CN203083457U - Anti-interception flyer having function of resisting laser irradiation - Google Patents
Anti-interception flyer having function of resisting laser irradiation Download PDFInfo
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- CN203083457U CN203083457U CN 201320068224 CN201320068224U CN203083457U CN 203083457 U CN203083457 U CN 203083457U CN 201320068224 CN201320068224 CN 201320068224 CN 201320068224 U CN201320068224 U CN 201320068224U CN 203083457 U CN203083457 U CN 203083457U
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Abstract
The utility model relates to an anti-interception flyer having the function of resisting laser irradiation, which comprises a processor, a detection module, a shell, a power supply, a protective layer and a track control system, wherein when a laser detection system detects the flyer and emits laser to the flyer, the protective layer on the surface of the flyer shell can reflect laser irradiated on the shell, therefore, the flyer cannot be destroyed and equipment in the flyer cannot be damaged; simultaneously, the detection module is used for detecting in a pre-set detection range and sending a detection result to the processor; and in the event of detecting that the flyer is tracked and intercepted by a detection system in the pre-set detection range, the detection module sends the detection result to the processor, the processor sends control signals to the track control system, and after receiving the control signals sent by the processor, the track control system controls the flyer to be separated from an original flying track, therefore, the flyer cannot be tracked and intercepted by 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 function 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 the 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, be meant the various detectable feature that reduces 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 detection system utilizes Detection Techniques in a single day to detect the airflight thing, just the airflight thing is followed the trail of interception, until described airflight thing is tackled successfully, causes the failure of this airflight thing goal task.
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 that aerial flyer is detected system and detects the back and follow the trail of the technical problem that interception can't break away from laser in the prior art, thereby a kind of flying object that can the backward-reflected laser interception is provided.
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 with anti-laser strike function comprises
Processor;
Detecting module is connected with described processor, is used for surveying in predefined spy journey and result of detection being sent to described processor;
Housing is used for protection and fixing described processor, described detecting module and described power supply;
Protective layer covers the skin of described housing, and the light that is used for shining described housing reflects away;
Control system is connected with described processor, is used to control the flight track of this flying object;
Power supply is used for to described processor, described detecting module and the power supply of described control system.
Described anti-interception flying object with anti-laser strike function, described protective layer is a reflector layer.
Described anti-interception flying object with anti-laser strike function, described protective layer is for arranging the polygon prism layer that is provided with.
Described anti-interception flying object with anti-laser strike function, 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 housing.
Described anti-interception flying object with anti-laser strike function, described reflector layer is metal reflective layer or graphite reflector layer.
Described anti-interception flying object with anti-laser strike function, described metal reflective layer is an aluminium lamination.
Described anti-interception flying object with anti-laser strike function also comprises the start-up control unit, links to each other with described processor, controls described processor dormancy when entry condition does not arrive, and controls described processor and start working when entry condition arrives.
Described anti-interception flying object with anti-laser strike function, described entry condition is preset time or predetermined geographical position.
Described anti-interception flying object with anti-laser strike function, described start-up control unit is a timer, and when described timer timing reached preset time, the described processor of described start-up control unit controls was started working, otherwise, the described processor dormancy of described start-up control unit controls.
Described anti-interception flying object with anti-laser strike function, described detecting module is radar or camera.
Technique scheme of the present utility model has the following advantages compared to existing technology:
(1) the anti-interception flying object with anti-laser strike function described in the utility model, comprise processor, detecting module, housing, power supply, protective layer and control system, when laser detection system detects this flying object, when this flying object emission laser, the protective layer of this flying object surface of shell can reflect away the laser that shines described housing, thereby protect described flying object not destroyed, 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 with anti-laser strike function described in the utility model, also comprise the start-up control unit, 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 start-up control unit is set in flying object, before the flight prerequisite, entry condition is set, when beginning to fly, the described processor sleep state of start-up control unit controls, when entry condition arrived, start-up control unit controls processor was started working, and 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
For the easier quilt of content of the present utility model is clearly understood, below in conjunction with accompanying drawing, the utility model is described in further detail, wherein,
Fig. 1 is the structural representation of the anti-interception flying object of the utility model embodiment 1 described release smog;
Fig. 2 is the structural representation of the anti-interception flying object of the utility model embodiment 2 described release smog.
Reference numeral is expressed as among the figure: 1-processor, 11-start-up control unit, 2-detecting module, 3-housing, 4-power supply, 8-protective layer, 9-control system.
The specific embodiment
Embodiment 1:
Described in the utility model have anti-laser hit 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 and control system 9; 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 processor 1; Described detecting module 2 is radar or camera.In the present embodiment, 2 of described detection moulds are radar.Described power supply 4 is used for to described processor 1, described detecting module 2 and 9 power supplies of described control system.Described housing 3 is used for protection and fixing described processor 1, described detecting module 2 and described power supply 4; Protective layer 8 covers the skin of described housing 3, and the light that is used for shining described housing 3 reflects away.Described protective layer 8 is a 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 to control the flight track of this flying object.Described power supply 4 is used for to described processor 1, described detecting module 2 and 9 power supplies of described control system.
When laser detection system detects this flying object, when this flying object emission laser, the aluminium lamination on these flying object housing 3 surfaces can reflect away the laser that shines described housing 3, 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, described flying object is a guided missile.When detecting interception target 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, the control guided missile breaks away from original flight track, thereby the tracking interception that breaks away from laser detection system, continue to carry out aerial mission, finally this guided missile can hit the other side, finishes the work.
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 is provided with.
As other embodiments, described protective layer 8 is outer field reflector layer that covers described housing 3 and the polygon prism layer that is arranged on the described reflector layer skin.
Embodiment 2:
Referring to shown in Figure 2, on the basis of embodiment 1, described flying object also comprises start-up control unit 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 preset time or predetermined geographical position; In the present embodiment, described start-up control unit 11 is a timer, and when described timer timing reached preset time, described timer was controlled described processor 1 and started working, otherwise described timer is controlled described processor 1 dormancy.
Anti-interception flying object with anti-laser strike function described in the utility model, also comprise start-up control unit 11, link to each other with described processor 1, when entry condition does not arrive, control described processor 1 dormancy, and when entry condition arrives, control described processor 1 and start working.If the flying distance of this flying object 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 flying object can't break away from when running into the tracking interception.Described start-up control unit 11 is set in flying object, before the flight prerequisite, entry condition is set, when beginning to fly, described processor 1 resting state of described start-up control unit 11 controls, when entry condition arrived, the described start-up control unit described processor 1 of 11 controls was started working, and this mode can guarantee that flying object 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, the foregoing description only is for example clearly is described, and is not the qualification 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 exhaustive to all embodiments.And conspicuous 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 function, it is characterized in that, comprises
Processor;
Detecting module is connected with described processor, is used for surveying in predefined spy journey and result of detection being sent to described processor;
Housing is used for protection and fixing described processor, described detecting module and described power supply;
Protective layer covers the skin of described housing, and the light that is used for shining described housing reflects away;
Control system is connected with described processor, is used to control the flight track of this flying object;
Power supply is used for to described processor, described detecting module and the power supply of described control system.
2. the anti-interception flying object with anti-laser strike function according to claim 1 is characterized in that described protective layer is a reflector layer.
3. the anti-interception flying object with anti-laser strike function according to claim 1 is characterized in that described protective layer is for arranging the polygon prism layer that is provided with.
4. the anti-interception flying object with anti-laser strike function according to claim 1 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 housing.
5. according to claim 2 or 4 described anti-interception flying objects, it is characterized in that described reflector layer is metal reflective layer or graphite reflector layer with anti-laser strike function.
6. the anti-interception flying object with anti-laser strike function according to claim 5 is characterized in that described metal reflective layer is an aluminium lamination.
7. the anti-interception flying object with anti-laser strike function according to claim 6 is characterized in that,
Also comprise the start-up control unit, link to each other, when entry condition does not arrive, control described processor dormancy, and when entry condition arrives, control described processor and start working with described processor.
8. the anti-interception flying object with anti-laser strike function according to claim 7 is characterized in that described entry condition is preset time or predetermined geographical position.
9. the anti-interception flying object with anti-laser strike function according to claim 8, it is characterized in that, described start-up control unit is a timer, when described timer timing reaches preset time, the described processor of described start-up control unit controls is started working, otherwise, the described processor dormancy of described start-up control unit controls.
10. the anti-interception flying object with anti-laser strike function according to claim 9 is characterized in that described detecting module is radar or camera.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201320068224 CN203083457U (en) | 2013-02-05 | 2013-02-05 | Anti-interception flyer having function of resisting laser irradiation |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201320068224 CN203083457U (en) | 2013-02-05 | 2013-02-05 | Anti-interception flyer having function of resisting laser irradiation |
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| Publication Number | Publication Date |
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| CN203083457U true CN203083457U (en) | 2013-07-24 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN 201320068224 Expired - Lifetime CN203083457U (en) | 2013-02-05 | 2013-02-05 | Anti-interception flyer having function of resisting laser irradiation |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103075925A (en) * | 2013-02-05 | 2013-05-01 | 王海龙 | Anti-interception flyer with laser attack resistance function |
-
2013
- 2013-02-05 CN CN 201320068224 patent/CN203083457U/en not_active Expired - Lifetime
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103075925A (en) * | 2013-02-05 | 2013-05-01 | 王海龙 | Anti-interception flyer with laser attack resistance function |
| CN103075925B (en) * | 2013-02-05 | 2015-12-30 | 王海龙 | There is the anti-interception flying object of anti-laser hits function |
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| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| AV01 | Patent right actively abandoned |
Granted publication date: 20130724 Effective date of abandoning: 20151230 |
|
| C25 | Abandonment of patent right or utility model to avoid double patenting |