CN203069059U - Anti-interception flying object with smog releasing function - Google Patents
Anti-interception flying object with smog releasing function Download PDFInfo
- Publication number
- CN203069059U CN203069059U CN 201320066762 CN201320066762U CN203069059U CN 203069059 U CN203069059 U CN 203069059U CN 201320066762 CN201320066762 CN 201320066762 CN 201320066762 U CN201320066762 U CN 201320066762U CN 203069059 U CN203069059 U CN 203069059U
- Authority
- CN
- China
- Prior art keywords
- processor
- smog
- flying object
- module
- described processor
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
Images
Landscapes
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
The utility model discloses an anti-interception flying object with a smog releasing function, which comprises a processor, a detection module, a release module, a housing, an induction device and a power source, wherein a hatchway is arranged on the housing in the position close to the release module and is connected with the processor through a second switch; the detection module performs detection in a predetermined detection range and the detection result is sent to the processor; when the detection module detects that a detection system is tracking and intercepting the flying object, the detection result is sent to the processor; on the basis of the result, the processor controls a first switch to close so as to allow the release module to release the smog; when the induction device inducts the smog in the housing, the induction result is sent to the processor; on the base of the result, the processor controls the second switch to close so as to open the hatchway, and the smog is released out to confuse the detection system of tracking and intercepting, so as to disturb the results of an optical observation instrument of the detection system, and accordingly, the flying object can escape under the cover of the smog.
Description
Technical field
The utility model relates to a kind of counnter attack waveguide technology, specifically is the anti-flying object of tackling of a kind of release smog, 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 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.
The utility model content
To be solved in the utility model is the technical problem that can't break away from after aerial flyer is detected system and detects in the prior art, thus the anti-interception flying object that can break away from after providing a kind of detection system to detect.
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 release smog 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;
Release module, be used for discharging smog, described release module links to each other with described processor via first switch, and described processor exists the result of detection of interceptor target to control described first switch closure and then control described release module work according in the predetermined spy journey that receives;
Housing, described housing is provided with hatch near described release module place, is used for discharging the described smog that described release module discharges, and described hatch is connected with described processor by second switch;
Induction installation, be connected with described processor, be used in the described housing of induction whether described smog being arranged, and will respond to the result and send to described processor, described processor is controlled described second switch closure according to described induction result and then is controlled described hatch and open when having sensed smog;
Power supply is used for giving described processor, detecting module, release module and the power supply of described induction installation.
Described anti-interception flying object, described release module is aerosol bomb.
Described anti-interception flying object, described aerosol bomb are the aerosol bomb that dry ice is made.
Described anti-interception flying object also comprises the startup control module, 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, described entry condition comprises predetermined time or predetermined geographical position.
Described anti-interception flying object, described startup control module is timer, when described timer timing reached predetermined time, described startup control module was controlled described processor and is started working, otherwise described startup control module is controlled described processor dormancy.
Described anti-interception flying object, 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 release smog function described in the utility model, comprise processor, detecting module, release module, housing, induction installation and power supply, housing is provided with hatch near described release module place, hatch is connected with processor by second switch, and induction installation is used in the described housing of induction whether described smog being arranged.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 processor, processor controls described first switch closure according to the result of detection that has the interceptor target in the predetermined spy journey that receives and then the control release module discharges smog, induction installation is sensed smog in the housing, should respond to the result and send to processor, processor controls the second switch closure according to this induction result and then the control hatch is opened, smog is discharged, be used for fascination and follow the trail of the detection system of interception, disturb the result of the optical observation instrument of this detection system, thereby detection system stops to follow the trail of interception, and this flying object takes advantage of the occasion to escape under the shielding of smog.
(2) the anti-interception flying object with release smog function described in the utility model, the aerosol bomb of release module for making for dry ice, when having detected detection system tracking interception, discharge dry ice, reduce the temperature of this thing in fashion when forming fog, reduce the release of thermal source, thus the infrared acquisition that makes detection system less than, thereby detection system stops to follow the trail of interception, and this flying object takes advantage of the occasion to escape under the shielding of smog.
(3) the anti-interception flying object with release smog function 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 the anti-interception flying object that discharges the smog function;
Fig. 2 is the utility model embodiment 2 described structural representations with the anti-interception flying object that discharges the smog function.
Reference numeral is expressed as among the figure: the 1-processor, 11-starts control module, 2-detecting module, 3-housing, 31-hatch, 4-power supply, 5-release module, 6-induction installation, 71-first switch, 72-second switch.
The specific embodiment
Embodiment 1:
Structure with the anti-interception flying object that discharges the smog function described in the utility model as shown in Figure 1, it comprises processor 1, detecting module 2, release module 5, housing 3, induction installation 6 and power supply 4, 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 release module 5 is used for discharging smog, described release module 5 links to each other with described processor 1 via first switch 71, and described processor 1 is controlled described first switch, 71 closures and then controlled described release module 5 work according to the result of detection that has the interceptor target in the predetermined spy journey that receives; In the present embodiment, described release module 5 is aerosol bomb.
Described housing 3 is provided with hatch 31 near described release module 5 places, is used for discharging the described smog that described release module 5 discharges, and described hatch 31 is connected with described processor 1 by second switch 72; In the present embodiment, described housing 3 is provided with hatch 31 near described aerosol bomb place, is used for discharging the described smog that described aerosol bomb discharges, and described hatch 31 is connected with described processor 1 by second switch 72.
Described induction installation 6 is connected with described processor 1, be used in the described housing 3 of induction whether described smog being arranged, and will respond to the result and send to described processor 1, described processor 1 is controlled described second switch 72 according to described induction result when having sensed smog closed and then control described hatch 31 and open; In the present embodiment, described induction installation 6 is sensor.
Described power supply 4 is used for giving described processor 1, detecting module 2, release module 5 and 6 power supplies of described induction installation.
Anti-interception flying object with release smog function described in the utility model, comprise processor 1, detecting module 2, release module 5, housing 3, induction installation 6 and power supply 4, described housing 3 is provided with hatch 31 near described release module 5 places, described hatch 31 is connected with described processor 1 by second switch 72, and described induction installation 6 is used in the described housing 3 of induction whether described smog being arranged.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, described 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 is controlled first switch, 71 closures and then is controlled described release module 5 according to the result of detection that has the interceptor target in the predetermined spy journey that receives and discharges smog, described induction installation 6 is sensed in the described housing 3 smog, should respond to the result and send to described processor 1, described processor 1 is controlled described second switch 72 closures according to this induction result and then is controlled described hatch 31 and open, smog is discharged, be used for fascination and follow the trail of the detection system of interception, disturb the result of the optical observation instrument of this detection system, this flying object takes advantage of the occasion to escape under the shielding of smog.
Flying object can be any class in guided missile, aircraft, the aircraft.In the present embodiment, described flying object is guided missile.When having detected the interceptor target in predefined spy journey, described detecting module 2 when following the trail of interception guided missile, result of that probe is sent to described processor 1, described processor 1 is controlled first switch, 71 closures and then is controlled described release module 5 according to the result of detection that has the interceptor target in the predetermined spy journey that receives and discharges smog, described induction installation 6 is sensed in the described housing 3 smog, should respond to the result and send to described processor 1, described processor 1 is controlled described second switch 72 closures according to this induction result and then is controlled described hatch 31 and open, smog is discharged, be used for fascination and follow the trail of the interceptor target of interception, disturb the result of the optical observation instrument of this interceptor target, guided missile takes advantage of the occasion to escape under the shielding of smog, and then can continue flight, final this guided missile can hit the other side, finishes the work.
As other embodiments, described aerosol bomb is the aerosol bomb that dry ice is made.When having detected detection system tracking interception, discharge dry ice, reduce the temperature of this thing in fashion when forming fog, reduce the release of thermal source, thereby the infrared acquisition that makes detection system less than, thereby detection system stops to follow the trail of interception, this flying object takes advantage of the occasion to escape under the shielding of smog.
Embodiment 2:
Referring to shown in Figure 2, on the basis of embodiment 1, described flying object 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 flying object with release smog function described in the utility model, also comprise and start control module 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 startup control module 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 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 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, 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 (7)
1. one kind has the anti-interception flying object that discharges the smog 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;
Release module, be used for discharging smog, described release module links to each other with described processor via first switch, and described processor exists the result of detection of interceptor target to control described first switch closure and then control described release module work according in the predetermined spy journey that receives;
Housing, described housing is provided with hatch near described release module place, is used for discharging the described smog that described release module discharges, and described hatch is connected with described processor by second switch;
Induction installation, be connected with described processor, be used in the described housing of induction whether described smog being arranged, and will respond to the result and send to described processor, described processor is controlled described second switch closure according to described induction result and then is controlled described hatch and open when having sensed smog;
Power supply is used for giving described processor, detecting module, release module and the power supply of described induction installation.
2. anti-interception flying object according to claim 1 is characterized in that, described release module is aerosol bomb.
3. anti-interception flying object according to claim 2 is characterized in that, described aerosol bomb is the aerosol bomb that dry ice is made.
4. according to the arbitrary described anti-interception flying object of claim 1-3, 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.
5. anti-interception flying object according to claim 4 is characterized in that, described entry condition comprises predetermined time or predetermined geographical position.
6. anti-interception flying object according to claim 5, 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.
7. anti-interception flying object according to claim 6 is characterized in that, described detecting module is radar or camera.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN 201320066762 CN203069059U (en) | 2013-02-05 | 2013-02-05 | Anti-interception flying object with smog releasing function |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN 201320066762 CN203069059U (en) | 2013-02-05 | 2013-02-05 | Anti-interception flying object with smog releasing function |
Publications (1)
Publication Number | Publication Date |
---|---|
CN203069059U true CN203069059U (en) | 2013-07-17 |
Family
ID=48767837
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN 201320066762 Expired - Lifetime CN203069059U (en) | 2013-02-05 | 2013-02-05 | Anti-interception flying object with smog releasing function |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN203069059U (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103075929A (en) * | 2013-02-05 | 2013-05-01 | 王海龙 | Anti-interception flyer with smoke releasing function |
-
2013
- 2013-02-05 CN CN 201320066762 patent/CN203069059U/en not_active Expired - Lifetime
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103075929A (en) * | 2013-02-05 | 2013-05-01 | 王海龙 | Anti-interception flyer with smoke releasing function |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US20120210855A1 (en) | System and method for launching countermeasures to missile attack | |
RU2490584C1 (en) | Fighter device for destruction of drones | |
US5430448A (en) | Object detection system | |
CN203069059U (en) | Anti-interception flying object with smog releasing function | |
CN203116620U (en) | Anti-intercept flyer with smog releasing function and bait object releasing function | |
CN203116618U (en) | Anti-interceptive flying object with separating layer and function of releasing smog | |
CN203116619U (en) | Anti-interceptive flying object with separating layer and functions of releasing smog and lure | |
CN203069060U (en) | Anti-interception flying object with functions of laser assault resistance and smog release | |
CN203069061U (en) | Anti-interception flying object with function of smog and bait material release | |
CN203148317U (en) | Anti-intercept flyer with laser-strike-resistance, smog release and separation functions | |
CN203116617U (en) | Anti-interceptive flying object with separating layer and function of releasing lure | |
CN203069062U (en) | Anti-interception flying object with functions of smog and bait material release and laser assault resistance | |
CN203083456U (en) | Anti-interception flyer with separable layer | |
CN103075924B (en) | Anti-interception flyer with separation layer and smoke and bait object releasing function | |
CN203069058U (en) | Anti-interception flying object with functions of laser assault resistance and separation | |
CN203083455U (en) | Anti-interception flyer having functions of resisting laser irradiation and releasing bait materials | |
CN203116622U (en) | Anti-interception flyer | |
CN203116621U (en) | Detachable anti-intercept and anti-laser-attack flyer capable of releasing bait object | |
CN103075922B (en) | Anti-interception flyer with functions of resisting laser attack and releasing smoke | |
CN203083457U (en) | Anti-interception flyer having function of resisting laser irradiation | |
CN103075929A (en) | Anti-interception flyer with smoke releasing function | |
CN103075926B (en) | Anti-interception flyer with separation layer and smoke releasing function | |
CN103075923A (en) | Anti-interception flyer with smoke and bait object releasing function | |
CN103090747B (en) | Anti-interception flyer with separating layer and function of releasing bait objects | |
CN103075927B (en) | Anti-interception flyer with functions of releasing smoke and bait object and resisting laser impact |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
AV01 | Patent right actively abandoned |
Granted publication date: 20130717 Effective date of abandoning: 20150325 |
|
RGAV | Abandon patent right to avoid regrant |