CN103471472B - A kind ofly launch the aerial anti-terrorism device that microrocket advances extraordinary bullet - Google Patents
A kind ofly launch the aerial anti-terrorism device that microrocket advances extraordinary bullet Download PDFInfo
- Publication number
- CN103471472B CN103471472B CN201310386970.5A CN201310386970A CN103471472B CN 103471472 B CN103471472 B CN 103471472B CN 201310386970 A CN201310386970 A CN 201310386970A CN 103471472 B CN103471472 B CN 103471472B
- Authority
- CN
- China
- Prior art keywords
- bullet
- microrocket
- control unit
- extraordinary
- bomb body
- 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.)
- Active
Links
Abstract
Launch the aerial anti-terrorism device that microrocket advances extraordinary bullet, comprise rotor flying applicator platform, control system (Airborne Control Unit, information transceiver, ground observing and controlling device), task system (equipment turntable, video camera, emitter, miniature extraordinary bullet); Miniature extraordinary bullet comprises bullet lid, middle bomb body (dacryagogue or screening smoke are housed), rear bomb body (be equipped with and drag photo etching) and microrocket and advances section (solid propellant is housed); Rotor flying applicator platform arrives in inaccessible criminal's environment by plane, the equipment turntable run-home region can rotated by control task system both direction, when ground handling operator sends execution instruction by object observing ambient conditions, microrocket starts the miniature extraordinary bullet of promotion along aiming at route flight to target area, dacryagogue (or screening smoke) detonation, to implement terrified offender's deterrence and to assist attack function.
Description
Technical field
The present invention relates to a kind of police special equipment, refer in particular to and a kind ofly launch the aerial anti-terrorism device that microrocket advances extraordinary bullet, it belongs to the aerial work system terrified offender being played to deterrent effect, belongs to public security equipment field.
Background technology
In order to play deterrence and auxiliary attack function for the terrified offender in inaccessible environment,
As being hidden in terrified offender in high building, in courtyard wall, in cavern, especially gun, the inaccessible terrified offender of explosive is held, or offender's abduction has hostage and is not easy to the situation of shooting attack, the army of therefore public security, People's Armed Police and execution anti-terrorism task, need a kind of can close to terrified offender's environment, deterrence and auxiliary attack function can be played to terrified offender again, be convenient to catch the effective tool of terrified offender.
For above-mentioned situation, the present invention proposes and develops a kind of can launch close to terrified offender's environment (like flying face high-rise window, fly into overhead in institute, cavern) the aerial extraordinary anti-terrorism device that the auxiliary attack such as miniature tear bombnoun, smoke shell equips from aerial.Meanwhile, the present invention proposes applicable aerial unmanned flight's platform, convenient operation and can accurately run-home task system, play the miniature bullet of extraordinary effect.
Summary of the invention
The invention provides and a kind ofly launch the aerial anti-terrorism device that microrocket advances extraordinary bullet, it can realize arriving in inaccessible criminal's environment by plane, terrified offender's remote-transmitter is had to the special device of deterrence and auxiliary attack function.
The present invention adopts following technical scheme: a kind ofly launch the aerial anti-terrorism device that microrocket advances extraordinary bullet, comprise rotor flying applicator platform, control system and be installed on the task system of rotor craft platform lower, described control system comprises Airborne Control Unit, information transceiver and ground observing and controlling device, described Airborne Control Unit and information transceiver are installed in described rotor craft platform body, described ground observing and controlling device is undertaken communicating by radio and information transceiver and transmits, described task system comprises equipment turntable, video camera, emitter and miniature extraordinary bullet, described equipment turntable is connected with described rotor flying applicator platform, described video camera and emitter are connected to described equipment turntable.
Described equipment turntable includes and horizontally rotates electric steering engine, horizontal stand, pitch rotation electric steering engine and tilt mount, describedly horizontally rotate electric steering engine and be connected with rotor craft platform body, its rotation is controlled by the electric wire connected with described Airborne Control Unit by Airborne Control Unit, described pitch rotation electric steering engine is arranged on described horizontal stand, and be connected with tilt mount, its rotation is also controlled by the electric wire connected with described Airborne Control Unit by Airborne Control Unit, described video camera and emitter are all connected with described tilt mount, described camera lens axis and emitter tubular axis line arrange and are on same level line, described video camera controls it by ground observing and controlling device by information transceiver and Airborne Control Unit and makes level and pitch rotation.
