CN207300054U - A kind of guided missile induces ball - Google Patents
A kind of guided missile induces ball Download PDFInfo
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- CN207300054U CN207300054U CN201720669613.3U CN201720669613U CN207300054U CN 207300054 U CN207300054 U CN 207300054U CN 201720669613 U CN201720669613 U CN 201720669613U CN 207300054 U CN207300054 U CN 207300054U
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- Prior art keywords
- guided missile
- ball
- induces
- induction
- induction ball
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Abstract
The utility model provides a kind of guided missile induction ball, including supply unit, control device and induction ball body, it is characterised in that：The induction ball body is the polyhedron being made of multiple LED pieces, and the polyhedron includes groove, ridge, outer dead centre and inner vertex.The guided missile of the utility model induces compact spherical structure, easy to use, easy disassembling, cost relatively low, has prominent inducing effect to the guided missile of laser and radar guidance.In civil field, radar reflector can be used as, while there is transmitting LED lamplight as signal source, the fields such as military and ship lifesaving in danger can be widely used in.
Description
Technical field
It the utility model is related to military defense field, more particularly to missile defence field.
Background technology
It is to determine the key factor of modern war triumph to obtain control of the air, and therefore, military secret is being accused each other and opposed with enemy plane
It can survive under the strike of square air defence missile most important.At present, guided missile has following several homing guidance modes.It is infrared
Guidance, the position of the airborne missile of high temperature etc. is detected by infrared photoreceptor in front of guided missile, constantly towards this target flight,
Explode when close to target.Radar guidance has two kinds, and a kind of is the radar detection target by fighter plane or warship etc.,
It is then sent to the guided missile of flight, guides missile flight and target, after having launched guided missile, aircraft cannot be directly off,
And it must continue to instruct the action of guided missile.Another kind is that radar system is carried on guided missile, and transmitting after image infrared guidance is the same, from
Oneself tracks target, and destroys.Laser guidance, by aircraft or manually launches beam of laser, impinges upon in the target to be attacked, so
After launch a guided missile, have optical inductor in front of guided missile, it is attacked, transmitting to target flight it can be found that bright LASER SPECKLE
Afterwards, it is impossible to close laser or be moved to beyond target.GPS is guided, and is usually what cruise missile used.Cruise missile will
Fly thousands of kilometers, and detour is goed deep into as aircraft, target of attack.Route of travel is pre-designed is placed in cruise missile
Face, then guides the position and direction of its flight by gps satellite.
It is mainly the following conflicting mode at present：Two kinds are commonly used for the guided missile of infrared guidance, one kind is spraying machine
Carrying fuel oil and light equipment, fuel oil is burnt in the air, abduct the infra-red missile such as AIM-9 etc, advantage is that interference region is big,
Shortcoming is aircraft to be lighted when holding reinforcing；Another kind is metal burning bullet, and combustible metal is stored in engine nozzle by opportunity of combat
Near, the used time is crossed by the heat wave back warp that aerostatic press or gravity are sprayed from engine nozzle and lighted, with close to 1200 degree or so of temperature
Degree is inveigled, and can play interference effect within 2 ~ 9 seconds, for inveigling enemy's infrared guidance weapon to depart from true target, have compared with
The infra-red radiation bullet of high-temperature, also known as IR decoy.For some radar areas of the guided missile generally use of radar guidance
Especially big decoy jamming bullet, this ammunition be it is a kind of in cartridge chamber equipped with a large amount of chafves to disturb the informationization of radar echo signal
Ammunition.It is dished out chaff block from body bottom in unfriendly target overhead.Split after the release of chaff block.Chaff is spread into cloud form simultaneously
Low speed lands, and produces scattering to enemy radar signal, makes its cisco unity malfunction.The jamming bomb that presently, there are, which generally has, to be prepared
Complex process, cost is higher, easily by environmental disturbances such as weather the shortcomings of.
Utility model content
In order to overcome the problems of the prior art, the utility model solves technical solution used by aforementioned technical problem
It is：A kind of guided missile induces ball, including supply unit, control device and induction ball body, and the induction ball body is by multiple LED
The polyhedron that lamp piece is formed, the polyhedron include groove, ridge, outer dead centre and inner vertex.
Preferably, the LED light plate shape is irregular fan-shaped, and the irregular sector is by two straight lines and one
Arc-shaped side is formed, two straight line equal lengths or unequal.
Any of the above-described scheme is preferably, and the groove is formed by connecting by two adjacent LED pieces straight lines, two institutes
State straight line equal length.
Any of the above-described scheme is preferably, and three grooves intersect, and intersection point forms inner vertex, and the inner vertex direction is
It is recessed to the inside of induction ball.
Any of the above-described scheme is preferably, and the ridge is formed by connecting by two adjacent LED pieces arc-shaped sides, described in two
Arc-shaped side radian is identical.
Any of the above-described scheme is preferably, and five ridges intersect, and intersection point forms outer dead centre, and the outer dead centre direction is prominent
Go out to the outside of induction ball.
Any of the above-described scheme is preferably, and is connected between adjacent LED lamp piece by one or more locating fasteners, described fixed
Position buckle is arranged on LED pieces straight line and arc-shaped side, and adjacent LED lamp piece also can be described viscous by multiple bonding spot gluings
Contact is evenly distributed on LED pieces straight line and arc-shaped side.
Any of the above-described scheme is preferably, and is set at the inner vertex and outer dead centre and determine square ring and is positioned, or setting
Adhesive spots carry out cemented in place.
Any of the above-described scheme is preferably, and the LED pieces include LED chip and COB substrates, the substrate surface coating
Metal coating.
Any of the above-described scheme is preferably, and the metal coating includes aluminized coating, spelter coating, silver coating, and thickness is 5 ~ 25
Micron.The aluminized coating, spelter coating, silver coating all have higher radar area, can have to radar-guided missile
Effect interference.
Any of the above-described scheme is preferably, and the metal coating surface is for plane or with concavo-convex out-of-flatness surface.Work as institute
State metal coating surface and be polished into smooth plane, visible ray and black light can be reflected, it is seen that light is for example red, it is orange, yellow, green,
The light such as green grass or young crops, indigo plant, purple, black light such as infrared ray, ultraviolet, X-ray, coffee ray, laser etc..For induced with laser
Guided missile, can by inducing the reflex of the polyhedral structure of ball and coating, laser get on guided missile induction ball formed it is polygonal
Multidirectional reflection is spent, the aiming to induced with laser guided missile interferes, and guided missile is lost target.When the metal coating surface
During for concavo-convex out-of-flatness surface, by rationally designing microcosmic coating bumps angle, strengthen radar area, to improve thunder
Up to signal reflex intensity, the signal identification of the radar system in guided missile can be disturbed, guided missile is hit induction ball so as to ensure mesh
Mark the safety of thing.
Any of the above-described scheme is preferably, and the supply unit is arranged on induction ball body interior, passes through card with LED pieces
Button connection, for induction ball power supply.LED pieces can assemble the lamp bead of different colours, shine after induction ball powers on, as
Optical signal source, outwards launches light signal.The guided missile induction ball can also be used as light source and radar reflector, applied to ship
The fields such as lifesaving in danger.
Any of the above-described scheme is preferably, and the supply unit wirelessly charges.
Any of the above-described scheme is preferably, and the control device includes MCU chip, and LCD drive circuits are incorporated into MCU chip
On.
Any of the above-described scheme is preferably, it is described induction ball body in can also set echo enhancer, noise jammer,
Deception jammer.
Any of the above-described scheme is preferably, and the guided missile induction ball is launched by emitter, and the emitter is set
On aircraft, warship or unmanned plane.
The guided missile induction ball of the utility model, for laser-guided bomb, can effectively swash in the multi-direction reflection of multi-angle
Light, interferes laser-guided bomb；After running into the strafing of radar electromagnetic wave, due to its coating material and multiaspect figure modelling
Radar electromagnetic wave can be amplified, the signal identification of the radar system in guided missile can be disturbed, radar decoy be formed, to break away from
The tracking of enemy radar.Guided missile induction ball when in use, can by grenade instrumentation, large area is continuously launched in the air, formed dry
Corridor or interference barrier are disturbed, to screen the operation of one's own side's group of planes.Can also to guided missile induce ball radar area into
Row design, interruption launch effective reflecting surface and the similar induction ball of true target, form many radar decoys, cause enemy radar
Operating personnel's interpretation is difficult and data handling system is overloaded.The utility model guided missile induction spherical structure it is compact, it is easy to use, tear open
Dressing is easy, cost is relatively low, has prominent inducing effect to the guided missile of laser and radar guidance., can conduct in civil field
Radar reflector, while there is transmitting LED lamplight as signal source, military and ship lifesaving in danger etc. can be widely used in
Field.
Brief description of the drawings
Fig. 1 is the top view for the preferred embodiment that ball is induced according to the guided missile of the utility model.
Fig. 2 is the front view that embodiment described in Fig. 1 of ball is induced according to the guided missile of the utility model.
Fig. 3 is the front view for another preferred embodiment that ball is induced according to the guided missile of the utility model.
Fig. 4 is the attached view for the embodiment illustrated in fig. 3 that ball is induced according to the guided missile of the utility model.
Fig. 5 is the front view for the further embodiment that ball is induced according to the guided missile of the utility model.
Fig. 6 is the attached view for the embodiment illustrated in fig. 5 that ball is induced according to the guided missile of the utility model.
Illustrate：1- grooves, 2- ridges, 3- outer dead centres, 4- inner vertexs.
Embodiment
In order to be further understood that the content of the invention of the utility model, below in conjunction with specific embodiment to the utility model
It is described in more detail, embodiment only has exemplary effect to the utility model, without the effect of any restrictions；
The insubstantial modifications that any those skilled in the art make on the basis of the utility model, should all belong to the utility model guarantor
The scope of shield.
Embodiment 1
As depicted in figs. 1 and 2, a kind of guided missile induction ball, including supply unit, control device and induction ball body, it is described
Induction ball body is the polyhedron being made of multiple LED pieces, and the polyhedron includes groove, ridge, outer dead centre and inner vertex.
In the present embodiment, the LED light plate shape is irregular fan-shaped, it is described it is irregular it is fan-shaped by two straight lines and
One arc-shaped side is formed, two straight line equal lengths, and preferably two straight line angles are 110 °.
In the present embodiment, the groove is formed by connecting by two adjacent LED pieces straight lines, three groove phases
Hand over, intersection point forms inner vertex, and the inner vertex direction is to be recessed to the inside of induction ball.
In the present embodiment, the ridge is formed by connecting by two adjacent LED pieces arc-shaped sides, and five ridges intersect,
Intersection point forms outer dead centre, and the outer dead centre direction is to protrude to the outside of induction ball.
In the present embodiment, connected between adjacent LED lamp piece by one or more locating fasteners, the locating fastener is set
Put on LED pieces straight line and arc-shaped side.
In the present embodiment, set at the inner vertex and outer dead centre and determine square ring and positioned.
In the present embodiment, the LED pieces include LED chip and COB substrates, and the substrate surface coating metal applies
Layer.
In the present embodiment, the metal coating is silver coating, and thickness is 10 microns.
In the present embodiment, the silver coating surface is polished into smooth plane, can reflect visible ray and black light,
The light such as visible ray such as red, orange, yellow, green, blue, blue, purple, black light such as infrared ray, ultraviolet, X-ray, coffee ray,
Laser etc.., can be by inducing the reflex of the polyhedral structure of ball and coating for the guided missile of induced with laser, laser is got to
The multidirectional reflection of multi-angle is formed on guided missile induction ball, the aiming to induced with laser guided missile interferes, and guided missile is lost mesh
Mark.Simultaneously as the silver coating all has higher radar area, radar signal reflections intensity can be improved, so that
The signal identification of the radar system in guided missile is disturbed, guided missile is hit induction ball so as to ensure the safety of object.
In the present embodiment, the supply unit is arranged on induction ball body interior, with LED pieces by snapping connection,
For induction ball power supply.LED pieces assemble the lamp bead of red, yellow, blue color at the same time, shine after induction ball powers on, as light
Signal source, outwards launches light signal.By the combination of different lamp bead colors, the light of different colours can be sent, such as reddish yellow light
Combination, sends orange-colored light, and the combination of champac light, sends green light, so that the optical signal of different colours is formed, for different colours and not
Light signal with flicker frequency sets different signal contents, and induction ball can be made to play the effect of optical signal source.It is described to lead
Bullet induction ball can also be used as light source and radar reflector, applied to fields such as ship lifesaving in danger.
In the present embodiment, the supply unit wirelessly charges.
In the present embodiment, the control device includes MCU chip, and LCD drive circuits are incorporated into MCU chip.
In the present embodiment, in the induction ball body echo enhancer, noise jammer, deception formula can also be set to do
Disturb machine.
In the present embodiment, the guided missile induction ball is launched by emitter, and the emitter is arranged on aircraft, army
On warship or unmanned plane.
The guided missile induction ball of the present embodiment, for laser-guided bomb, can the effectively multi-direction reflection laser of multi-angle,
Laser-guided bomb is interfered；After running into the strafing of radar electromagnetic wave, coating material and multiaspect figure modelling meeting due to it
Radar electromagnetic wave is amplified, the signal identification of the radar system in guided missile can be disturbed, forms radar decoy, to break away from enemy
The tracking that Fanglei reaches.Guided missile induction ball when in use, can by grenade instrumentation, large area is continuously launched in the air, formed interference
Corridor or interference barrier, to screen the operation of one's own side's group of planes, can also induce guided missile the radar area of ball to carry out
Design, interruption launch effective reflecting surface and the similar induction ball of true target, form many radar decoys, cause enemy radar to grasp
Make personnel's interpretation difficulty and data handling system overload.The utility model guided missile induction spherical structure it is compact, it is easy to use, dismounting
Easily, cost is relatively low, has prominent inducing effect to the guided missile of laser and radar guidance.In civil field, thunder can be used as
Up to reflector, while there is transmitting LED lamplight as signal source, the neck such as military and ship lifesaving in danger can be widely used in
Domain.
Embodiment 2
As shown in Figure 3 and Figure 4, a kind of guided missile induction ball, including supply unit, control device and induction ball body, it is described
Induction ball body is the polyhedron being made of multiple LED pieces, and the polyhedron includes groove, ridge, outer dead centre and inner vertex.
In the present embodiment, the LED light plate shape is irregular fan-shaped, it is described it is irregular it is fan-shaped by two straight lines and
One arc-shaped side is formed, and two straight line equal lengths, two straight line angles are 95 °.The groove is by two adjacent LED light
Piece straight line is formed by connecting, two straight line equal lengths.Three the groove intersects, and intersection point forms inner vertex, described
Inner vertex direction is to be recessed to the inside of induction ball.The ridge is formed by connecting by two adjacent LED pieces arc-shaped sides, described in two
Arc-shaped side radian is identical.Five the ridge intersects, and intersection point forms outer dead centre, and the outer dead centre direction is to be prominent to outside induction ball
Portion.The angle angle that 2 cathetus side angle of embodiment is compared in embodiment 1 reduces, in induction bulb diameter（Outer dead centre to induction ball
Circle center distance）Under same case, make the inner vertex deeper into induction ball inside, compared to embodiment 1 have bigger surface area,
Be conducive to strengthen the multi-direction reflection of multi-angle to laser or radar.
In the present embodiment, it is evenly distributed between adjacent LED lamp piece by multiple bonding spot gluings, the adhesive spots
On LED pieces straight line and arc-shaped side.
In the present embodiment, adhesive spots are set to carry out cemented in place at the inner vertex and outer dead centre.
In the present embodiment, the LED pieces include LED chip and COB substrates, and the substrate surface coating metal applies
Layer.
In the present embodiment, the metal coating includes aluminized coating, and thickness is 5 ~ 25 microns.The aluminized coating surface is band
Concavo-convex out-of-flatness surface.By varying local coatings thickness, microcosmic coating bumps angle is rationally designed, strengthens radar reflection face
Product, to improve radar signal reflections intensity, can disturb the signal identification of the radar system in guided missile, guided missile is hit induction ball
So as to ensure the safety of object.
In the present embodiment, the supply unit is arranged on induction ball body interior, with LED pieces by snapping connection,
For induction ball power supply.LED pieces can assemble the lamp bead of different colours, shine after induction ball powers on, as optical signal
Source, outwards launches light signal.Guided missile induction ball can also be used as light source and radar reflector, rescue applied to ship is in danger
The field such as raw.
In the present embodiment, the supply unit wirelessly charges.
In the present embodiment, the control device includes MCU chip, and LCD drive circuits are incorporated into MCU chip.
In the present embodiment, in the induction ball body echo enhancer, noise jammer, deception formula can also be set to do
Disturb machine.
In the present embodiment, the guided missile induction ball is launched by emitter, and the emitter is arranged on aircraft, army
On warship or unmanned plane.
Embodiment 3
Embodiment 3 is similar to Example 1, the difference is that as shown in Figure 5 and Figure 6, the guided missile induction ball in the present embodiment
Shape is close to rugby shape, and the LED light plate shape is irregular fan-shaped, and the irregular sector is by two straight lines and one
Arc-shaped side is formed, and two straight line edge lengths are unequal.The groove is formed by connecting by two adjacent LED pieces straight lines, and two
A straight line equal length.Three grooves intersect composition inner vertex, and the inner vertex direction is to be recessed to induction ball
It is internal.The ridge is formed by connecting by two adjacent LED pieces arc-shaped sides, and two arc-shaped side radians are identical.Described in five
Ridge intersects, and intersection point forms outer dead centre, and the outer dead centre direction is to protrude to the outside of induction ball.
Since guided missile induces ball integrally close to rugby shape, and centered on symmetrical irregular polyhedrons, in the present embodiment
Guided missile induction ball warp cross grenade instrumentation transmitting after, under gravity and airflow function, produce irregular rotation at a high speed in the air, it is right
It is stronger in the albedo of laser and radar, and angle and direction is changeable, enemy's signal receiving device can be produced stronger
Interference.
Although the utility model, those skilled in the art has shown and described referring particularly to its preferred embodiment
It is appreciated that the various changes that can be made in form and details are new without departing from this practicality described in the appended claims
The scope of type.It is described in detail above in association with specific embodiment of the utility model, but is not the limit to the utility model
System.Every foundation the technical essence of the utility model still falls within this practicality to any simple modification made for any of the above embodiments
The scope of new technique scheme.
Claims (11)
1. a kind of guided missile induces ball, including supply unit, control device and induction ball body, it is characterised in that：The induction ball
Body is the polyhedron being made of multiple LED pieces, and the polyhedron includes groove, ridge, outer dead centre and inner vertex；The LED
Lamp plate shape is irregular fan-shaped, and the irregular sector is made of two straight lines and an arc-shaped side, two straight line length of sides
Spend equal or unequal；The groove is formed by connecting by two adjacent LED pieces straight lines, two straight line edge lengths phases
Deng；Three the groove intersects, and intersection point forms inner vertex, and the inner vertex direction is to be recessed to the inside of induction ball；The ridge by
Two adjacent LED pieces arc-shaped sides are formed by connecting, and two arc-shaped side radians are identical；Five the ridge intersects, intersection point structure
Into outer dead centre, the outer dead centre direction is to protrude to the outside of induction ball.
2. guided missile according to claim 1 induces ball, it is characterised in that：Pass through one or more between adjacent LED lamp piece
Locating fastener connects, and the locating fastener is arranged on LED pieces straight line and arc-shaped side, and adjacent LED lamp piece also can be by more
A bonding spot gluing, the adhesive spots are evenly distributed on LED pieces straight line and arc-shaped side.
3. guided missile according to claim 1 induces ball, it is characterised in that：Set at the inner vertex and outer dead centre and determine square ring
Positioned, or set adhesive spots to carry out cemented in place.
4. guided missile according to claim 1 induces ball, it is characterised in that：The LED pieces include LED chip and COB bases
Plate, the substrate surface coat metal coating.
5. guided missile according to claim 4 induces ball, it is characterised in that：The metal coating include aluminized coating, spelter coating,
Silver coating, thickness are 5~25 microns.
6. guided missile according to claim 4 induces ball, it is characterised in that：The metal coating surface is for plane or with bumps
Out-of-flatness surface.
7. guided missile according to claim 1 induces ball, it is characterised in that：The supply unit is arranged in induction ball body
Portion, with LED pieces by snapping connection, for induction ball power supply.
8. guided missile according to claim 7 induces ball, it is characterised in that：The supply unit wirelessly charges.
9. guided missile according to claim 1 induces ball, it is characterised in that：The control device includes MCU chip, and LCD drives
It is dynamic circuit integrated in MCU chip.
10. guided missile according to claim 1 induces ball, it is characterised in that：It can also be set back in the induction ball body
Ripple booster, noise jammer, deception jammer.
11. guided missile according to claim 1 induces ball, it is characterised in that：The guided missile induction ball is thrown by grenade instrumentation
Penetrate, the grenade instrumentation is arranged on ground, aircraft, warship or unmanned plane.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720669613.3U CN207300054U (en) | 2017-06-09 | 2017-06-09 | A kind of guided missile induces ball |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720669613.3U CN207300054U (en) | 2017-06-09 | 2017-06-09 | A kind of guided missile induces ball |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207300054U true CN207300054U (en) | 2018-05-01 |
Family
ID=62449832
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720669613.3U Expired - Fee Related CN207300054U (en) | 2017-06-09 | 2017-06-09 | A kind of guided missile induces ball |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207300054U (en) |
-
2017
- 2017-06-09 CN CN201720669613.3U patent/CN207300054U/en not_active Expired - Fee Related
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| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20180501 |
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| CF01 | Termination of patent right due to non-payment of annual fee |