CN203116621U - Detachable anti-intercept and anti-laser-attack flyer capable of releasing bait object - Google Patents
Detachable anti-intercept and anti-laser-attack flyer capable of releasing bait object Download PDFInfo
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- CN203116621U CN203116621U CN 201320068445 CN201320068445U CN203116621U CN 203116621 U CN203116621 U CN 203116621U CN 201320068445 CN201320068445 CN 201320068445 CN 201320068445 U CN201320068445 U CN 201320068445U CN 203116621 U CN203116621 U CN 203116621U
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Abstract
The utility model provides a detachable anti-intercept and anti-laser-attack flyer capable of releasing a bait object. The detachable anti-intercept and anti-laser-attack flyer capable of releasing the bait object comprises a shell body, a separation layer, a processor, a detection module, a power supply, at least one bait object, a protection layer, an orbit control system and a third switch, wherein the processor, the detection module, the power supply, the bait object, the protection layer, the orbit control system and the third switch are arranged in the shell body, and the third switch controls the separation layer to break away from the shell body. When the detection module detects that an interceptor target exists in a scheduled detection travel, the processor controls the third switch to be turned off and therefore to control the separation layer to break away from the shell body. Meanwhile, the processor controls a second switch to be turned off and therefore controls a hatch to be opened, therefore the bait object is released, and the flyer seizes the chance to escape. When a laser detection system detects the flyer and sends laser to the flyer, a protection layer on the outer surface of the separation layer will reflect the laser emitted on the separation layer, therefore the flyer is protected from damage, and equipment in the flyer is not damaged. Meanwhile, the processor sends a control signal to the orbit control system to control the flyer to break away from an original flying obit and to escape the tracking and the intercepting of the laser detection system.
Description
Technical field
The utility model relates to a kind of counnter attack waveguide technology, specifically is a kind of anti-interception flying object that anti-laser hits, discharges the bait thing and can separate that has, and belongs to the space flight technical field.
Background technology
At present, space exploration mainly contains various scouting Detection Techniques such as radar detection, visible light detection, laser acquisition, infrared acquisition, acoustic sounding, be used for surveying and finding the airflight thing, correspondingly the anti-Detection Techniques means in space are also given tit for tat, use various anti-detection methods to realize the airflight thing by various Detection Techniques means discoveries, thus can safe flight.
Along with advancing by leaps and bounds of modern science, sound, light, electricity, etc. the fast development of technology greatly enriched the obtaining means of information, and these technology are also changing detection and the defense system of countries in the world.Stealth technology is a kind of military technology that grows up in Detection Techniques and anti-Detection Techniques progress, the stealth technology stealth technique that is otherwise known as, refer to reduce the various detectable feature of target, make enemy's detecting devices be difficult to find or make the integrated technology of the detectivity reduction of enemy's detecting devices.Stealth technology is the cross-application technology of multiple subject technologies such as integrated fluid dynamics, material science, electronics, optics, acoustics, by changing the detectable information characteristics of target, making enemy's detection system be difficult for finding or finding the complex art that distance shortens, is development and the extension that traditional camouflage is moved towards high-techization.Modern stealth technology is subjected to the great attention of each main military country of the world as the effective means that improves armament systems survival ability and penetration ability.
But enemy's detection system utilizes Detection Techniques in a single day to detect target, just target is followed the trail of interception, makes target can't break away from enemy's detection system, causes the mission failure of target.Advantages such as laser has high energy, high focusing, and is high-speed, present many countries are developing superlaser equipment energetically, destroy the airflight thing with laser high temperature, thereby the airflight thing is tackled successfully.
The utility model content
To be solved in the utility model is the technical problem that can't break away from after flyer aerial in the prior art is detected system and detects, thus can break away from after providing a kind of detection system to detect have an anti-interception flying object that anti-laser hits, discharges the bait thing and can separate.
For solving the problems of the technologies described above, the utility model is achieved through the following technical solutions:
A kind of anti-interception flying object that has anti-laser strike, discharges the bait thing and can separate comprises,
Housing and separating layer,
And be arranged on the 3rd switch that processor, detecting module, hatch, power supply, at least one bait thing protective layer, control system and the described separating layer of control in the described housing breaks away from described housing;
Wherein,
Described detecting module is connected with described processor, is used for surveying in predefined spy journey and result of detection being sent to described processor;
Hatch is used for discharging described bait thing, is arranged on the close described bait thing place of described housing, and described hatch is connected with described processor by second switch; Described processor is controlled described second switch closure according to the result of detection that has the interceptor target in the predetermined spy journey that receives and then is controlled described hatch and open;
At least one bait thing, when described hatch was opened, at least one described bait thing broke away from described housing;
Described separating layer is arranged on the skin of described housing; Described processor is controlled described the 3rd switch closure and then is separated described separating layer according to the result of detection that receives when having detected target;
Protective layer covers the skin of described separating layer, and the light that is used for shining described separating layer reflects away;
Control system is connected with described processor, is used for the flight track of this flying object of control;
Described power supply is used for giving above-mentioned each module for power supply.
The described anti-interception flying object that has anti-laser strike, discharges the bait thing and can separate, the aerostat that described bait thing is the spray metal film and/or bait decoy warhead and/or true bullet.
The described anti-interception flying object that has anti-laser strike, discharges the bait thing and can separate, described the 3rd switch is arranged in the described housing, described separating layer is provided with separates executing agency, when described the 3rd switch closure, the action of described separation executing agency drives described separating layer and breaks away from described housing.
Described have an anti-interception flying object that anti-laser hits, discharges the bait thing and can separate, and described separation executing agency is priming device.
The described anti-interception flying object that has anti-laser strike, discharges the bait thing and can separate, described priming device is electric cap.
The described anti-interception flying object that has anti-laser strike, discharges the bait thing and can separate, described protective layer is reflector layer or arranges the polygon prism layer that arranges.
The described anti-interception flying object that has anti-laser strike, discharges the bait thing and can separate, described protective layer are the outer field reflector layer and the polygon prism layer that is arranged on the described reflector layer skin that covers described separating layer.
The described anti-interception flying object that has anti-laser strike, discharges the bait thing and can separate, described reflector layer is metal reflective layer or graphite reflector layer.
The described anti-interception flying object that has anti-laser strike, discharges the bait thing and can separate, also comprise the startup control module, link to each other with described processor, when entry condition does not arrive, control described processor dormancy, and when entry condition arrives, control described processor and start working; Described entry condition is predetermined time or predetermined geographical position.
The described anti-interception flying object that has anti-laser strike, discharges the bait thing and can separate, described startup control module is timer, when described timer timing reaches predetermined time, described startup control module is controlled described processor and is started working, otherwise described startup control module is controlled described processor dormancy.
Technique scheme of the present utility model has the following advantages compared to existing technology:
(1) the anti-interception flying object that has anti-laser strike, discharges the bait thing and can separate described in the utility model, comprise housing and separating layer, and be arranged on the 3rd switch that described housing interior processor, detecting module, hatch, power supply, at least one bait thing, protective layer, control system and the described separating layer of control break away from described housing; Described detecting module is surveyed in predefined spy journey and result of detection is sent to described processor, when following the trail of this flying object of interception result of that probe is sent to described processor when described detecting module detects detection system in predefined spy journey, described processor is controlled described the 3rd switch closure and then is separated described separating layer according to the result of detection that receives when having detected target; Simultaneously, described processor is controlled described second switch closure and then is controlled described hatch and open, thereby discharges described bait thing.These bait things have had the multifrequency nature of flying object, as speed characteristics, infrared signature, radar reflect property, aerodynamic characteristic etc., be enough to mix the spurious with the genuine, the difficult real target of distinguishing of the sensor on the detection system, this mode is very big to the threat of detection system.If bait decoy warhead quantity is more, the sensor on the detection system is the more difficult real target of distinguishing in many objective bodies just, and this flying object takes advantage of the occasion to escape under the shielding of bait thing.
When laser detection system detects this flying object, during to this flying object emission laser, the protective layer on this flying object separating layer surface can reflect away the laser that shines described separating layer, thereby protects described flying object not destroyed, and the equipment in the described flying object does not damage; Simultaneously, described detecting module is surveyed in predefined spy journey and result of detection is sent to described processor, when detecting detection system in predefined spy journey, detecting module when following the trail of this flying object of interception, result of that probe is sent to described processor, described processor transmits control signal to described control system, after described control system receives the control signal of described processor transmission, control this flying object and break away from original flight track, break away from the tracking interception of laser detection system.
(2) the anti-interception flying object that has anti-laser strike, discharges the bait thing and can separate described in the utility model, also comprise the startup control module, link to each other with described processor, when entry condition does not arrive, control described processor dormancy, and when entry condition arrives, control described processor and start working.If the flying distance of this flying object is short, processor can be in running order always, but when flying distance is long, if processor is in running order always, power supply can exhaust in the flight way, and processor can not carry out work, this flying object can't break away from when running into the tracking interception.The startup control module is set in flying object, before the flight prerequisite, entry condition is set, when beginning to fly, start control module and control described processor sleep state, when entry condition arrives, start control module control processor and start working, this mode can guarantee that flying object is long in flying distance, processor also can be worked when running into the interception tracking, and power consumption was little when processor was in dormancy, energy-conserving and environment-protective.
Description of drawings
Content of the present utility model is easier clearly to be understood in order to make, below in conjunction with accompanying drawing, the utility model is described in further detail, wherein,
Fig. 1 is the utility model embodiment 1 described structural representation with anti-interception flying object that anti-laser hits, release bait thing also can separate;
Fig. 2 is the utility model embodiment 2 described structural representations with anti-interception flying object that anti-laser hits, release bait thing also can separate.
Reference numeral is expressed as among the figure: 01-bait thing, and the 02-separating layer, the 1-processor, 11-starts control module, 2-detecting module, 3-housing, 31-hatch, 4-power supply, 72-second switch, 73-the 3rd switch, 8-protective layer, 9-control system.
The specific embodiment
Embodiment 1:
The structure of the anti-interception flying object that has anti-laser strike, release bait thing and can separate described in the utility model as shown in Figure 1, it comprises housing 3 and separating layer 02, and is arranged on processor 1, detecting module 2, hatch 31, power supply 4, at least one bait thing 02, protective layer 8, the control system 9 in the described housing 3 and controls the 3rd switch 73 that described separating layer 02 breaks away from described housing 3; Wherein, described detecting module 2 is connected with described processor 1, is used for surveying in predefined spy journey and result of detection being sent to described receipts processor 1; Described detecting module 2 is radar or camera.In the present embodiment, 2 of described detection moulds are radar.
Hatch 31 is used for discharging described bait thing 01, is arranged on close described bait thing 01 place of described housing 3, and described hatch 31 is connected with described processor 1 by second switch 72; Described processor 1 is controlled described second switch 72 closures according to the result of detection that has the interceptor target in the predetermined spy journey that receives and then is controlled described hatch 31 and open.
Described at least one bait thing 01, when described hatch 31 was opened, at least one described bait thing 01 broke away from described housing 3; Wherein, the size of described aerostat is identical with the described anti-interception flying object that has anti-laser strike, release bait thing and can separate with shape, and in the present embodiment, described bait thing 01 is 1 bait decoy warhead.Described separating layer 02 is arranged on the skin of described housing 3; Described processor 1 is controlled described the 3rd switch 73 closures and then is separated described separating layer 02 according to the result of detection that receives when having detected target; Described protective layer 8 covers the skin of described separating layer 02, reflects away for the light that will shine described separating layer 02; Described protective layer 8 is reflector layer, and described reflector layer is metal reflective layer or graphite reflector layer, and in the present embodiment, described protective layer 8 is one deck aluminium lamination.Described control system 9 is connected with described processor 1, is used for the flight track of this flying object of control.Described power supply 4 is used for giving above-mentioned each module for power supply.
