.It is appreciated that inclining if ammunition horizontal emission from the distance ratio to land is emitted to The distance tiltedly emitted, and the resistance being subject to is bigger, to influence the stability and accuracy of ammunition transmitting;And if in order to It realizes inclination transmitting, is tilted to control unmanned plane, can more influence the stability of ammunition transmitting instead.Therefore, pass through Bindiny mechanism 1 is set, can just to realize certain launch angle under smooth flight or resting state in unmanned plane.
In some embodiments, the angle between the mounting 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 connect with mounting plate 2, unmanned aerial vehicle platform respectively.In some preferred realities It applies in example, the bindiny mechanism 1 is hollow frame, and the trigger mechanism 3 is set in the bindiny mechanism 1, in this way can be to hair It penetrates mechanism 3 and forms certain protection, extend the service life of the ammunition emitter.Certainly, the trigger mechanism 3 can also be with It is directly arranged on mounting plate 2, specifically, the trigger mechanism 3 can be single-chip microcontroller.
Preferably, the angle between the mounting plate 2 and the unmanned aerial vehicle platform is 15-70 °, the 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 mounting plate 2 and the unmanned aerial vehicle platform It is adjustable.First rotating bracket 11 ' and second rotating bracket 12 ' of the bindiny mechanism 1 ' including shaft connection, described first Rotating bracket 11 ' is fixedly connected with unmanned aerial vehicle platform, and second rotating bracket 12 ' is fixedly connected with mounting plate 2.So also It is that the second rotating bracket 12 ' can be rotated around the first rotating bracket 11 ', namely as shown in arrow R in figure, be rotated, thus It drives mounting plate 2 and cartridge 7 to be rotated, realizes certain launch angle, and launch angle is adjustable.Specifically, can Being adjusted by the way that steering engine is arranged.
Preferably, the cartridge 7 is hung on the mounting plate 2 by suspending assembly 4.Further, described hang Hanging component 4 includes clip, can fix cartridge 7 well using clip, and easy to disassemble is replaced.The clip includes Edge and the first clip 41 disposed in parallel in 2 vertical direction of mounting plate and the second clip 42, can load more ammunitions.It is preferred that Ground is detachably connected between first clip 41 and the second clip 42, specifically, can be first clip 41 and second Clip 42 is connected by a connecting plate 43, and first clip 41 and the second clip 42 are connected with connecting plate by screw It connects.
In some preferred embodiments, the mounting plate 2 is equipped with image collecting device 5, utilizes the image collector Setting 5 can be carried out aiming, increase the accuracy of transmitting, and described image acquisition device 5 can be camera etc..
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 ammunition emitter provided in first embodiment.The terminal control mechanism 30 It is communicated to connect with the ammunition emitter 10, unmanned plane 20.It is appreciated that the ammunition emitter 10 is mounted on unmanned plane On 20, the terminal control mechanism 30 can be the console positioned at ground, therefore may be implemented at a distance to 20 He of unmanned plane The control of ammunition emitter 10, to accurately emit ammunition.It is appreciated that when the mounting plate of the ammunition emitter 10 When angle between 2 and unmanned aerial vehicle platform is adjustable, the terminal control mechanism 30 can the long-range progress of control connecting mechanism 1 ' The adjustment of angle.
Further, when the mounting plate 2 of the ammunition emitter 10 is equipped with image collecting device 5, the end Holding control device 30 includes an image processing unit.Namely handled using 5 acquired images of image collecting device Analysis, so that launch site can accurately be aimed at.It is preferred that in unmanned plane 20 and/or the setting positioning of ammunition emitter 10 Device, terminal control mechanism 30 can obtain unmanned plane 20 and/or 10 present position of ammunition emitter by locator at any time, thus It can preferably be controlled.

Claims (10)

1. a kind of ammunition emitter, is fixed on unmanned aerial vehicle platform, the ammunition emitter includes mounting plate, institute The upper setting trigger mechanism and cartridge of mounting plate are stated, the cartridge is for loading ammunition, and the trigger mechanism is for controlling Emit ammunition;It is characterized in that:Side of the mounting plate far from cartridge is in angle by a bindiny mechanism and unmanned aerial vehicle platform Degree connection, and the angle between the mounting plate and the unmanned aerial vehicle platform is less than or equal to 90 °.
2. ammunition emitter as described in claim 1, it is characterised in that:The bindiny mechanism is section sky triangular in shape Heart framework, the angle between the mounting plate and the unmanned aerial vehicle platform are fixed.
3. ammunition emitter as claimed in claim 2, it is characterised in that:Between the mounting 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 set to the bindiny mechanism It is interior.
5. ammunition emitter as described in claim 1, it is characterised in that:The bindiny mechanism includes the first of shaft connection Rotating bracket and the second rotating bracket, first rotating bracket are fixedly connected with unmanned aerial vehicle platform, second rotating bracket It is fixedly connected with mounting plate, the angle between the mounting plate and the unmanned aerial vehicle platform is adjustable.
6. ammunition emitter as described in claim 1, it is characterised in that:The cartridge is hung by suspending assembly in institute It states on mounting plate.
7. ammunition emitter as claimed in claim 6, it is characterised in that:The suspending assembly includes clip.
8. the ammunition emitter as described in claim any one of 1-7, it is characterised in that:The mounting plate is equipped with image Acquisition device.
9. a kind of 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 connect with the ammunition emitter, UAV Communication.
10. ammunition emission system as claimed in claim 9, it is characterised in that:When on the mounting plate of the ammunition emitter When equipped with image collecting device, the terminal control mechanism includes an image processing unit.
CN201721886419.7U 2017-12-28 2017-12-28 A kind of ammunition emitter and system Expired - Fee Related CN208102352U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201721886419.7U CN208102352U (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
CN201721886419.7U CN208102352U (en) 2017-12-28 2017-12-28 A kind of ammunition emitter and system

Publications (1)

Publication Number Publication Date
CN208102352U true CN208102352U (en) 2018-11-16

Family

ID=64130305

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201721886419.7U Expired - Fee Related CN208102352U (en) 2017-12-28 2017-12-28 A kind of ammunition emitter and system

Country Status (1)

Country Link
CN (1) CN208102352U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108016618A (en) * 2017-12-28 2018-05-11 深圳城际快机科技有限公司 A kind of ammunition emitter and system

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108016618A (en) * 2017-12-28 2018-05-11 深圳城际快机科技有限公司 A kind of ammunition emitter and system

Similar Documents

Publication Publication Date Title
EP3837488B1 (en) Close proximity countermeasures for neutralizing target aerial vehicles
CN107054678B (en) A kind of vehicle-mounted anti-unmanned plane net bullet intercepting system
CN204822085U (en) Unmanned aerial vehicle with arrest ware
CN105573343A (en) Capture system based on unmanned aerial vehicle
CN107071364B (en) Anti-unmanned aerial vehicle device and method based on multi-camera tracking and positioning
CN208102352U (en) A kind of ammunition emitter and system
CN108016618A (en) A kind of ammunition emitter and system
CN108820214A (en) A kind of aircraft, which is examined, beats control emission system
CN203558208U (en) Rotor craft capable of carrying weapon delivery mechanism
CN113848992A (en) Target detection location and automatic shooting system based on unmanned aerial vehicle and armed beating robot
US20180004203A1 (en) Unmanned Aerial Vehicle Weapon System and Method of Operation
WO2017080109A1 (en) Intelligent unmanned aerial vehicle system for remotely detecting target on basis of infrared
CN104503458A (en) Micro individual combat unmanned plane system
CN208882113U (en) A kind of aircraft, which is examined, beats control emission system
CN208630855U (en) A kind of multi-rotor unmanned aerial vehicle with smog identification function
CN209521870U (en) A kind of air firing unmanned plane
RU2578524C2 (en) System for controlling integrated methods for combating small-sized unmanned aerial vehicles
CN208108918U (en) A kind of net gun apparatus based on unmanned aerial vehicle platform
CN205405272U (en) Unmanned aerial vehicle system of arresting
CN209521849U (en) A kind of airship formula unmanned plane
CN105539850A (en) Multi-angle air launching system based on aircraft
CN210882619U (en) Fire control unmanned aerial vehicle
CN112424067A (en) Flying body
CN208139937U (en) A kind of double hairnet gun apparatus based on unmanned aerial vehicle platform
CN113758368A (en) Novel laser simulation confrontation induction device

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: 20181116

Termination date: 20181228

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