CN104990465B - Follow the trail of and scout locator and the guided missile with the locator - Google Patents
Follow the trail of and scout locator and the guided missile with the locator Download PDFInfo
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- CN104990465B CN104990465B CN201510428515.6A CN201510428515A CN104990465B CN 104990465 B CN104990465 B CN 104990465B CN 201510428515 A CN201510428515 A CN 201510428515A CN 104990465 B CN104990465 B CN 104990465B
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- Prior art keywords
- locator
- guided missile
- enemy
- definition camera
- trail
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Abstract
Locator is scouted the invention discloses following the trail of; it includes Miniature high-definition camera, locator, self-destruction control priming device, glass fiber reinforced plastic protective cover, containment vessel, rotary shaft and mini radio altimeter; Miniature high-definition camera is covered with glass fiber reinforced plastic protective cover; locator, self-destruction control priming device and mini radio altimeter are closed in containment vessel, and containment vessel inside is filled with self-destruction blast or burning type medicine.Invention additionally discloses a kind of guided missile that locator is scouted with tracking, follow the trail of and scout locator in guided missile, guided missile head part and guided missile body portion connect blasting bolt.Injected with the guided missile for following the trail of scouting locator to enemy plane; things such as the glass fiber reinforced plastic protective covers covered on Miniature high-definition camera while taking off when Missile Body is separated with guided missile head; and slightly delayed explosibility; high-definition camera work on locator; to we report enemy position and shooting periphery situation photo (video) after at once from Ruined; make enemy can not find reason, be easy to guide the next step attack action of my army.
Description
Technical field
Followed the trail of the present invention relates to one kind and scout the standages such as enemy aircraft, naval vessel, tank vehicle (such as airplane parking area or storehouse
Room, military dock etc.) tracking and position device, more particularly to it is a kind of can follow the trail of scout the above-mentioned target of enemy tracking scout
Locator.
The invention further relates to a kind of guided missile that locator is scouted with above-mentioned tracking.
Background technology
Current China's periphery international environment is complicated, and potential military conflict may upgrade outburst at any time.Potentially, it is following
The disputes such as enemy and our border territory (ocean), resource are increasingly disagreed, are conflicted constantly, and we are it is necessary to have Corresponding Countermeasures.
In following outbreak of war, the war machine (instrument) brood of enemy is made a clean sweep of, war hidden danger is eliminated in bud or
War scope control in minimum, war time control reaches war effect best, and firmly control the master in battlefield most short
Dynamic power.
Current all types of camouflage means and technology are really brilliant, and the target of camouflage really debate by true and false difficulty, even if
Use advanced reconnaissance satellite or surveillance plane, it is also difficult to distinguish true and false target.
Accordingly, it is desirable to provide a kind of new technical scheme solves the above problems.
The content of the invention
The technical problem to be solved in the invention is to provide a kind of scouting enemy aircraft, naval vessel, tank vehicle etc. followed the trail of and stops
Locator is scouted in the tracking for putting place (such as airplane parking area or storehouse, military dock).
The technical problem that the present invention also needs to solve is to provide a kind of guided missile that locator is scouted with tracking.Can be quick
Insertion enemy plane, obtains and follows the trail of information.
To solve technical problem of the invention, the technical solution adopted by the present invention is：
Follow the trail of and scout locator, it includes that Miniature high-definition camera, locator, self-destruction control priming device, fiberglass are protected
Shield, containment vessel, rotary shaft and mini radio altimeter, the mini radio altimeter are used to control Miniature high-definition to image
The startup of head and locator, installs self-destruction and controls in the control connecting line between the mini radio altimeter and locator
Quick-fried device, is connected by rotary shaft between the Miniature high-definition camera and locator and rotated, outside the Miniature high-definition camera
Glass fiber reinforced plastic protective cover is covered with, the locator, self-destruction control priming device and mini radio altimeter are closed in protection
In shell, the containment vessel inside is filled with self-destruction blast or burning type medicine.
The containment vessel upper surface is embedded in glass fiber reinforced plastic protective cover inner side.
A kind of with the guided missile for following the trail of scouting locator, it includes guided missile head and Missile Body, and the guided missile head part is installed
Wing card, locator, self-destruction control priming device and mini radio altimeter in the containment vessel and containment vessel are arranged on
Guided missile head part, the Miniature high-definition camera in the glass fiber reinforced plastic protective cover and glass fiber reinforced plastic protective cover is arranged on Missile Body portion
Point, the guided missile head part and guided missile body portion connect blasting bolt.
Beneficial effects of the present invention：Injected with the guided missile for following the trail of scouting locator, Missile Body and guided missile head point to enemy plane
From when things such as the glass fiber reinforced plastic protective covers covered on Miniature high-definition camera while take off, and slightly delayed explosibility, on locator
High-definition camera work, to we report enemy position and shooting periphery situation photo (video) after at once from Ruined, make enemy look for not
Go out reason, be easy to guide the next step attack action of my army.
Brief description of the drawings
Fig. 1 is structural representation of the invention.
Fig. 2 is the schematic view of the mounting position followed the trail of and scout locator in guided missile of the invention.
Fig. 2 a are the enlarged diagram at A in Fig. 2.
Fig. 3 is the schematic diagram followed the trail of and scout in locator insertion enemy plane body of the invention.
Wherein, 1, Miniature high-definition camera, 2, locator, 3, self-destruction control priming device, 4, glass fiber reinforced plastic protective cover, 5, protect
Protective case, 6, rotary shaft, 7, mini radio altimeter, 8, control connecting line, 9, self-destruction blast or burning type medicine, 10, guided missile
Head, 11, Missile Body, 12, wing card, 13, blasting bolt, 14, the adiabatic protecting against shock resistance to compression protected material bed of material.
Specific embodiment
The invention will be further described with specific embodiment below in conjunction with the accompanying drawings.Following examples are merely to illustrate this hair
It is bright, it is not limited to protection scope of the present invention.
Shown in Fig. 1, Fig. 2, Fig. 2 a, Fig. 3, of the invention tracking scouts locator, and it includes Miniature high-definition camera 1, determines
Position device 2, self-destruction control priming device 3, glass fiber reinforced plastic protective cover 4, containment vessel 5, rotary shaft 6 and mini radio altimeter 7, it is miniature
Radio altimeter 7 is used to control the startup of Miniature high-definition camera 1 and locator 2, mini radio altimeter 7 and locator
Self-destruction control priming device 3 is installed, by rotation between Miniature high-definition camera 1 and locator 2 in the control connecting line 8 between 2
The connection of rotating shaft 6 is rotated, and Miniature high-definition camera 1 is covered with glass fiber reinforced plastic protective cover 4, locator 2, self-destruction control priming device 3 and
Mini radio altimeter 7 is closed in containment vessel 5, and the inside of containment vessel 5 is filled with self-destruction blast or burning type medicine 9.
The upper surface of containment vessel 5 is embedded in the inner side of glass fiber reinforced plastic protective cover 4.Coordinate the later stage guided missile insertion enemy plane after, guided missile head with
Missile Body is separated.
A kind of guided missile that locator is scouted with above-mentioned tracking, it includes guided missile head 10 and Missile Body 11, guided missile head 10
Divide and wing card 12 is installed, locator 2, self-destruction control priming device 3 and micro radio electrical height in containment vessel 5 and containment vessel 5
Table 7 is arranged on guided missile head part, and the Miniature high-definition camera 1 in glass fiber reinforced plastic protective cover 4 and glass fiber reinforced plastic protective cover 4 is arranged on and leads
Body part, guided missile head part and guided missile body portion connection blasting bolt 13.
The tracking is scouted locator and is arranged in guided missile, and its surrounding sets the multilayer heat insulation protecting against shock resistance to compression protected material bed of material
14, together separated together with glass fiber reinforced plastic protective cover 4 after guided missile head 10 is separated with Missile Body 11.
The protection shell (i.e. guided missile head part, refers to Fig. 2) of guided missile is designed and produced must be extremely firm, just as on aircraft
Black box, but volume should be as small as possible, and it is anti-must live the huge impact of external force, scout positioning without the tracking inside damage
Device.The self-destruction of internal band controls priming device 3, self-destruction immediately after completion task（As a miniature time bomb）.Micro radio
Electrical height table 7 is used to measure it with ground relative altitude.
Follow the trail of target：In initial stage of war or when there is small-scale military conflict, enemy and we's opportunity of combat (such as naval vessel, tank vehicle
Also in a similar manner) air battle, enemy is annihilated to obtain at one stroke, and the nest brood of enemy is made a clean sweep of, deliberately when with enemy's air battle,
Not once by enemy plane grand slam, but launch a guided missile to enemy plane (or naval vessel, tank vehicle etc. also in a similar manner) (or big gun
This is a kind of special guided missile (or shell) (such as Fig. 1) to play) ﹐, and a minimum class with high-definition camera is kept inside it
Like GPS（The BEI-DOU position system of China）Locator, enemy plane (or naval vessel, tank vehicle etc.) fuselage is stealthily inserted, to enemy
A kind of missile miss that we launches does not hit, a kind of sensation of the blast that passes each other so close that they almost rubbed each other.This locator insertion enemy plane body (or warship
Ship, tank vehicle etc.) in, just as ji fishes in the sea, enemy plane of leaving (or naval vessel, tank vehicle etc.) enemy base (such as Fig. 3) is taken back,
(particularly to enemy plane, storehouse is shut down after enemy to base), work is automatically begun to immediately, (also can be by satellite or high-altitude to us
Scounting aeroplane receive) report enemy position and shooting periphery situation photo (video) after at once from Ruined, make enemy can not find reason.
This similar GPS（The BEI-DOU position system of China）Tracking scout locator, concrete application is (to be with air battle
Example)：When there is small-scale air battle between ourselves and the enemy, my machine chooses a frame enemy plane as scouting positioning object is followed the trail of, and is injected to it
This inside keeps an air-launched missile for the similar GPS locator with minimum high-definition camera, and this guided missile is opposed in contact
Machine moment, front end wing card 12 opens immediately, prevents guided missile head 10 from inserting too deep in enemy plane body, because (2 Mach quickly of missile velocity
More than), kinetic energy is very big, it is easy to insert in enemy plane body (refer to Fig. 3).
It is connected with Missile Body 11 on V-type fixture block and band when this nose of missile has inserted enemy plane Ti Nei ﹐ its guided missile head 10
Blasting bolt 13 explode immediately, guided missile head is separated with Missile Body, and (this is modern existing ripe Separation skill
Art), the grade thing of glass fiber reinforced plastic protective cover 4 covered on Miniature high-definition camera 1 while lifting when Missile Body 11 is separated with guided missile head 10
Fall (refer to Fig. 2) (after guided missile head is completely disengaged from Missile Body) and slightly delayed explosibility (Missile Body blast after departing from), it is fixed to expose
High-definition camera on the device of position, is easy to the high-definition camera on locator to work.While also causing one kind to enemy plane, we launches
Missile miss blast sensation.High-definition camera can have the camera lens of 2 (as needed, or 1 good) different angles
Head, and can be rotated by 360 degree of directions of rotary shaft work, it is as comprehensive as possible to take high-definition image (or video).
Base is opposed when enemy plane flies back, when contact the runway ground is landed in base, is followed the trail of and is scouted locator (by mini radio
Altimeter controls high-definition camera and locator to start, and micro radio altimeter can measure enemy plane actual height from the ground) it is vertical
Work is automatically begun to, (particularly to enemy plane, storehouse is shut down) after being come to a complete stop to enemy plane ,-road shoots the periphery and inside of enemy plane
Situation photo (or video), to our (can also be received by satellite or high-altitude scounting aeroplane) report enemy's accurate location and shooting
Periphery situation photo (or video), after completing to shoot reconnaissance mission, i.e., automatic is destroyed from Ruined devices.Just in case high definition is taken the photograph
As head cisco unity malfunction, at least, the locator of similar GPS (Big Dipper) still can report enemy accurate geographical position, guide my army
Next step attack action.
Destroy target：After obtaining accurate enemy nest (base) position, we disposes rapidly the action scheme of next step, according to need
Will, if give accurate targeted elimination, eliminate these hidden danger, reach the strategy that the war machine (instrument) brood to opposing is made a clean sweep of
Purpose.
This tracking is scouted, and that leaves somebody at large the better to apprehend him is accurately positioned to enemy's nest (base), can not receive enemy's camouflage means
Deceiving and disturbing with technology, accomplish it is steady, accurate, pinpoint strike enemy resolutely, eliminate enemy, eliminate war hidden danger.
Claims (2)
1. a kind of with the guided missile for following the trail of scouting locator, it is characterised in that：Following the trail of scouting locator includes that Miniature high-definition is imaged
Head, locator, self-destruction control priming device and mini radio altimeter, the mini radio altimeter are miniature for controlling
The startup of high-definition camera and locator, installs certainly in the control connecting line between the mini radio altimeter and locator
Control priming device is ruined, is connected by rotary shaft between the Miniature high-definition camera and locator and rotated, the Miniature high-definition
Camera is covered with glass fiber reinforced plastic protective cover, and the locator, self-destruction control priming device and mini radio altimeter are sealed
Close in containment vessel, the containment vessel inside is filled with self-destruction blast or burning type medicine；Leading for locator is scouted with following the trail of
Bullet includes guided missile head and Missile Body, and wing card is installed in the guided missile head part, locator in the containment vessel and containment vessel, from
Ruin control priming device and mini radio altimeter is arranged on guided missile head part, the glass fiber reinforced plastic protective cover and fiberglass are protected
Miniature high-definition camera in shield is arranged on guided missile body portion, the guided missile head part and guided missile body portion connection blast spiral shell
Bolt；
In contact enemy plane moment, the front end wing card of guided missile head part opens guided missile immediately, when this nose of missile has inserted enemy plane
Its guided missile head of Ti Nei ﹐ and Missile Body connection blasting bolt explode immediately, guided missile head is separated with Missile Body, Missile Body with lead
Bullet takes the glass fiber reinforced plastic protective cover covered on Miniature high-definition camera off when separating, and guided missile head is led after being completely disengaged from Missile Body
Projectile explosive, exposes the high-definition camera on locator, is easy to the high-definition camera on locator to work；When enemy plane flies back enemy's base
Ground, base land contact the runway ground when, follow the trail of scout locator by mini radio altimeter control high-definition camera and
Locator starts, and mini radio altimeter can measure enemy plane actual height from the ground, and after being come to a complete stop to enemy plane ,-road shoots enemy
The periphery on airport and inner case photo, the periphery situation photo of enemy's accurate location and shooting is reported to us, is completed shooting and is detectd
After examining task, i.e., automatic is destroyed from Ruined devices.
2. according to claim 1 a kind of with the guided missile for following the trail of scouting locator, it is characterised in that：On the containment vessel
End face is embedded in glass fiber reinforced plastic protective cover inner side.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510428515.6A CN104990465B (en) | 2015-07-21 | 2015-07-21 | Follow the trail of and scout locator and the guided missile with the locator |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510428515.6A CN104990465B (en) | 2015-07-21 | 2015-07-21 | Follow the trail of and scout locator and the guided missile with the locator |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN104990465A CN104990465A (en) | 2015-10-21 |
| CN104990465B true CN104990465B (en) | 2017-06-30 |
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ID=54302308
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510428515.6A Expired - Fee Related CN104990465B (en) | 2015-07-21 | 2015-07-21 | Follow the trail of and scout locator and the guided missile with the locator |
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Families Citing this family (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107101539B (en) * | 2017-02-28 | 2019-04-30 | 湖北航天技术研究院总体设计所 | Unpowered transmitting delivery system cylinder separation method under a kind of big deep-water submersible |
| CN114838623A (en) * | 2022-05-24 | 2022-08-02 | 石家庄兵甲堂高科技有限公司 | Striking guiding indication device based on radio signal |
| CN114919485A (en) * | 2022-06-15 | 2022-08-19 | 中国人民解放军陆军炮兵防空兵学院 | Scout car |
Family Cites Families (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5943009A (en) * | 1997-02-27 | 1999-08-24 | Abbott; Anthony Steven | GPS guided munition |
| JPH10276358A (en) * | 1997-03-31 | 1998-10-13 | Mitsubishi Electric Corp | Video display system |
| SI1316774T1 (en) * | 2001-11-28 | 2006-12-31 | Rheinmetall Waffe Munition | High penetration and lateral effect projectiles having an integrated fragment generator |
| CN1403781A (en) * | 2002-10-21 | 2003-03-19 | 张宝林 | Portable dual high-speed air defense missile |
| CN102328746B (en) * | 2011-07-05 | 2015-04-15 | 罗晓晖 | Bag-release delay-control-type invisible bombing system of aircraft |
| CN103063086A (en) * | 2012-06-04 | 2013-04-24 | 叶锋 | Missile image guiding system |
| CN203190896U (en) * | 2013-04-24 | 2013-09-11 | 晋西工业集团有限责任公司 | Civil rocket projectile with locating function |
| CN203824443U (en) * | 2014-05-17 | 2014-09-10 | 中国人民武装警察部队工程大学 | Reconnoitering bullet |
| CN104251647B (en) * | 2014-08-28 | 2016-08-24 | 李淑兰 | The gun-launcher bullet that recording is scouted can be shot |
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2015
- 2015-07-21 CN CN201510428515.6A patent/CN104990465B/en not_active Expired - Fee Related
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| CN104990465A (en) | 2015-10-21 |
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