CN206479091U - A kind of portable a variety of MISSILE LAUNCHING hunting gears - Google Patents
A kind of portable a variety of MISSILE LAUNCHING hunting gears Download PDFInfo
- Publication number
- CN206479091U CN206479091U CN201720069155.XU CN201720069155U CN206479091U CN 206479091 U CN206479091 U CN 206479091U CN 201720069155 U CN201720069155 U CN 201720069155U CN 206479091 U CN206479091 U CN 206479091U
- Authority
- CN
- China
- Prior art keywords
- movement articulator
- portable
- shaped
- missile
- variety
- 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
The utility model discloses the portable a variety of MISSILE LAUNCHING hunting gears of one kind, including tripod, rotation is supported by U-shaped arbitrary-movement articulator on tripod, U-shaped arbitrary-movement articulator is provided with pitching frame, pitching frame is horizontally supported at the top open part of U-shaped arbitrary-movement articulator, and with the free degree of the rotary-top along U-shaped arbitrary-movement articulator, the top of pitching frame is provided with MISSILE LAUNCHING module, lower section is provided with optronic tracker, U-shaped arbitrary-movement articulator connects provided with the motor for driving U-shaped arbitrary-movement articulator rotation and pitching frame pitching, optronic tracker with motor signal.The utility model can make all kinds of portable missile emission process it is highly efficient, light, automation, it is convenient to carry out dismounting assembling, the weight of each component is also undertaken within load in the normal of people, it is easy to teams and groups' march carrying, it can also be directly anchored on offroad vehicle, can also be applied widely on small sweeper, seagoing vessel.
Description
Technical field
The utility model is related to air defence missile lift-off technology field, and in particular to a kind of portable a variety of MISSILE LAUNCHINGs are servo-actuated
Device.
Background technology
At present, lightweight because portable missile has small volume, range is near, simple to operate, using flexible, is easy to take
The features such as band and hidden camouflage, the extensive use in army's Terminal defense short-range air-defense, but portable air defense missile artificial bone-head for shoulder
Shoulder in operation transmitting, quick-reaction capability is poor, and target acquisition is dumb, multiple target saturation attack dynamics is little, existing announcement
The portable duplex multiple missile launcher that patent CN203550783U is carried, there is artificial capture method target, manually adjusts orientation in it
Direction and pitch orientation, the shortcomings of response speed is slow, and different type guided missile can not be selected according to different destruction targets, enter
The autonomous networking operation of row.
Utility model content
The purpose of this utility model is to overcome above-mentioned the deficiencies in the prior art to make all kinds of portable missiles there is provided one kind
Emission process is efficient, light, automation portable a variety of MISSILE LAUNCHING hunting gears.
Rotation is supported by U-shaped servo-actuated on a kind of portable a variety of MISSILE LAUNCHING hunting gears, including tripod, tripod
Frame, U-shaped arbitrary-movement articulator is provided with pitching frame, and pitching frame is horizontally supported at the top open part of U-shaped arbitrary-movement articulator, and with along it is U-shaped with
The free degree of the rotary-top of moving frame, the top of pitching frame is provided with MISSILE LAUNCHING module, and lower section is provided with optronic tracker, it is U-shaped with
Moving frame is provided with the motor for driving U-shaped arbitrary-movement articulator rotation and pitching frame pitching, optronic tracker and motor signal phase
Connect.
It is used as further describing for above-mentioned technical proposal：
The U-shaped arbitrary-movement articulator is embedded in provided with the power module for being used to convert alternating current to direct current.
It is used as further describing for above-mentioned technical proposal：
The MISSILE LAUNCHING module includes guided missile installing plate, and guided missile installing plate is provided with the artificial percussion lock of simulation, ground
Power supply rotating device and STT missile device.
It is used as further describing for above-mentioned technical proposal：
The optronic tracker includes target pointing instrumentation and laser range finder.
It is used as further describing for above-mentioned technical proposal：
GPS positioning device is additionally provided with the U-shaped arbitrary-movement articulator.
It is used as further describing for above-mentioned technical proposal：
The tripod is focused on fixation kit including three supporting arm frames, one end ends of three supporting arm frames, Gu
Determine to be provided with rotary components in component, the bottom of U-shaped arbitrary-movement articulator is arranged on rotary components.
The utility model can make all kinds of portable missile emission process it is highly efficient, light, automation, facilitate and dismantled
Assembling, the weight of each component is also undertaken within load in the normal of people, is easy to teams and groups' march carrying, can also be directly anchored to get over
, can also be applied widely on small sweeper, seagoing vessel on wild car.
Brief description of the drawings
Fig. 1 is structural representation of the present utility model；
Fig. 2 is the structural representation of U-shaped arbitrary-movement articulator in the utility model；
Fig. 3 is the structural representation of tripod in the utility model.
Embodiment
A kind of portable a variety of MISSILE LAUNCHING hunting gears provided referring to Fig. 1, the utility model, including tripod 1, three
Rotation is supported by U-shaped arbitrary-movement articulator 2 on foot stool 1, and U-shaped arbitrary-movement articulator 2 is provided with pitching frame 3, and pitching frame 3 is horizontally supported at U-shaped servo-actuated
The top open part of frame 2, and with the free degree of the rotary-top along U-shaped arbitrary-movement articulator 2, the top of pitching frame 3 is sent out provided with guided missile
Module 4 is penetrated, lower section is provided with optronic tracker 5, referring to Fig. 2, U-shaped arbitrary-movement articulator 2 rotates and pitching provided with the U-shaped arbitrary-movement articulator 2 of driving
The motor 6 of the pitching of frame 3, optronic tracker 5 connects with the signal of motor 6.
Because the utility model is using building block system, modular, easy-to-assemble element structure, so being both easy to teams and groups
March is carried, and development rate is fast on the spot, can be installed again with vehicle-mounted, it might even be possible to installed on small sweeper.
In use, being launched using tripod 1, under the guide of optronic tracker 5, motor 6 drives U-shaped arbitrary-movement articulator 2
And pitching frame 3 is acted, can accurate and flexible both horizontally and vertically from motion tracking, seizure, lock onto target.(target is believed
Breath be converted into two axle control commands, realize two-axle interlocking, can in the horizontal direction 360 ° rotation, -10 ° in vertical direction~
65 ° of swings.Its kinematic accuracy can reach 2mrad.)
Even if ground goes to pot, when non-transformer is supplied, it can be rapidly converted to manually operated.According to coming to attack target according to sky
Snares of love such as " antiaircraft bodyguard ", which is provided, finds target bearing, the parameter such as speed, and (such as 10min) deploys equipment at the appointed time
Pre- frame, optronic tracker 5 starts the movement simultaneously in orientation and pitch orientation according to target designation data, intercepts and captures, tracks target.
After intercepting and capturing, tracking target, MISSILE LAUNCHING module 4 activates readied missile, firepower control necessary to measurement and calculating tackle target
Protocol processed.When target operational distance effective into guided missile, operator presses button, boost motor igniting.Guided missile is sent out
Second of attack can be started to same target by penetrating rear operator, or attack next target.
In the present embodiment, U-shaped arbitrary-movement articulator 2 is embedded in provided with the power module for being used to convert alternating current to direct current.Electricity
Source module includes direct current linear power supply, Switching Power Supply.During the short of electricity of outfield, can directly it be powered with mobile power station.
In the present embodiment, MISSILE LAUNCHING module 4 includes guided missile installing plate, and guided missile installing plate is provided with the artificial percussion dress of simulation
Put, ground power supply rotating device and STT missile device.Form a whole module, quick detachable, maintenance.It is whole by wire communication
End, realizes the information exchange with operational chain of command, includes the communication of data and voice.
In the present embodiment, optronic tracker 5 includes target pointing instrumentation and laser range finder.Target pointing instrumentation is infrared imaging
Instrument, be mainly used in it is round-the-clock round the clock between target is scanned for, aim at and tracked.
In the present embodiment, GPS positioning device is additionally provided with U-shaped arbitrary-movement articulator 2.It by two by being separated by a certain distance
What GPS and its location control instrument were constituted, for carrying out positioning and directing to whole device.
In the present embodiment, referring to Fig. 3, tripod 1 includes one end end of three supporting arm frames 11, three supporting arm frames 11
It is focused in fixation kit 12, fixation kit 12 being provided with rotary components 13, the bottom of U-shaped arbitrary-movement articulator 2 is arranged on rotary components
On 13.The rotation that U-shaped arbitrary-movement articulator horizontal direction can be allowed to carry out 360 °.
Described above is only preferred embodiment of the present utility model, and protection domain of the present utility model is not limited merely to
Above-described embodiment, all technical schemes belonged under the utility model thinking belong to protection domain of the present utility model.It should refer to
Go out, for those skilled in the art, some improvement under the premise of the utility model principle is not departed from and
Retouching, these improvements and modifications also should be regarded as protection domain of the present utility model.
Claims (6)
1. a kind of portable a variety of MISSILE LAUNCHING hunting gears, it is characterised in that：Including tripod, rotation is supported by tripod
U-shaped arbitrary-movement articulator, U-shaped arbitrary-movement articulator is provided with pitching frame, and pitching frame is horizontally supported at the top open part of U-shaped arbitrary-movement articulator, and has
Along the free degree of the rotary-top of U-shaped arbitrary-movement articulator, the top of pitching frame is provided with MISSILE LAUNCHING module, and lower section is provided with photoelectric tracking
Instrument, U-shaped arbitrary-movement articulator is provided with the motor for driving U-shaped arbitrary-movement articulator rotation and pitching frame pitching, optronic tracker and driving electricity
Machine signal connects.
2. the portable a variety of MISSILE LAUNCHING hunting gears of one kind according to claim 1, it is characterised in that：It is described it is U-shaped with
Moving frame is embedded in provided with the power module for being used to convert alternating current to direct current.
3. the portable a variety of MISSILE LAUNCHING hunting gears of one kind according to claim 1, it is characterised in that：The guided missile hair
Penetrating module includes guided missile installing plate, and guided missile installing plate is provided with the artificial percussion lock of simulation, ground power supply rotating device and guided missile
Controller.
4. the portable a variety of MISSILE LAUNCHING hunting gears of one kind according to claim 1, it is characterised in that：The photoelectricity with
Track instrument includes target pointing instrumentation and laser range finder.
5. the portable a variety of MISSILE LAUNCHING hunting gears of one kind according to claim 1, it is characterised in that：It is described it is U-shaped with
GPS positioning device is additionally provided with moving frame.
6. the portable a variety of MISSILE LAUNCHING hunting gears of one kind according to claim 1, it is characterised in that：The tripod
One end end including three supporting arm frames, three supporting arm frames is focused in fixation kit, fixation kit being provided with rotation group
Part, the bottom of U-shaped arbitrary-movement articulator is arranged on rotary components.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720069155.XU CN206479091U (en) | 2017-01-20 | 2017-01-20 | A kind of portable a variety of MISSILE LAUNCHING hunting gears |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720069155.XU CN206479091U (en) | 2017-01-20 | 2017-01-20 | A kind of portable a variety of MISSILE LAUNCHING hunting gears |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206479091U true CN206479091U (en) | 2017-09-08 |
Family
ID=59753626
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720069155.XU Active CN206479091U (en) | 2017-01-20 | 2017-01-20 | A kind of portable a variety of MISSILE LAUNCHING hunting gears |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206479091U (en) |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108548452A (en) * | 2018-04-28 | 2018-09-18 | 施新红 | A kind of novel optical transmission equipment |
| CN109595986A (en) * | 2018-12-13 | 2019-04-09 | 上海航天设备制造总厂有限公司 | A kind of missile launch test device |
| RU2708809C1 (en) * | 2019-02-14 | 2019-12-11 | Российская Федерация, от имени которой выступает ФОНД ПЕРСПЕКТИВНЫХ ИССЛЕДОВАНИЙ | Armament complex |
| CN110645831A (en) * | 2019-11-21 | 2020-01-03 | 广州皓想光学仪器有限公司 | Auxiliary sighting device for improving hitting precision of ground missile |
| CN110887405A (en) * | 2019-11-27 | 2020-03-17 | 贵州航天特种车有限责任公司 | Rocket projectile vehicle-mounted and ground integrated launching vehicle |
| CN111059960A (en) * | 2019-12-19 | 2020-04-24 | 中山市翔宇精密光电仪器有限公司 | Safe and stable's bipod for firearms |
| CN114166066A (en) * | 2022-01-17 | 2022-03-11 | 中国人民解放军军事科学院国防工程研究院工程防护研究所 | Assembled remote control shooting platform |
-
2017
- 2017-01-20 CN CN201720069155.XU patent/CN206479091U/en active Active
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108548452A (en) * | 2018-04-28 | 2018-09-18 | 施新红 | A kind of novel optical transmission equipment |
| CN109595986A (en) * | 2018-12-13 | 2019-04-09 | 上海航天设备制造总厂有限公司 | A kind of missile launch test device |
| RU2708809C1 (en) * | 2019-02-14 | 2019-12-11 | Российская Федерация, от имени которой выступает ФОНД ПЕРСПЕКТИВНЫХ ИССЛЕДОВАНИЙ | Armament complex |
| CN110645831A (en) * | 2019-11-21 | 2020-01-03 | 广州皓想光学仪器有限公司 | Auxiliary sighting device for improving hitting precision of ground missile |
| CN110887405A (en) * | 2019-11-27 | 2020-03-17 | 贵州航天特种车有限责任公司 | Rocket projectile vehicle-mounted and ground integrated launching vehicle |
| CN111059960A (en) * | 2019-12-19 | 2020-04-24 | 中山市翔宇精密光电仪器有限公司 | Safe and stable's bipod for firearms |
| CN114166066A (en) * | 2022-01-17 | 2022-03-11 | 中国人民解放军军事科学院国防工程研究院工程防护研究所 | Assembled remote control shooting platform |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN206479091U (en) | A kind of portable a variety of MISSILE LAUNCHING hunting gears | |
| CN106288964A (en) | A kind of anti-low slow bug system of defense | |
| CN105159318B (en) | Conservation culture monitoring device and system | |
| CN105204516B (en) | Ecological agriculture monitoring method, apparatus and system | |
| CN105559228A (en) | Intelligent riding helmet | |
| CN205015741U (en) | Companion flies unmanned aerial vehicle system of taking photo by plane and control cabinet and unmanned aerial vehicle thereof | |
| CN101866006A (en) | Rotary multi-sensor photoelectric radar | |
| CN112326686A (en) | Unmanned aerial vehicle intelligent cruise pavement disease detection method, unmanned aerial vehicle and detection system | |
| CN107140209A (en) | A kind of unmanned plane targeted system | |
| CN108507403A (en) | Self propelled Antiaircraft Gun multi-axial cord consistency detection device based on intelligent photoelectric calibration technique | |
| CN107885230A (en) | Depopulated helicopter control system and its control method with laser guided weapon | |
| CN103599631B (en) | Based on flying saucer simulated training system and the method for machine vision | |
| CN105573343A (en) | Capture system based on unmanned aerial vehicle | |
| CN105262986A (en) | Equipment and system for tracing and monitoring wild Macaque | |
| CN107403481A (en) | Information interaction system and information collecting device for unmanned vehicle | |
| CN110844026A (en) | Multi-degree-of-freedom bionic robot fish for real-time mobile monitoring of water quality and control method thereof | |
| CN111044989A (en) | Laser decoy interference equipment lures partial effect outfield evaluation system | |
| CN211527210U (en) | Robot target vehicle and robot target vehicle system | |
| CN205212941U (en) | Satellite sensing wild animal tracer | |
| CN107726929A (en) | A kind of field climbing rope that can launch | |
| CN214566043U (en) | Unmanned ship and unmanned aerial vehicle warm vortex information acquisition device in coordination | |
| CN113848992A (en) | Target detection location and automatic shooting system based on unmanned aerial vehicle and armed beating robot | |
| CN107328310B (en) | Multiple target target ship TT＆C system | |
| CN206654197U (en) | Unmanned plane in a kind of Multifunctional air | |
| CN211452056U (en) | Intelligent aiming slingshot |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |