CN103075921B - There is the anti-interception flying object of anti-laser hits, release bait object function - Google Patents
There is the anti-interception flying object of anti-laser hits, release bait object function Download PDFInfo
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- CN103075921B CN103075921B CN201310045402.9A CN201310045402A CN103075921B CN 103075921 B CN103075921 B CN 103075921B CN 201310045402 A CN201310045402 A CN 201310045402A CN 103075921 B CN103075921 B CN 103075921B
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- 238000001514 detection method Methods 0.000 claims abstract description 44
- 239000011241 protective layer Substances 0.000 claims abstract description 18
- 239000010410 layer Substances 0.000 claims description 26
- 230000005059 dormancy Effects 0.000 claims description 10
- 239000004411 aluminium Substances 0.000 claims description 8
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical group [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 8
- 229910052782 aluminium Inorganic materials 0.000 claims description 8
- 238000003475 lamination Methods 0.000 claims description 8
- 238000007599 discharging Methods 0.000 claims description 6
- 239000011104 metalized film Substances 0.000 claims description 6
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims description 4
- 239000010439 graphite Substances 0.000 claims description 4
- 229910002804 graphite Inorganic materials 0.000 claims description 4
- 239000000523 sample Substances 0.000 abstract description 6
- 230000005540 biological transmission Effects 0.000 abstract description 4
- 238000005516 engineering process Methods 0.000 description 13
- 238000000034 method Methods 0.000 description 3
- 230000018109 developmental process Effects 0.000 description 2
- 230000007123 defense Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000012530 fluid Substances 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 239000000155 melt Substances 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 230000003287 optical effect Effects 0.000 description 1
- 230000007903 penetration ability Effects 0.000 description 1
- 230000000284 resting effect Effects 0.000 description 1
- 230000007958 sleep Effects 0.000 description 1
- 230000004083 survival effect Effects 0.000 description 1
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Abstract
The anti-interception flying object with anti-laser hits, release bait object function of the present invention; comprise processor, detecting module, housing, power supply, protective layer, control system, hatch and at least one bait object; when described detecting module detects detection system at this flying object of pursuit and interception in the spy journey preset, result of that probe is sent to processor, it is closed and then control hatch and open and discharge described bait object that processor controls second switch.When laser detection system detects this flying object, during to this flying object Emission Lasers, the laser reflection being irradiated to housing can be gone out by the protective layer of this flying object case surface, thus protects described flying object not destroyed, and the equipment in described flying object does not damage; Meanwhile, processor transmits control signal to control system, and control system controls this flying object and departs from original flight track after receiving the control signal of processor transmission, departs from the pursuit and interception of laser detection system.
Description
Technical field
The present invention relates to a kind of anti-Antimissile Technology, specifically a kind of have anti-laser hits, release bait object function anti-interception flying object, belong to space flight technical field.
Background technology
At present, space exploration mainly contains the various scouting Detection Techniques such as radar detection, visible ray detection, laser acquisition, infrared acquisition, acoustic detection, for detection and discovery airflight thing, correspondingly the anti-Detection Techniques means in space are also given tit for tat, use various anti-detection method to realize airflight thing not found by various Detection Techniques means, thus can safe flight.
Along with advancing by leaps and bounds of modern science, sound, optical, electrical, 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 grown up in Detection Techniques and anti-Detection Techniques progress, stealth technology is otherwise known as stealth technique, refer to the various detectable feature reducing target, make enemy's detecting devices be difficult to the integrated technology finding or the detectivity of enemy's detecting devices is reduced.Stealth technology is the cross-application technology of the multiple subject technologies such as integrated fluid dynamics, material science, electronics, optics, acoustics, by changing the detectable information characteristics of target, enemy's detection system is not easily found or detective distance shorten complex art, be development and the extension of conventional camouflage technological direction high-tech.Modern Stealth Technique, as the effective means improving armament systems survival ability and penetration ability, is subject to the great attention of each main military country of the world.
But detection system utilizes Detection Techniques once detect airflight thing, just carries out pursuit and interception to airflight thing, until tackle successfully to described airflight thing, cause the failure of this airflight thing goal task.
Laser has high energy, high focusing, the advantages such as high speed, and current many countries are developing superlaser equipment energetically, destroy airflight thing, thus tackle successfully airflight thing with laser high temperature.
Summary of the invention
To be solved by this invention is that in prior art, aerial flyer is detected system looks and tackles the technical problem that cannot depart to rear laser traces, thus provide a kind of can the flying object of backward-reflected laser interception.
For solving the problems of the technologies described above, the present invention is achieved by the following technical solutions:
Have anti-laser hits, release bait object function an anti-interception flying object, comprise
Processor;
Detecting module, is connected with described processor, for carrying out detecting in the spy journey preset and result of detection being sent to received processor;
Housing, for the protection of fixing described processor, described detecting module and described power supply;
Protective layer, covers the skin of described housing, for being reflected away by the light being irradiated to described housing;
Control system, is connected with described processor, for controlling the flight track of this flying object;
Hatch, for discharging described bait object, be arranged on the close described bait object place of described housing, described hatch is connected with described processor by second switch; It is closed and then control described hatch and open that described processor controls described second switch according to the result of detection received;
At least one bait object described, when described hatch is opened, bait object described at least one departs from described housing;
Power supply, powers for giving described processor, described detecting module and described control system.
Described have anti-laser hits, release bait object function anti-interception flying object, described protective layer is reflector layer.
Described have anti-laser hits, release bait object function anti-interception flying object, described protective layer is the polygon prism layer of spread configuration.
Described have anti-laser hits, release bait object function anti-interception flying object, described protective layer is the outer field reflector layer covering described housing and the polygon prism layer be arranged on described reflector layer skin.
Described have anti-laser hits, release bait object function anti-interception flying object, described reflector layer is metallic reflective layer or graphite reflector layer.
Described have anti-laser hits, release bait object function anti-interception flying object, described metallic reflective layer is aluminium lamination.
Described have anti-laser hits, release bait object function anti-interception flying object, described bait object is aerostat and or bait decoy warhead and or the true bullet of metallized films.
Described have anti-laser hits, release bait object function anti-interception flying object, also comprise startup control unit, be connected with described processor, control described processor dormancy when entry condition does not arrive, and control described processor when entry condition arrives and start working.
Described have anti-laser hits, release bait object function anti-interception flying object, described entry condition is predetermined time or predetermined geographical position.
Described have anti-laser hits, release bait object function anti-interception flying object, described startup control unit is timer, when reaching predetermined time when described timer, described startup control unit controls described processor and starts working, otherwise described startup control unit controls described processor dormancy.
Technique scheme of the present invention has the following advantages compared to existing technology:
(1) of the present invention have anti-laser hits, release bait object function anti-interception flying object; comprise processor, detecting module, housing, power supply, protective layer, control system, hatch and at least one bait object; when described detecting module detects detection system at this flying object of pursuit and interception in the spy journey preset, result of that probe is sent to described processor; it is closed and then control described hatch and open that described processor controls described second switch according to the result of detection received, thus discharge described bait object.When laser detection system detects this flying object, during to this flying object Emission Lasers, the laser reflection being irradiated to described housing can be gone out by the protective layer of this flying object case surface, thus protects described flying object not destroyed, and the equipment in described flying object does not damage; Simultaneously, described detecting module carries out detecting and result of detection is sent to described processor in the spy journey preset, when detecting module detects detection system at this flying object of pursuit and interception in the spy journey preset, 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 depart from original flight track, depart from the pursuit and interception of laser detection system.
(2) of the present invention have anti-laser hits, release bait object function anti-interception flying object, also comprise startup control unit, be connected with described processor, control described processor dormancy when entry condition does not arrive, and control described processor when entry condition arrives and start working.If the flying distance of this flying object is short, processor can be always in running order, but when flying distance is long, if processor is always in running order, power supply can exhaust in flight way, and processor can not carry out work, this flying object, when running into pursuit and interception, cannot depart from.Startup control unit is set in flying object, before flight prerequisite, entry condition is set, when starting to fly, start control unit and control described processor sleep state, when entry condition arrives, start control unit control processor and start working, this mode can ensure that flying object is longer in flying distance, run into processor when interception is followed the trail of and also can work, and when processor is in dormancy, power consumption is little, energy-conserving and environment-protective.
Accompanying drawing explanation
In order to make content of the present invention be more likely to be clearly understood, below in conjunction with accompanying drawing, the present invention is further detailed explanation, wherein,
Fig. 1 is the structural representation of the anti-interception flying object discharging smog described in the embodiment of the present invention 1;
Fig. 2 is the structural representation of the anti-interception flying object discharging smog described in the embodiment of the present invention 2.
In figure, Reference numeral is expressed as: 01-bait object, 1-processor, and 11-starts control unit, 2-detecting module, 3-housing, 31-hatch, 4-power supply, 72-second switch, 8-protective layer, 9-control system.
Detailed description of the invention
Embodiment 1:
Of the present invention have anti-laser hits, release bait object function anti-interception flying object structure as shown in Figure 1, it comprises processor 1, detecting module 2, housing 3, power supply 4, protective layer 8, control system 9, hatch 31 and at least one bait object 01; Wherein, described detecting module 2 is connected with described processor 1, for carrying out detecting in the spy journey preset and result of detection being sent to described processor 1; Described detecting module 2 is radar or camera.In the present embodiment, described detection mould 2 pieces is radar.Described power supply 4 is powered for giving described processor 1, described detecting module 2 and described control system 9.Described housing 3 is for the protection of fixing described processor 1, described detecting module 2 and described power supply 4; Protective layer 8 covers the skin of described housing 3, for being reflected away by the light being irradiated to described housing 3.Described protective layer 8 is reflector layer, and described reflector layer is metallic 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, for controlling the flight track of this flying object.Described hatch 31 is for discharging described bait object 01, and be arranged on close described bait object 01 place of described housing 3, described hatch 31 is connected with described processor 1 by second switch 72; It is closed and then control described hatch 31 and open that described processor 1 controls described second switch 72 according to the result of detection received.Bait object 01 described at least one, when described hatch 31 is opened, bait object 01 described at least one departs from described housing 3, and in the present embodiment, described bait object 01 is 1 bait decoy warhead.Described power supply 4 is powered for giving described processor 1, described detecting module 2 and described control system 9.
When described detecting module 2 detects detection system at this flying object of pursuit and interception in the spy journey preset, result of that probe is sent to described processor 1, it is closed and then control described hatch 31 and open that described processor 1 controls described second switch 72 according to the result of detection received, thus discharge described bait object 01.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 sensor difficulty in detection system distinguishes real target, and this mode is very large to the threat of detection system.
When laser detection system detects this flying object, during to this flying object Emission Lasers, the laser reflection being irradiated to described housing 3 can be gone out by the aluminium lamination of this flying object case surface, thus protects described flying object not destroyed, and the equipment in described flying object does not damage; Simultaneously, described detecting module 2 carries out detecting and result of detection is sent to described processor 1 in the spy journey preset, when detecting module 2 detects detection system at this flying object of pursuit and interception in the spy journey preset, 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 depart from original flight track, depart from the pursuit and interception of laser detection system.
Flying object can be any class in guided missile, aircraft, aircraft.In the present embodiment, described flying object is guided missile.Result of that probe is sent to described processor 1 when described detecting module 2 detects detection system at pursuit and interception guided missile in the spy journey preset, it is closed and then control described hatch 31 and open that described processor 1 controls described second switch 72 according to the result of detection received, thus discharging described bait object 01, guided missile takes advantage of the occasion to depart from detection system.When laser detection system detects guided missile, during to guided missile Emission Lasers, the laser reflection being irradiated to described housing 3 can be gone out by the aluminium lamination on tub surface, thus protects described guided missile not destroyed, and the equipment in described guided missile does not damage; Simultaneously, 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 depart from original flight track, depart from the pursuit and interception of laser detection system, and then proceed task, until task completes, successfully strike target.
As other embodiments, described aluminium lamination can be multilayer, and after the aluminium lamination of outside melts because laser irradiates, adjacent aluminium lamination can continue the light be irradiated on described housing 3 to reflect away, and protected effect is better.
As other embodiments, described protective layer 8 be graphite reflector layer or other there is the metal metallic reflective layer of reflective character.
As other embodiments, described protective layer 8 is the polygon prism layer of spread configuration.
As other embodiments, described protective layer 8 is for covering the outer field reflector layer of described housing 3 and the polygon prism layer be arranged on described reflector layer skin.
As other embodiments, described bait decoy warhead quantity is more, and the sensor in detection system is the more difficult real target distinguished in many objective bodies just, and this flying object takes advantage of the occasion to escape under the shielding of bait object.
As other embodiments, described bait object 01 is aerostat or the chaff of metallized films.
As other embodiments, described bait object 01 is aerostat and the bait decoy warhead of metallized films.
As other embodiments, described bait object 01 is chaff and bait decoy warhead.
As other embodiments, described bait object 01 is true bullet.When this flying object is in hostile area, discharge true bullet, hit target of attack.
As other embodiments, described bait object 01 is the aerostat of metallized films, bait decoy warhead and true bullet.This flying object takes advantage of the occasion to escape under the aerostat of metallized films and the shielding of bait decoy warhead.When this flying object is in hostile area, discharge true bullet, hit target of attack.
Embodiment 2:
Shown in Figure 2, on the basis of embodiment 1, described flying object also comprises startup control unit 11, be connected with described processor 1, the dormancy of described processor 1 is controlled when entry condition does not arrive, and control described processor 1 when entry condition arrives and start working, described entry condition comprises predetermined time or predetermined geographical position; In the present embodiment, described startup control unit 11 is timer, and when reaching predetermined time when described timer, described timer controls described processor 1 and starts working, otherwise described timer controls the dormancy of described processor 1.
Of the present invention have anti-laser hits, release bait object function anti-interception flying object, also comprise and start control unit 11, be connected with described processor 1, control the dormancy of described processor 1 when entry condition does not arrive, and control described processor 1 when entry condition arrives and start working.If the flying distance of this flying object is short, described processor 1 can be always in running order, but when flying distance is long, if described processor 1 is always in running order, described power supply 4 can exhaust in flight way, described processor 1 can not carry out work, and this flying object, when running into pursuit and interception, cannot depart from.Described startup control unit 11 is set in flying object, before flight prerequisite, entry condition is set, when starting to fly, described startup control unit 11 controls described processor 1 resting state, when entry condition arrives, described startup control unit 11 controls described processor 1 and starts working, and this mode can ensure that flying object is longer in flying distance, run into described processor 1 when interception is followed the trail of and also can work, and when described processor 1 is in dormancy, power consumption is little, energy-conserving and environment-protective.
Obviously, above-described embodiment is only for clearly example being described, and the restriction not 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 exhaustive without the need to also giving all embodiments.And thus the apparent change of extending out or variation be still among the protection domain of the invention.
