CN205090877U - Portable guided missile follow -up emitter - Google Patents
Portable guided missile follow -up emitter Download PDFInfo
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- CN205090877U CN205090877U CN201520761849.0U CN201520761849U CN205090877U CN 205090877 U CN205090877 U CN 205090877U CN 201520761849 U CN201520761849 U CN 201520761849U CN 205090877 U CN205090877 U CN 205090877U
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Abstract
The utility model provides a portable guided missile follow -up emitter, include: collapsible tripod, power module, two follow -up revolving stages, photoelectric tracking appearance, missile launch device, power module installs on collapsible tripod, settles above the power module by two follow -up revolving stages of electronic level and vertical turn driven, is equipped with the missile launch device on one side of two follow -up revolving stages, the opposite side is equipped with the photoelectric tracking appearance, and the top is equipped with GPS positioner. The utility model discloses it is high -efficient, light, automatic to enable the missile launch process. It can break into a plurality of groups, and every group is lighter than 70kg, and the two people march be convenient for is carried, also can the snap -on on the cross country vehicle.
Description
Technical field
The utility model relates to air defence missile lift-off technology field, is specially the servo-actuated emitter of a kind of portable missile.
Background technology
At present, because portable missile accuracy at target is high, use and take care of the advantages such as simple, tactical mobility is good, disguise is strong, be used widely at near-earth air defence do-nothing system, but in the artificial operation issue pickaback of portable air defense missile, quick-reaction capability is poor, target acquisition is dumb, carries inconvenience.The portable duplex multiple missile launcher (open (bulletin) number: 203550783U) that the patent of existing announcement is carried, there is artificial capture method target in it, manually adjusts horizontal direction and vertical direction, the shortcomings such as response speed is slow.
Utility model content
The technical problem that the utility model solves is to provide a kind of portable missile servo-actuated emitter, can make that Missile Launching Process is efficient, light, automation.It can be split into some groups, and often group is less than 70kg, is convenient to two people's marches and carries, also can directly be fixed on offroad vehicle, to solve the problem proposed in above-mentioned background technology.
The technical problem that the utility model solves realizes by the following technical solutions: the servo-actuated emitter of a kind of portable missile, comprise: Foldable tripod, power module, the servo-actuated turntable of two axles, optronic tracker, guided missile launcher, described power module is arranged on Foldable tripod, the servo-actuated turntable of two axles driven by the gentle vertical rotary of electric water is settled above power module, two axles are servo-actuated, and turntable side is provided with guided missile launcher, opposite side is provided with optronic tracker, and top is provided with GPS positioner.
The servo-actuated turntable of described two axle comprises rotation body, rotating body lower end is arranged on fixed support by servo controller, drive unit is provided with between servo controller and rotation body, on fixed support, side is provided with gag lever post, rotate body both sides and be provided with window, window lower end is rotationally connected by hinge and rotation body, upper end is arranged on by hasp rotates on body, rotate body top and be provided with top cover, top cover is provided with handle, handle is arranged on top cover by handle Connection Block, rotate body front end and be provided with electric limiting baffle plate assembly, level meter group is provided with on the upside of electric limiting baffle plate assembly, electric limiting baffle plate assembly side is provided with orientation locking device.
Described optronic tracker comprises thermal infrared imager and laser range finder.
Described guided missile launcher is that duplex is sent out, three to be sent out, tetrad sends out one in emitter.
Described GPS positioner is made up of two GPS in a distance and position indicator thereof, is used for carrying out positioning and directing to whole device.
Described Foldable tripod comprises little arm component, large arm component, triangular element, and be provided with large arm component outside triangular element, large arm component outer end is provided with little arm component.
The servo-actuated turntable of described two axle is arranged on power module upper end by pivot pin, and optronic tracker is arranged on the servo-actuated turntable of two axles by plum blossom knob.
Compared with prior art, the beneficial effects of the utility model are: the utility model can make that Missile Launching Process is efficient, light, automation.It can be split into some groups, and often group is less than 70kg, is convenient to two people's marches and carries, also can directly be fixed on offroad vehicle.
Accompanying drawing explanation
Fig. 1 is front view schematic diagram of the present utility model.
Fig. 2 is left view schematic diagram of the present utility model.
Fig. 3 is three-dimensional icon of the present utility model intention.
Fig. 4 is the servo-actuated turntable structure schematic diagram of two axle of the present utility model.
Fig. 5 is the servo-actuated turntable three-dimensional icon intention of two axle of the present utility model.
Detailed description of the invention
In order to make actualizing technology means of the present utility model, creation characteristic, reach object and effect is easy to understand, below in conjunction with concrete diagram, set forth the utility model further.
As shown in Figures 1 to 3, the servo-actuated emitter of a kind of portable missile, comprise: Foldable tripod 1, the servo-actuated turntable 3 of power module 2, two axle, optronic tracker 5, guided missile launcher 4, described power module 2 is arranged on Foldable tripod 1, power module 2 settles the servo-actuated turntable 3 of two axles driven by the gentle vertical rotary of electric water above, two axles servo-actuated turntable 3 side is provided with guided missile launcher 4, opposite side is provided with optronic tracker 5, and top is provided with GPS positioner 6.
As Fig. 4, shown in Fig. 5, the servo-actuated turntable 3 of described two axle comprises rotation body 32, rotating body 32 lower end is arranged on fixed support 311 by servo controller 33, drive unit 314 is provided with between servo controller 33 and rotation body 32, on fixed support 311, side is provided with gag lever post 316, rotate body 32 both sides and be provided with window 310, window 310 lower end is rotationally connected by hinge 314 and rotation body 32, upper end is arranged on by hasp 319 rotates on body 32, rotate body 32 top and be provided with top cover 31, top cover 31 is provided with handle 315, handle 315 is arranged on top cover 31 by handle Connection Block 39, rotate body 32 front end and be provided with electric limiting baffle plate assembly 36, level meter group 35 is provided with on the upside of electric limiting baffle plate assembly 36, electric limiting baffle plate assembly 36 side is provided with orientation locking device 34, when target information converts two axle control commands to, realize two-axle interlocking, can 360 ° of rotations in the horizontal direction,-10 ° in vertical direction ~ 65 ° swings, its kinematic accuracy can reach 2mrad.
Described optronic tracker 5 comprises thermal infrared imager and laser range finder, for the automatic acquisition and tracking of target.
Described guided missile launcher 4 for duplex send out, three to send out, tetrad sends out one in emitter.
Described power module is voltage-stabilized power supply alternating current input being converted to multi-channel DC output; there is perfect protection system; the power module of a kind of high stability, high reliability, for power supplies such as fire control computer, servo-actuated servo-drive system, missile control system, photoelectric follow-ups.
Described GPS positioner 6 is made up of two GPS in a distance and position indicator thereof, is used for carrying out positioning and directing to whole device.
Described Foldable tripod comprises little arm component, large arm component, triangular element, and be provided with large arm component outside triangular element, large arm component outer end is provided with little arm component, and it can be used for supporting and maintain mechanism and run well.
The servo-actuated turntable 3 of described two axle is arranged on power module 2 upper end by pivot pin, and optronic tracker 5 is arranged on the servo-actuated turntable 3 of two axles by plum blossom knob.
Operation principle of the present utility model is:
First by A-frame from folded state launch open, after power module fast-assembling, follower scaffold is got on and locks, then from the left side by guided missile launcher 4 fast-assembling, GPS positioner 6, by geodimeter 5 fast-assembling, finally installs by the right.
The parameters such as the speed finding azimuth of target, the angle of pitch, distance are provided according to empty snares of love such as " antiaircraft bodyguard ", (such as 1min) launches the pre-frame of equipment at the appointed time, geodimeter starts to move in the horizontal and vertical directions according to target designation data simultaneously, intercepting and capturing, tracking target.After intercepting and capturing, tracking target, operation refers to press locking press button, and system is while activation readied missile, and automatic measurements and calculations tackle the necessary firepower control protocol of target.When target enters the effective operational distance of guided missile, operator presses button, and boost motor is lighted a fire.After MISSILE LAUNCHING, operator can start second time attack to same target, or attacks next target.
More than show and describe general principle of the present utility model and principal character and advantage of the present utility model.The technical staff of the industry should understand; the utility model is not restricted to the described embodiments; what describe in above-described embodiment and description just illustrates principle of the present utility model; under the prerequisite not departing from the utility model spirit and scope; the utility model also has various changes and modifications, and these changes and improvements all fall within the scope of claimed the utility model.Claimed scope of the present utility model is defined by appending claims and equivalent thereof.
Claims (6)
1. the servo-actuated emitter of portable missile, it is characterized in that: comprising: Foldable tripod, power module, the servo-actuated turntable of two axles, optronic tracker, guided missile launcher, described power module is arranged on Foldable tripod, the servo-actuated turntable of two axles driven by the gentle vertical rotary of electric water is settled above power module, two axles are servo-actuated, and turntable side is provided with guided missile launcher, opposite side is provided with optronic tracker, and top is provided with GPS positioner.
2. the servo-actuated emitter of a kind of portable missile according to claim 1, it is characterized in that: the servo-actuated turntable of described two axle comprises rotation body, rotating body lower end is arranged on fixed support by servo controller, drive unit is provided with between servo controller and rotation body, on fixed support, side is provided with gag lever post, rotate body both sides and be provided with window, window lower end is rotationally connected by hinge and rotation body, upper end is arranged on by hasp rotates on body, rotate body top and be provided with top cover, top cover is provided with handle, handle is arranged on top cover by handle Connection Block, rotate body front end and be provided with electric limiting baffle plate assembly, level meter group is provided with on the upside of electric limiting baffle plate assembly, electric limiting baffle plate assembly side is provided with orientation locking device.
3. the servo-actuated emitter of a kind of portable missile according to claim 1, is characterized in that: described optronic tracker comprises thermal infrared imager and laser range finder.
4. the servo-actuated emitter of a kind of portable missile according to claim 1, is characterized in that: described guided missile launcher is that duplex is sent out, three to be sent out, tetrad sends out one in emitter.
5. the servo-actuated emitter of a kind of portable missile according to claim 1, it is characterized in that: described Foldable tripod comprises little arm component, large arm component, triangular element, be provided with large arm component outside triangular element, large arm component outer end is provided with little arm component.
6. the servo-actuated emitter of a kind of portable missile according to claim 1, is characterized in that: the servo-actuated turntable of described two axle is arranged on power module upper end by pivot pin, and optronic tracker is arranged on the servo-actuated turntable of two axles by plum blossom knob.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520761849.0U CN205090877U (en) | 2015-09-29 | 2015-09-29 | Portable guided missile follow -up emitter |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520761849.0U CN205090877U (en) | 2015-09-29 | 2015-09-29 | Portable guided missile follow -up emitter |
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| CN205090877U true CN205090877U (en) | 2016-03-16 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201520761849.0U Active CN205090877U (en) | 2015-09-29 | 2015-09-29 | Portable guided missile follow -up emitter |
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Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110108161A (en) * | 2019-05-13 | 2019-08-09 | 上海机电工程研究所 | Guided missile launcher |
| CN111397439A (en) * | 2020-03-16 | 2020-07-10 | 上海机电工程研究所 | Portable guided missile firepower control equipment |
| CN112504011A (en) * | 2020-12-24 | 2021-03-16 | 中国人民解放军空军工程大学 | Ground-to-air missile weapon system killer area calculation model system |
-
2015
- 2015-09-29 CN CN201520761849.0U patent/CN205090877U/en active Active
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110108161A (en) * | 2019-05-13 | 2019-08-09 | 上海机电工程研究所 | Guided missile launcher |
| CN110108161B (en) * | 2019-05-13 | 2021-05-14 | 上海机电工程研究所 | Missile launching device |
| CN111397439A (en) * | 2020-03-16 | 2020-07-10 | 上海机电工程研究所 | Portable guided missile firepower control equipment |
| CN111397439B (en) * | 2020-03-16 | 2022-06-28 | 上海机电工程研究所 | Portable guided missile firepower control equipment |
| CN112504011A (en) * | 2020-12-24 | 2021-03-16 | 中国人民解放军空军工程大学 | Ground-to-air missile weapon system killer area calculation model system |
| CN112504011B (en) * | 2020-12-24 | 2022-10-14 | 中国人民解放军空军工程大学 | Ground-to-air missile weapon system killing area calculation model system |
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| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant |