CN113218250A - Method and facility for protecting safety of air-raid shelter - Google Patents
Method and facility for protecting safety of air-raid shelter Download PDFInfo
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- CN113218250A CN113218250A CN202110242829.2A CN202110242829A CN113218250A CN 113218250 A CN113218250 A CN 113218250A CN 202110242829 A CN202110242829 A CN 202110242829A CN 113218250 A CN113218250 A CN 113218250A
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- ground
- air
- floccule
- bomber
- fighter
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41H—ARMOUR; ARMOURED TURRETS; ARMOURED OR ARMED VEHICLES; MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL
- F41H11/00—Defence installations; Defence devices
- F41H11/02—Anti-aircraft or anti-guided missile or anti-torpedo defence installations or systems
- F41H11/04—Aerial barrages
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- General Engineering & Computer Science (AREA)
- Arrangements For Transmission Of Measured Signals (AREA)
Abstract
The invention relates to the field of air-raid protection, in particular to a method and a facility for protecting air-raid safety, wherein the method comprises the following steps: s1, monitoring a certain airspace outside a leading airspace through a monitoring device; s2, when the monitoring device monitors that a crime bomber or a fighter comes, the ground launching device launches the floccule concentrated cannonball to the air; s3, exploding the floccule concentrated cannonball after reaching the designated height to form floccules suspended in the air, and further forming a network for protecting a space, namely an skynet; s4, after the bomber or the fighter arrives at the floccule cover area, the floccule is sucked by the bomber or the fighter to damage the engine, so that the bomber or the fighter loses power and crashes. The method has the advantages of low implementation difficulty and low cost, and is suitable for the protection of the air-raid shelter.
Description
Technical Field
The invention relates to the field of national airspace protection, in particular to a method and a facility for protecting national airspace safety.
Background
Bombers or fighters are weaponry that need to enter into the airspace for infringement, and during the flight they need to intake a large amount of air, some of which supplies oxygen to the engine, ensuring its proper operation. The existing means of hitting bombers or fighters is to locate and track bombers or fighters by missiles and then to hit the bombers or the fighters. Missile and positioning tracking system are high in cost and not beneficial to reducing cost. If early warning can be given when a bomber or fighter is offending and some substance interfering with the bomber or fighter's engine is released in the airspace, causing the bomber or fighter to lose power and crash, the cost of hitting the bomber or fighter can be greatly reduced and national airspace is safeguarded.
Disclosure of Invention
Aiming at the defects of the prior art, the invention provides a method and a facility for protecting the safety of the air-raid shelter, and the method and the facility can give out early warning in advance when a bomber or a fighter makes a violation, and release floccules which damage the bomber or the fighter engine in the air to form a skynet, thereby effectively playing a role in integrally protecting the air-raid shelter.
In order to achieve the purpose, the invention provides the following technical scheme: a method for protecting the safety of a space, which is characterized in that: the method comprises the following steps: s1, monitoring a certain airspace outside a leading airspace through a monitoring device; s2, when the monitoring device monitors that a crime bomber or a fighter comes, the ground launching device launches the floccule concentrated cannonball to the air; s3, exploding the floccule concentrated cannonball after reaching the designated height to form floccules suspended in the air, and further forming a network for protecting a space, namely an skynet; s4, after the bomber or the fighter arrives at the floccule cover area, the floccule is sucked by the bomber or the fighter to damage the engine, so that the bomber or the fighter loses power and crashes.
After the technical scheme is adopted, a network covering the sky can be formed after the floccule concentrated cannonball explodes, the bomber or the fighter enters the network covering range, the air inlet sucks floccule, and the air inlet channel of the engine is blocked, so that the bomber or the fighter loses power and crashes, and the hitting cost and the hitting difficulty can be greatly reduced.
The invention also discloses a facility for protecting the safety of the air space, which is characterized in that: the monitoring device is connected with a ground command center through wireless communication, the ground command center is connected with a ground transmitting device through wireless communication, and the ground command center is further connected with an alarm device through a line.
After the technical scheme is adopted, the monitoring device is used for monitoring bombers or fighters offending outside the air, when the monitoring device receives the signals, the signals are transmitted to the ground command center, and meanwhile, the alarm device is triggered, and the ground command center controls the ground transmitting device to transmit the floccule concentrated cannonball into the air and then explode.
As a preferred technical scheme, the monitoring device is a satellite which is transmitted to the air from the ground.
After the technical scheme is adopted, the air-raid shelter can be monitored in real time, and the air-raid shelter is accurate and sensitive.
As preferred technical scheme, ground emitter include the fixing base, the fixing base upside is equipped with the transmission storehouse, transmission storehouse and launching tube intercommunication, transmission storehouse one side is equipped with the filler hole, the filler hole outside is equipped with the closing cap of switch, end connection ignition behind the transmission storehouse, ignition and ground command center wireless communication are connected.
After the technical scheme is adopted, the ground command center controls the ignition switch after receiving the signal, so that the floccule concentrated cannonball is launched into the air from the launching tube.
As a preferred technical scheme, the included angle between the emission tube and the horizontal plane is 60-90 degrees (including 60 degrees and 90 degrees).
After the technical scheme is adopted, the launching height of the floccule concentrated cannonball is guaranteed.
As a preferable technical scheme, a foam end cover is sleeved at the outer end part of the emission tube and is in a cylindrical shape with one side opened.
After adopting above-mentioned technical scheme, the foam end cover can play rain-proof effect, and strikes very easily and open, does not influence normal transmission.
The shell is fixed at the bottom of the shell, the shell is filled with concentrated liquid, the shell is also filled with an explosive device, and the explosive device is connected with a ground command center through wireless communication.
After the technical scheme is adopted, the ground command center can detonate the explosive device after the floccule concentrated cannonball is launched and lifted off, so that the floccule is scattered in the air.
As a preferred technical scheme, the concentrated solution is a mixture of polyurethane, asbestos wool and carbon powder, and the percentage of each component is 95%, 3% and 2% respectively.
After the technical scheme is adopted, the mixture is exploded to form foam through the explosion action volume of the explosion device and is scattered in the air to form a skynet, so that the destruction effect on the bombers or fighters can be realized.
As a preferable technical scheme, the ground transmitting device is arranged on the ground where the air-space boundary line is located, the suburban ground where the residential area is located and the ground of the key protection area.
After the technical scheme is adopted, the bomber or the fighter is struck just after entering the air, and an important protection effect is achieved for residents and key protection areas.
As a preferred technical scheme, the key protection areas comprise ground command centers, ammunition depots, grain bins, power plants, hospitals, schools and major engineering facilities.
After the technical scheme is adopted, the ground important area can be effectively protected.
Compared with the prior art, the invention provides a method and a facility for protecting the safety of the air traffic, which have the following beneficial effects:
1. the monitoring device and the alarm device can monitor a certain range outside the air space, and when a bomber or a fighter comes, signals can be transmitted to the command center in real time and alarm to remind workers to deal with the bomber or the fighter in time.
2. According to the invention, through the arrangement of the ground launching device, the floccule concentrated cannonball can be launched into the air and exploded, a large-area floccule is formed in the air and suspended in the air to form an aerial net, and after the bomber or the fighter enters the aerial net, the air inlet sucks in the floccule which can damage the engine, so that the bomber or the fighter loses power and falls down, the bomber or the fighter is effectively destroyed, and the cost and the hitting difficulty can be reduced; in addition, the carbon powder also has the function of conducting electricity for the airplane working by electricity, so that the inner circuit of the airplane is short-circuited, and the airplane can be burnt in a short time.
3. The invention can avoid the problem that the cable connection and the laying line are complex through wireless communication connection, and the construction is more flexible.
Drawings
FIG. 1 is a flow chart of a method of the present invention;
FIG. 2 is a schematic view of a plant embodying the present invention;
FIG. 3 is a schematic structural diagram of a ground transmitting device;
figure 4 is a schematic diagram of the structure of a floe-concentrated projectile of the present invention.
In the figure: 1. a monitoring device; 2. a ground launch device; 21. a base; 22. a launch bin; 221. a feeding port; 23. a launch tube; 24. sealing the cover; 3. a ground command center; 4. a floccule-enriched shell; 41. a housing; a rocket projectile; 43. an explosive device.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
As shown in fig. 1 to 4, a method for protecting national airspace security includes the following steps: s1, monitoring a certain airspace outside the airspace through the monitoring device 1; s2, when the monitoring device 1 monitors a bomber or a fighter, the ground launching device 2 launches the floccule concentrated cannonball 4 to the air; s3, exploding the floccule concentrated cannonball 4 after reaching a specified height to form foam floccules suspended in the air, and further forming a network for protecting a neck space, namely an skynet; s4, after the bomber or the fighter arrives at the floccule cover area, the floccule is sucked by the bomber or the fighter to damage the engine, so that the bomber or the fighter loses power and crashes. The floccule concentrated cannonball 4 can form a network covering the sky after explosion, the bomber or the fighter enters the network covering range, and the air inlet sucks floccule and blocks an air inlet channel of an engine, so that the engine of the bomber or the fighter is lack of oxygen and loses power to crash, and the hitting cost and the hitting difficulty can be greatly reduced.
The invention also discloses a facility for protecting national airspace safety, which comprises a monitoring device 1, wherein the monitoring device 1 is connected with a ground command center 3 through wireless communication, the ground command center 3 is connected with a ground transmitting device 2 through wireless communication, and the ground command center 3 is also connected with an alarm device through a line (the prior art). The monitoring device 1 is used for monitoring bombers or fighters of the offenders outside the air, when receiving signals, the monitoring device transmits the signals to the ground command center 3, and simultaneously triggers the alarm device, and the ground command center 3 controls the ground transmitting device 2 to transmit the floccule concentrated cannonball 4 into the air and then explode. The monitoring device 1 is a satellite which is transmitted to the air from the ground. The air-raid monitoring system can monitor the air-raid, and is accurate and sensitive.
In the above embodiment, specifically, the ground emitting device 2 includes a fixing base 21, the upper side of the fixing base 21 is provided with an emitting bin 22, the emitting bin 22 is communicated with an emitting tube 23, one side of the emitting bin 22 is provided with a filling opening 221, the outer side of the filling opening 221 is provided with a switchable cover 24 (prior art, known to those skilled in the art), the rear end of the emitting bin 22 is connected with an ignition device (not shown), and the ignition device is in wireless communication connection with the ground command center 3 (prior art, known to those skilled in the art, and other undescribed structures of the ground emitting device 2 are known to those skilled in the art). After receiving the signal, the ground command center 3 controls the ignition switch to make the floccule-concentrated cannonball 4 be launched into the air from the launching tube 23. The included angle between the emission tube 23 and the horizontal plane is 70 degrees. The launching height of the floccule condensed cannonball 23 is ensured. The outer end of the transmitting tube 23 is sleeved with a foam end cover (not shown) which is in a cylindrical shape with one side opened. The foam end cover can play a rainproof role, and is easy to impact and open, so that normal launching is not influenced.
In the above embodiment, specifically, the floccule-enriched cannonball 4 comprises a casing 41 (made of plastic, glass fiber reinforced plastic or metal), a rocket launcher 42 is fixed at the bottom of the casing 41, a (high-pressure filling) concentrated solution is contained in the casing 41, an explosive device 43 (in the prior art) is further contained in the casing 41, and the explosive device 43 is connected with the ground command center 3 through wireless communication (in the prior art). After the floe-concentrated cannonball 4 is launched and lifted off, the ground command center 3 may detonate the explosive device 43, thereby causing the floe to fall into the air. The concentrated solution is a mixture of polyurethane, asbestos wool and carbon powder, and the percentage of each component is 95%, 3% and 2% respectively. The mixture is exploded to form foam through the explosion action volume of the explosion device 43 and is scattered and suspended in the high altitude to form a skynet, so that the mixture can have destructive effect on the bombers or fighters, and the destructive mechanism is as follows: the foam is absorbed by the air inlet of the bomber or the fighter, the asbestos wool and the carbon powder (the asbestos wool and the carbon powder are high-temperature resistant materials and cannot be easily combusted) can block the air inlet, and the inside of the engine can lack oxygen and lose power, so that the bomber or the fighter can crash. And the polyurethane, the asbestos wool and the carbon powder are relatively environment-friendly, and can not cause serious pollution to the environment.
In the above embodiment, more specifically, the ground emission devices 2 are installed on the ground where the airspace boundary line is located, the suburban ground where the residential area is located, and the ground of the key protection area. The bomber or fighter is struck just before entering the air, and plays an important role in protecting residents and key protection areas. The key protection areas comprise ground command centers, ammunition depots, grain bins, power plants, hospitals, schools and major engineering facilities. Can play an effective protection role for important areas on the ground.
The components used in the present invention are all common standard components or components known to those skilled in the art, and the structure and principle thereof are well known to those skilled in the art.
It is noted that, herein, relational terms such as first and second, and the like may be used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Also, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.
Claims (10)
1. A method for protecting the safety of a space, which is characterized in that: the method comprises the following steps: s1, monitoring a certain airspace outside a leading airspace through a monitoring device; s2, when the monitoring device monitors that a crime bomber or a fighter comes, the ground launching device launches the floccule concentrated cannonball to the air; s3, exploding the floccule concentrated cannonball after reaching the designated height to form floccules suspended in the air, and further forming a network for protecting a space, namely an skynet; s4, after the bomber or the fighter arrives at the floccule cover area, the floccule is sucked by the bomber or the fighter to damage the engine, so that the bomber or the fighter loses power and crashes.
2. The invention also discloses a facility for protecting the safety of the air space, which is characterized in that: the monitoring device is connected with a ground command center through wireless communication, the ground command center is connected with a ground transmitting device through wireless communication, and the ground command center is further connected with an alarm device through a line.
3. A space-saving safety protection system according to claim 2, wherein: the monitoring device is a satellite which is transmitted to the air from the ground.
4. A space-saving safety protection system according to claim 2, wherein: the ground emission device include the fixing base, the fixing base upside is equipped with the transmission storehouse, transmission storehouse and launching tube intercommunication, transmission storehouse one side is equipped with the filler opening, the filler opening outside is equipped with the closing cap of switch, end connection ignition behind the transmission storehouse, ignition and bottom surface command center wireless communication are connected.
5. A space-saving safety protection system according to claim 4, wherein: the included angle between the emission tube and the horizontal plane is 60-90 degrees.
6. A space-saving safety protection system according to claim 4, wherein: the outer end part of the emission tube is sleeved with a foam end cover which is in a cylindrical shape with one side opened.
7. A method of securing airspace as claimed in claim 1, wherein: the floccule concentrated cannonball comprises a shell, a rocket emitter is fixed at the bottom of the shell, concentrated liquid is contained in the shell, an explosive device is also contained in the shell, and the explosive device is connected with a ground command center through wireless communication.
8. A space-saving safety protection system according to claim 7, wherein: the concentrated solution is a mixture of polyurethane, asbestos wool and carbon powder, and the percentage of each component is 95%, 3% and 2% respectively.
9. A space-saving safety protection system according to claim 2, wherein: the ground transmitting device is arranged on the ground where the air-receiving boundary line is located, the suburban ground where the residential area is located and the ground of the key protection area.
10. A space-saving safety protection system according to claim 9, wherein: the key protection areas comprise ground command centers, ammunition depots, grain bins, power plants, hospitals, schools and major engineering facilities.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202110242829.2A CN113218250A (en) | 2021-03-05 | 2021-03-05 | Method and facility for protecting safety of air-raid shelter |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202110242829.2A CN113218250A (en) | 2021-03-05 | 2021-03-05 | Method and facility for protecting safety of air-raid shelter |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN113218250A true CN113218250A (en) | 2021-08-06 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202110242829.2A Pending CN113218250A (en) | 2021-03-05 | 2021-03-05 | Method and facility for protecting safety of air-raid shelter |
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Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4196668A (en) * | 1975-11-18 | 1980-04-08 | Morlock Guenter E | Stopping operating enemy vehicles, vessels and aircrafts |
| US20020189432A1 (en) * | 2001-06-19 | 2002-12-19 | Facciano Andrew B. | Composite concentric launch canister |
| US20060021538A1 (en) * | 2002-08-29 | 2006-02-02 | Lloyd Richard M | Kinetic energy rod warhead deployment system |
| CN101139429A (en) * | 2007-02-14 | 2008-03-12 | 陈永培 | Nano antibiotic sponge and processing technology thereof |
| CN106059653A (en) * | 2016-08-02 | 2016-10-26 | 中国民用航空飞行学院 | Aircraft signal transmission system and signal transmission method thereof |
| CN109813187A (en) * | 2018-12-19 | 2019-05-28 | 山东师范大学 | A kind of aerial thunder and its working method of countering intrusions aircraft |
| CN110196000A (en) * | 2019-05-30 | 2019-09-03 | 董恬纲 | Metal powder shell |
-
2021
- 2021-03-05 CN CN202110242829.2A patent/CN113218250A/en active Pending
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4196668A (en) * | 1975-11-18 | 1980-04-08 | Morlock Guenter E | Stopping operating enemy vehicles, vessels and aircrafts |
| US20020189432A1 (en) * | 2001-06-19 | 2002-12-19 | Facciano Andrew B. | Composite concentric launch canister |
| US20060021538A1 (en) * | 2002-08-29 | 2006-02-02 | Lloyd Richard M | Kinetic energy rod warhead deployment system |
| CN101139429A (en) * | 2007-02-14 | 2008-03-12 | 陈永培 | Nano antibiotic sponge and processing technology thereof |
| CN106059653A (en) * | 2016-08-02 | 2016-10-26 | 中国民用航空飞行学院 | Aircraft signal transmission system and signal transmission method thereof |
| CN109813187A (en) * | 2018-12-19 | 2019-05-28 | 山东师范大学 | A kind of aerial thunder and its working method of countering intrusions aircraft |
| CN110196000A (en) * | 2019-05-30 | 2019-09-03 | 董恬纲 | Metal powder shell |
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Application publication date: 20210806 |
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