The anti-interception flying object that has anti-laser strike, discharges the bait thing and can separate described in the utility model, comprise housing 3 and separating layer 02, and be arranged on processor 1, detecting module 2, hatch 31, power supply 4, at least one bait thing 01, protective layer 8, the control system 9 in the described housing 3 and control the 3rd switch 73 that described separating layer 02 breaks away from described housing 3; Described detecting module 2 is surveyed in predefined spy journey and result of detection is sent to described processor 1, when following the trail of this flying object of interception result of that probe is sent to described processor 1 when described detecting module 2 detects detection system in predefined spy journey, described processor 1 is controlled described the 3rd switch 73 closures and then is separated described separating layer 02 according to the result of detection that receives when having detected target; Simultaneously, described processor 1 is controlled described second switch 72 closures and then is controlled described hatch 31 and open, thereby discharges described bait thing 01.The bait decoy warhead has had the multifrequency nature of true bullet, as speed characteristics, infrared signature, radar reflect property, aerodynamic characteristic etc., be enough to mix the spurious with the genuine, the difficult real target of distinguishing of the sensor on the detection system, this mode is very big to the threat of detection system.
When laser detection system detects this flying object, during to this flying object emission laser, the aluminium lamination on this flying object separating layer 02 surface can reflect away the laser that shines described separating layer 02, thereby protects described flying object not destroyed, and the equipment in the described flying object does not damage; Simultaneously, described detecting module 2 is surveyed in predefined spy journey and result of detection is sent to described processor 1, when detecting detection system in predefined spy journey, detecting module 2 when following the trail of this flying object of interception, result of that probe is sent to described processor 1, described processor 1 transmits control signal to described control system 9, after described control system 9 receives the control signal of described processor 1 transmission, control this flying object and break away from original flight track, break away from the tracking interception of laser detection system.
Flying object can be any class in guided missile, aircraft, the aircraft.In the present embodiment, this flying object is guided missile.When following the trail of this guided missile of interception result of that probe is sent to described processor 1 when described detecting module 2 detects detection system in predefined spy journey, described processor 1 is controlled described the 3rd switch 73 closures and then is separated described separating layer 02 according to the result of detection that receives when having detected target; Simultaneously, described processor 1 is controlled described second switch 72 closures and then is controlled described hatch 31 and open, thereby discharges described bait thing 01.The bait decoy warhead has had the multifrequency nature of true bullet, as speed characteristics, infrared signature, radar reflect property, aerodynamic characteristic etc., be enough to mix the spurious with the genuine, the difficult real target of distinguishing of the sensor on the detection system, this mode is very big to the threat of detection system.
When laser detection system detects this guided missile, during to this MISSILE LAUNCHING laser, the aluminium lamination on this guided missile separating layer 02 surface can reflect away the laser that shines described separating layer 02, thereby protects described guided missile not destroyed, and the equipment in the described guided missile does not damage; Simultaneously, described detecting module 2 is surveyed in predefined spy journey and result of detection is sent to described processor 1, when detecting detection system in predefined spy journey, detecting module 2 when following the trail of this guided missile of interception, result of that probe is sent to described processor 1, described processor 1 transmits control signal to described control system 9, after described control system 9 receives the control signal of described processor 1 transmission, control this guided missile and break away from original flight track, break away from the tracking interception of laser detection system, finish the work thereby can successfully strike target.
As other embodiments, described bait decoy warhead quantity is more, and the sensor on the detection system is the more difficult real target of distinguishing in many objective bodies just, and this guided missile takes advantage of the occasion to escape under the shielding of bait thing.