The transmitting tube bearing that described emitter comprises transmitting tube and is connected with it, described transmitting tube bearing and tilt mount are connected, when executing the task, in described transmitting tube, miniature extraordinary bullet is installed, described miniature extraordinary bullet comprises bullet lid, middle bomb body, rear bomb body and microrocket advance section, described bullet lid and middle bomb body are by resin adhesion, described middle bomb body is connected with rear bomb body by screw thread, described rear bomb body advances section to be connected by screw thread and microrocket, described middle bomb body is in-built puts dacryagogue or screening smoke, in described rear bomb body, device drags photo etching, described microrocket advances device solid propellant in section, ignition wire is inserted with in described solid propellant, the other end of described ignition wire is connected with Airborne Control Unit, when described Airborne Control Unit by information transceiver receive that ground observing and controlling device sends execute the task instruction time, starting ignition electric wire switch, the miniature extraordinary bomb body of microrocket Work Promote is along aiming at route flight to target area, behind target approach region, bullet lid comes off, described dacryagogue or screening smoke detonation produce the smog that enough prestige are attacked.
The present invention has following beneficial effect:
(1) anti-terrorism device of the present invention can realize taking unmanned rotary wing aircraft as platform, and maneuverability also can hover, and can arrive in environment residing for inaccessible terrified offender by plane;
(2) the extraordinary bullet of anti-terrorism device of the present invention is using microrocket as propulsion plant, recoilless, can remote-transmitter, can from ground observation to terrified offender's image by aerial video camera, accurate run-home is launched, and avoids ground operational staff to be subject to terrified offender injury;
(3) the extraordinary bullet of anti-terrorism device of the present invention tear-gas or smog and drag light action, both can play deterrence and containment effect to terrified offender, and be convenient to catch, avoid again hostage and offender to be subject to material injury.
Accompanying drawing explanation
Fig. 1 is the system schematic that transmitting microrocket of the present invention advances the aerial anti-terrorism device of extraordinary bullet.
Fig. 2 is the structural representation of the task system of aerial anti-terrorism device of the present invention.
Fig. 3 is the control structure block diagram that transmitting microrocket of the present invention advances the aerial anti-terrorism device of extraordinary bullet.
Fig. 4 is that the microrocket of aerial anti-terrorism device of the present invention advances extraordinary bullet outline drawing.
Fig. 5 is that the microrocket of aerial anti-terrorism device of the present invention advances extraordinary bullet interior arrangement figure.
Fig. 6 is the action effect figure that the transmitting microrocket of aerial anti-terrorism device of the present invention advances extraordinary bullet.
Fig. 7 is the aerial work figure that transmitting microrocket of the present invention advances the aerial anti-terrorism device of extraordinary bullet.
Wherein:
1-rotor flying applicator platform; 2-task system; 3-Airborne Control Unit; 4-information transceiver; 5-ground observing and controlling device; 6-horizontally rotates electric steering engine; 7-horizontal stand; 8-pitch rotation electric steering engine; 9-tilt mount; 10-video camera; 11-transmitting tube; 12-transmitting tube bearing; 13-bullet lid; Bomb body in 14-; Bomb body after 15; 16-microrocket advances section; 17-dacryagogue or screening smoke; 18-drags photo etching; 19-solid propellant; 20-ignition wire; The miniature extraordinary bullet of 21-.
Detailed description of the invention
Please refer to shown in Fig. 1, the present invention launches microrocket and advances the rotor flying applicator platform 1 of the aerial anti-terrorism device of extraordinary bullet to be the unmanned multi-rotor aerocraft of microminiature (as six rotor unmanned aircrafts), is mainly used in carrying anti-terrorism equipment and performs airflight task.Unmanned multi-rotor aerocraft adopts brushless motor and screw to be used as power device, and the composite manufacture of rotor craft platform body, Airborne Control Unit and information transceiver are arranged in rotor craft platform body.Task system 2 is arranged on the bottom of rotor flying applicator platform 1, makes task system 2 have enough spaces and changes attitude and perform launch mission.Ground observing and controlling device 5, carry out communicating with the information transceiver 4 on rotor flying applicator platform 1 by radio and transmit, ground observing and controlling device 5 can observe the video image of video camera Real-time Obtaining on rotor flying applicator platform 1; Rotor flying applicator platform 1 can fly close to target environment, and can accurately hover over aerial, when finding run-home location-appropriate (as the window that aims at the mark), sending instruction, launch miniature extraordinary bullet 21 by ground observing and controlling device 5.