Claims (5)
1. there is an anti-interception flying object for anti-laser hits, release bait object function, it is characterized in that, comprise
Processor;
Detecting module, is connected with described processor, for carrying out detecting in the spy journey preset and result of detection being sent to described processor;
Housing, for the protection of fixing described processor, described detecting module and power supply;
Protective layer, covers the skin of described housing, and for being reflected away by the light being irradiated to described housing, described protective layer is the outer field reflector layer covering described housing and the polygon prism layer be arranged on described reflector layer skin;
Control system, is connected with described processor, for controlling the flight track of this flying object;
Hatch, for discharging described bait object, be arranged on the close described bait object place of described housing, described hatch is connected with described processor by second switch; It is closed and then control described hatch and open that described processor controls described second switch according to the result of detection received;
Bait object described at least one, when described hatch is opened, bait object described at least one departs from described housing, and described bait object is the aerostat of metallized films and/or bait decoy warhead and/or true bullet;
Described power supply, powers for giving described processor, described detecting module and described control system;
Also comprise startup control unit, be connected with described processor, control described processor dormancy when entry condition does not arrive, and control described processor when entry condition arrives and start working.
2. the anti-interception flying object with anti-laser hits, release bait object function according to claim 1, it is characterized in that, described reflector layer is metallic reflective layer or graphite reflector layer.
3. the anti-interception flying object with anti-laser hits, release bait object function according to claim 2, it is characterized in that, described metallic reflective layer is aluminium lamination.
4. the anti-interception flying object with anti-laser hits, release bait object function according to claim 1, it is characterized in that, described entry condition is predetermined time or predetermined geographical position.
5. the anti-interception flying object with anti-laser hits, release bait object function according to claim 4, it is characterized in that, described startup control unit is timer, when reaching predetermined time when described timer, described startup control unit controls described processor and starts working, otherwise described startup control unit controls described processor dormancy.
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| CN201310045402.9A CN103075921B (en) | 2013-02-05 | 2013-02-05 | There is the anti-interception flying object of anti-laser hits, release bait object function |
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| CN201310045402.9A CN103075921B (en) | 2013-02-05 | 2013-02-05 | There is the anti-interception flying object of anti-laser hits, release bait object function |
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| CN103075921A CN103075921A (en) | 2013-05-01 |
| CN103075921B true CN103075921B (en) | 2015-12-30 |
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Citations (3)
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|---|---|---|---|---|
| FR2721996A1 (en) * | 1994-06-29 | 1996-01-05 | Perin Gerald | Missile able to confront defensive armaments as laser guided missile |
| CN201242408Y (en) * | 2008-05-21 | 2009-05-20 | 卢振东 | Multi-warhead guided missile of sub-gasbag-loaded interceptor missile |
| CN203083455U (en) * | 2013-02-05 | 2013-07-24 | 王海龙 | Anti-interception flyer having functions of resisting laser irradiation and releasing bait materials |
Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN100428672C (en) * | 2004-08-09 | 2008-10-22 | 电子科技大学 | Device and method for realizing remote control dormancy and wake-up in radio network |
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2013
- 2013-02-05 CN CN201310045402.9A patent/CN103075921B/en active Active
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2721996A1 (en) * | 1994-06-29 | 1996-01-05 | Perin Gerald | Missile able to confront defensive armaments as laser guided missile |
| CN201242408Y (en) * | 2008-05-21 | 2009-05-20 | 卢振东 | Multi-warhead guided missile of sub-gasbag-loaded interceptor missile |
| CN203083455U (en) * | 2013-02-05 | 2013-07-24 | 王海龙 | Anti-interception flyer having functions of resisting laser irradiation and releasing bait materials |
Non-Patent Citations (1)
| Title |
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| 激光反导与导弹反激光措施综述;宋亚萍等;《激光与红外》;20081031;第38卷(第10期);第969页 * |
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Effective date of registration: 20181009 Address after: 215200 No. 1188 west two ring road, Shengze Town, Wujiang District, Suzhou, Jiangsu. Patentee after: Suzhou Shengze science and Technology Pioneer Park Development Co., Ltd. Address before: 215228 10, Wujiang Textile Science and Technology Pioneer Park, 1188, west two ring road, Shengze Town, Wujiang, Suzhou. Patentee before: Relax and suitable new textile material Science and Technology Ltd. in Suzhou |
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