As other embodiments, described bait thing 01 is aerostat or the chaff of spray metal film.
As other embodiments, aerostat and bait decoy warhead that described bait thing 01 is the spray metal film.
As other embodiments, described bait thing 01 is chaff and bait decoy warhead.
As other embodiments, described bait thing 01 is true bullet.When this guided missile in the enemy zone, discharge true bullet, hit target of attack.
As other embodiments, aerostat, bait decoy warhead and true bullet that described bait thing 01 is the spray metal film.This guided missile takes advantage of the occasion to escape under the shielding of the aerostat of spray metal film and bait decoy warhead.When this guided missile in the enemy zone, discharge true bullet, hit target of attack.
As other embodiments, described aluminium lamination can be multilayer, and after the aluminium lamination of outside melted owing to the laser irradiation, the light that adjacent aluminium lamination can continue will shine on the described housing 3 reflected away, the protection better effects if.
As other embodiments, described protective layer 8 has the metal metal reflective layer of reflective character for graphite reflector layer or other.
As other embodiments, described protective layer 8 is for arranging the polygon prism layer that arranges.
As other embodiments, described protective layer 8 is the outer field reflector layer that covers described housing 3 and the polygon prism layer that is arranged on the described reflector layer skin.
As other embodiments, the outer surface of described housing 3 also arranges layer protective layer, described separating layer 02 is with after described housing 3 separates, when laser detection system detects this guided missile, during to this MISSILE LAUNCHING laser, the protective layer of described housing 3 outer surfaces of this guided missile can reflect away the laser that shines described housing 3, thereby protects described guided missile not destroyed, and the equipment in the described guided missile does not damage; Simultaneously, described detecting module 2 is surveyed in predefined spy journey and result of detection is sent to described processor 1, when detecting detection system in predefined spy journey, detecting module 2 when following the trail of this guided missile of interception, result of that probe is sent to described processor 1, described processor 1 transmits control signal to described control system 9, after described control system 9 receives the control signal of described processor 1 transmission, control this guided missile and break away from original flight track, break away from the tracking interception of laser detection system.
Embodiment 2:
Referring to shown in Figure 2, on the basis of embodiment 1, described guided missile also comprises startup control module 11, link to each other with described processor 1, when not arriving, entry condition controls described processor 1 dormancy, and when entry condition arrives, control described processor 1 and start working, described entry condition comprises predetermined time or predetermined geographical position; In the present embodiment, described startup control module 11 is timer, and when described timer timing reached predetermined time, described timer was controlled described processor 1 and started working, otherwise described timer is controlled described processor 1 dormancy.
Anti-interception guided missile described in the utility model also comprises starting control module 11, links to each other with described processor 1, controls described processor 1 dormancy when entry condition does not arrive, and controls described processor 1 and start working when entry condition arrives.If the flying distance of this guided missile is short, described processor 1 can be in running order always, but when flying distance is long, if described processor 1 is in running order always, described power supply 4 can exhaust in the flight way, described processor 1 can not carry out work, and this guided missile can't break away from when running into the tracking interception.Described startup control module 11 is set in guided missile, before the flight prerequisite, entry condition is set, when beginning to fly, described processor 1 resting state of described startup control module 11 controls, when entry condition arrived, the described processor 1 of described startup control module 11 controls was started working, and this mode can guarantee that guided missile is long in flying distance, described processor 1 also can be worked when running into the interception tracking, and power consumption was little when described processor 1 was in dormancy, energy-conserving and environment-protective.
Obviously, above-described embodiment only is for example clearly is described, and is not the restriction to embodiment.For those of ordinary skill in the field, can also make other changes in different forms on the basis of the above description.Here need not also can't give all embodiments exhaustive.And the apparent variation of being extended out thus or change still are among the protection domain of the invention.
Claims (10)
1. one kind has the anti-interception flying object that anti-laser hits, discharges the bait thing and can separate, and it is characterized in that, comprise,
Housing and separating layer,
And be arranged on the 3rd switch that processor, detecting module, power supply, at least one bait thing, protective layer, control system and the described separating layer of control in the described housing breaks away from described housing;
Wherein,
Described detecting module is connected with described processor, is used for surveying in predefined spy journey and result of detection being sent to described processor;
Hatch is used for discharging described bait thing, is arranged on the close described bait thing place of described housing, and described hatch is connected with described processor by second switch; Described processor is controlled described second switch closure according to the result of detection that receives and then is controlled described hatch and open;
At least one bait thing, when described hatch was opened, at least one described bait thing broke away from described housing;
Described separating layer is arranged on the skin of described housing; Described processor is controlled described the 3rd switch closure and then is separated described separating layer according to the result of detection that receives when having detected target;
Protective layer covers the skin of described separating layer, and the light that is used for shining described separating layer reflects away;
Control system is connected with described processor, is used for the flight track of this flying object of control;
Described power supply is used for giving above-mentioned each module for power supply.
2. the anti-interception flying object that has anti-laser strike, discharges the bait thing and can separate according to claim 1 is characterized in that,
The aerostat that described bait thing is the spray metal film and/or bait decoy warhead and/or true bullet.
3. the anti-interception flying object that has anti-laser strike, discharges the bait thing and can separate according to claim 1 and 2 is characterized in that,
Described the 3rd switch is arranged in the described housing, and described separating layer is provided with separates executing agency, and when described the 3rd switch closure, the action of described separation executing agency drives described separating layer and breaks away from described housing.
4. according to claim 3 have an anti-interception flying object that anti-laser hits, discharges the bait thing and can separate, and it is characterized in that, described separation executing agency is priming device.
5. the anti-interception flying object that has anti-laser strike, discharges the bait thing and can separate according to claim 4 is characterized in that described priming device is electric cap.
6. the anti-interception flying object that has anti-laser strike, discharges the bait thing and can separate according to claim 5 is characterized in that, described protective layer is reflector layer or arranges the polygon prism layer that arranges.
7. the anti-interception flying object that has anti-laser strike, discharges the bait thing and can separate according to claim 5 is characterized in that, described protective layer is the outer field reflector layer and the polygon prism layer that is arranged on the described reflector layer skin that covers described separating layer.
8. according to claim 6 or the 7 described anti-interception flying objects that have anti-laser strike, discharge the bait thing and can separate, it is characterized in that described reflector layer is metal reflective layer or graphite reflector layer.
9. according to claim 8 have an anti-interception flying object that anti-laser hits, discharges the bait thing and can separate, it is characterized in that, also comprise the startup control module, link to each other with described processor, when entry condition does not arrive, control described processor dormancy, and when entry condition arrives, control described processor and start working; Described entry condition is predetermined time or predetermined geographical position.
10. according to claim 9 have an anti-interception flying object that anti-laser hits, discharges the bait thing and can separate, it is characterized in that, described startup control module is timer, when described timer timing reaches predetermined time, described startup control module is controlled described processor and is started working, otherwise described startup control module is controlled described processor dormancy.
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| CN 201320068445 CN203116621U (en) | 2013-02-05 | 2013-02-05 | Detachable anti-intercept and anti-laser-attack flyer capable of releasing bait object |
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| CN 201320068445 CN203116621U (en) | 2013-02-05 | 2013-02-05 | Detachable anti-intercept and anti-laser-attack flyer capable of releasing bait object |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103075928A (en) * | 2013-02-05 | 2013-05-01 | 王海龙 | Anti-interception flyer with functions of resisting laser attack, releasing bait object and separating |
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2013
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103075928A (en) * | 2013-02-05 | 2013-05-01 | 王海龙 | Anti-interception flyer with functions of resisting laser attack, releasing bait object and separating |
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