Please refer to shown in Fig. 2, the task system 2 in the present invention's aerial anti-terrorism device comprises equipment turntable, video camera 10, emitter and miniature extraordinary bullet; Described equipment turntable includes and horizontally rotates electric steering engine 6, horizontal stand 7, pitch rotation electric steering engine 8 and tilt mount 9; Horizontally rotate electric steering engine 6 to be connected with rotor craft platform body, horizontal stand 7 with horizontally rotate electric steering engine rotating shaft and be connected, horizontally rotate electric steering engine 6 and can handle horizontal stand 7 and do to horizontally rotate; Pitch rotation electric steering engine 8 is arranged on horizontal stand 7, tilt mount 9 one end and horizontal stand 7 chain connection, and tilt mount 9 other end is connected with the rotating shaft of pitch rotation electric steering engine, and pitch rotation electric steering engine 8 can be handled tilt mount 9 and make pitch rotation; Video camera 10 and emitter are all fixed on the bottom of tilt mount 9, and in the present invention, camera lens axis and emitter tubular axis line arrange and be on same level line; When horizontal stand 7 rotates with tilt mount 9, video camera and emitter rotate simultaneously.The transmitting tube bearing 12 that emitter of the present invention comprises transmitting tube 11 and is connected with it.
Please refer to shown in Fig. 3, it is the control structure block diagram that transmitting microrocket of the present invention advances the aerial anti-terrorism device of extraordinary bullet.Control system is one of key technology of the present invention, comprises air craft carried part and above ground portion, and its core component is Airborne Control Unit.Airborne Control Unit is the controller controlling the flight of rotor flying applicator platform, is also the controller that task system performs; Airborne Control Unit comprises mini inertial sensor (gyro, accelerometer), micro pressure altimeter, satellite navigation receiver, micro-process computer and control software design; One group of passage of Airborne Control Unit is connected with the motor electronic speed regulator of rotor flying applicator platform, controls the attitude stabilization of rotor flying applicator platform and flies by instruction track (remote control or predetermined paths); Another group passage of Airborne Control Unit is connected with information transceiver, the state of flight of rotor flying applicator platform is transferred to ground observing and controlling device by information transceiver, is accepted the telecommand (comprise flight directive, instruction of executing the task) of ground observing and controlling device simultaneously by information transceiver; Another group of passage of Airborne Control Unit is connected with task system, respectively with electric wire with horizontally rotate electric steering engine, pitch rotation electric steering engine, video camera play ignition wire with miniature special type and be connected; Video camera is connected with information transceiver by cable, and the video image information of picked-up is transferred to ground observing and controlling device by information transceiver; Ground observing and controlling device has video image display, can observe the target environment video image of Airborne camera picked-up, when ground handling operator judges the scopodromic appropriate location of task system equipment turntable, and can operation issue button; When Airborne Control Unit receives the telecommand of the extraordinary bullet of transmitting of ground observing and controlling device, Airborne Control Unit starting ignition electric wire switch, launches miniature extraordinary bullet.
Please refer to shown in Fig. 4 and Fig. 5, it is the microrocket propelling extraordinary bullet outline drawing of aerial anti-terrorism device of the present invention.Miniature extraordinary bullet 21 advances section 16 and internal charge to form by bullet lid 13, middle bomb body 14, rear bomb body 15, microrocket.The housing construction of miniature extraordinary bullet is processed into by alloy aluminum, and bullet lid 13 is taper, and middle bomb body 14 is all cylindrical shape with rear bomb body 15, and microrocket advances section 16 front portion to be divided into cylindrical shape, and its rear section is horn mouth taper; Bullet lid 13 and middle bomb body 14 are with resin bonding, and middle bomb body 14 is connected by screw thread with rear bomb body 15, and rear bomb body 15 and microrocket advance section 16 to be connected by screw thread; Bullet lid 13 and device dacryagogue or screening smoke 17 in middle bomb body 14, in rear bomb body 15, device drags photo etching 18, and microrocket advances device solid propellant 19 in section 16; Be inserted with ignition wire 20 in solid propellant 19, the other end of ignition wire 20 is connected with Airborne Control Unit 3; When Airborne Control Unit 3 starting ignition electric wire switch, light solid propellant 19, the reaction of microrocket jet flow promotes miniature extraordinary bullet 21 and advances along transmitting tube 11 direction.
Please refer to shown in Fig. 6, it is the action effect figure that the transmitting microrocket of aerial anti-terrorism device of the present invention advances extraordinary bullet.When microrocket advances the solid propellant 19 in section 16 to light, miniature extraordinary bullet 21 target approach district; Microrocket advances the burning solid propellant of section front end to light very soon and drags photo etching 18 in rear bomb body 15, drags photo etching 18 also along with spraying backward; Drag photo etching 18 jet flow and send long dazzling light (especially in darker indoor), deterrent effect is risen to terrified offender; Be hit by a bullet dacryagogue in body or screening smoke are lighted in the front end that photo etching is dragged in burning simultaneously, and the medicament in middle bomb body fires, and washes bullet lid very soon open, and dacryagogue or screening smoke are diffused in target area rapidly; The effect of dacryagogue or screening smoke will make terrified offender lose the hazardous act abilities such as shooting, and outdoor police can rush in indoor implementation and arrest terrified offender.
Please refer to shown in Fig. 7, it is the aerial work situation that transmitting microrocket of the present invention advances the aerial anti-terrorism device of extraordinary bullet.Aerial anti-terrorism device can be arrived in by plane near terrified offender region, and ground handling operator can, by observing directly terrified offender's field condition, implement to launch Special micro bullet.
The above is only the preferred embodiment of the present invention, it should be pointed out that for those skilled in the art, can also make some improvement under the premise without departing from the principles of the invention, and these improvement also should be considered as protection scope of the present invention.
Claims (1)
1. launch the aerial anti-terrorism device that microrocket advances extraordinary bullet for one kind, comprise rotor flying applicator platform (1), control system and be installed on the task system (2) of rotor flying applicator platform (1) bottom, it is characterized in that: described control system comprises Airborne Control Unit (3), information transceiver (4) and ground observing and controlling device (5), described Airborne Control Unit (3) and information transceiver (4) are installed in described rotor craft platform body, described ground observing and controlling device (5) is carried out communicating with information transceiver (4) by radio and is transmitted, described task system (2) comprises equipment turntable, video camera (10), emitter and miniature extraordinary bullet (21), described equipment turntable is connected with described rotor flying applicator platform (1), described video camera (10) and emitter are connected to described equipment turntable, described equipment turntable includes and horizontally rotates electric steering engine (6), horizontal stand (7), pitch rotation electric steering engine (8) and tilt mount (9), describedly horizontally rotate electric steering engine (6) and be connected with rotor craft platform body, its rotation is controlled by the electric wire connected with described Airborne Control Unit (3) by Airborne Control Unit (3), described pitch rotation electric steering engine (8) is arranged on described horizontal stand (7), and be connected with tilt mount (9), its rotation is also controlled by the electric wire connected with described Airborne Control Unit (3) by Airborne Control Unit (3), described video camera (10) and emitter are all connected with described tilt mount (9), described camera lens axis and emitter tubular axis line are arranged in the same horizontal line, described video camera (10) controls it by ground observing and controlling device (5) by information transceiver (4) and Airborne Control Unit (3) and makes level and pitch rotation, the transmitting tube bearing (12) that described emitter comprises transmitting tube (11) and is connected with it, described transmitting tube bearing (12) and tilt mount (9) are connected, when executing the task, in described transmitting tube (11), miniature extraordinary bullet (21) is installed, described miniature extraordinary bullet (21) comprises bullet lid (13), middle bomb body (14), rear bomb body (15) and microrocket advance section (16), described bullet lid (13) and middle bomb body (14) are by resin adhesion, described middle bomb body (14) is connected with rear bomb body (15) by screw thread, described rear bomb body (15) advances section (16) to be connected by screw thread and microrocket, the interior device dacryagogue of described middle bomb body (14) or screening smoke (17), the interior device of described rear bomb body (15) drags photo etching (18), described microrocket advances section (16) interior device solid propellant (19), ignition wire (20) is inserted with in described solid propellant (19), the other end of described ignition wire (20) is connected with Airborne Control Unit (3), when described Airborne Control Unit (3) by information transceiver (4) receive that ground observing and controlling device (5) sends execute the task instruction time, starting ignition electric wire switch, the miniature extraordinary bomb body of microrocket Work Promote is along aiming at route flight to target area, behind target approach region, bullet lid comes off, described dacryagogue or screening smoke detonation produce the smog that enough prestige are attacked.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310386970.5A CN103471472B (en) | 2013-08-30 | 2013-08-30 | A kind ofly launch the aerial anti-terrorism device that microrocket advances extraordinary bullet |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310386970.5A CN103471472B (en) | 2013-08-30 | 2013-08-30 | A kind ofly launch the aerial anti-terrorism device that microrocket advances extraordinary bullet |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN103471472A CN103471472A (en) | 2013-12-25 |
| CN103471472B true CN103471472B (en) | 2015-09-16 |
Family
ID=49796426
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201310386970.5A Active CN103471472B (en) | 2013-08-30 | 2013-08-30 | A kind ofly launch the aerial anti-terrorism device that microrocket advances extraordinary bullet |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN103471472B (en) |
Families Citing this family (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110199239A (en) * | 2016-11-28 | 2019-09-03 | M·A·格里芬 | Remote control equipment and system |
| CN107084643B (en) * | 2017-03-28 | 2019-03-29 | 东南大学 | A kind of holder transmitter and its automatic identification and sighting system |
| US11143479B2 (en) * | 2018-06-12 | 2021-10-12 | Lei He | Artificial and intelligent anti-terrorism device for stopping ongoing crime |
| CN110270020B (en) * | 2019-07-08 | 2021-02-19 | 西安航天化学动力有限公司 | Recoilless window breaker mounted on unmanned aerial vehicle |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201235938Y (en) * | 2008-07-04 | 2009-05-13 | 中国船舶重工集团公司第七一七研究所 | Machine-carried visible light image apparatus |
| CN202392374U (en) * | 2011-09-09 | 2012-08-22 | 深圳市大疆创新科技有限公司 | Gyroscopic dynamic self-balancing pan/tilt/zoom (PTZ) |
| CN202765289U (en) * | 2012-07-30 | 2013-03-06 | 江阴市公安局 | Multi-rotor police unmanned aerial vehicle |
| CN202765293U (en) * | 2012-09-21 | 2013-03-06 | 刘鹏 | Rotor craft capable of carrying firearms |
| RU130953U1 (en) * | 2012-12-04 | 2013-08-10 | Дмитрий Витальевич Табачников | UNMANNED AIRCRAFT (OPTIONS) |
Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR20050071844A (en) * | 2004-01-05 | 2005-07-08 | 김병선 | Mechanism of rotary wing type for unmanned aerial vehicle |
-
2013
- 2013-08-30 CN CN201310386970.5A patent/CN103471472B/en active Active
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201235938Y (en) * | 2008-07-04 | 2009-05-13 | 中国船舶重工集团公司第七一七研究所 | Machine-carried visible light image apparatus |
| CN202392374U (en) * | 2011-09-09 | 2012-08-22 | 深圳市大疆创新科技有限公司 | Gyroscopic dynamic self-balancing pan/tilt/zoom (PTZ) |
| CN202765289U (en) * | 2012-07-30 | 2013-03-06 | 江阴市公安局 | Multi-rotor police unmanned aerial vehicle |
| CN202765293U (en) * | 2012-09-21 | 2013-03-06 | 刘鹏 | Rotor craft capable of carrying firearms |
| RU130953U1 (en) * | 2012-12-04 | 2013-08-10 | Дмитрий Витальевич Табачников | UNMANNED AIRCRAFT (OPTIONS) |
Also Published As
| Publication number | Publication date |
|---|---|
| CN103471472A (en) | 2013-12-25 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| JP6921147B2 (en) | Multimode unmanned aerial vehicle | |
| JP7185033B2 (en) | Close Proximity Countermeasures for Neutralization of Target Aircraft | |
| JP2020519843A (en) | Unmanned aerial vehicle (UAVS) interception and counterattack system and method | |
| US20160293015A1 (en) | Projectile launched uav reconnaissance system and method | |
| CN111770881A (en) | Remotely controllable aviation ordnance | |
| US20120043411A1 (en) | Unmanned aerial vehicle system | |
| US20150142210A1 (en) | Surveillance system | |
| CN103471472B (en) | A kind ofly launch the aerial anti-terrorism device that microrocket advances extraordinary bullet | |
| KR20080037434A (en) | Flight machine with camera for suicidal explosion, and apparatus for controlling it | |
| CN108619641B (en) | Fire extinguishing system and method for vertical emission guidance fire extinguishing body | |
| JP2644700B2 (en) | How to guide fire bombs | |
| AU2020201173B2 (en) | Multimode unmanned aerial vehicle | |
| CN207741641U (en) | A kind of big gun penetrates unmanned plane | |
| CN110861776A (en) | Unmanned aerial vehicle and system for throwing tear-gas shells and method for throwing tear-gas shells in human-in-loop mode | |
| CN108036680A (en) | A kind of big gun penetrates unmanned plane | |
| WO2023238834A1 (en) | Fall trajectory control system |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant |