CN109813187A - A kind of aerial thunder and its working method of countering intrusions aircraft - Google Patents
A kind of aerial thunder and its working method of countering intrusions aircraft Download PDFInfo
- Publication number
- CN109813187A CN109813187A CN201811559056.5A CN201811559056A CN109813187A CN 109813187 A CN109813187 A CN 109813187A CN 201811559056 A CN201811559056 A CN 201811559056A CN 109813187 A CN109813187 A CN 109813187A
- Authority
- CN
- China
- Prior art keywords
- thunder
- seed
- engine
- gas bag
- aircraft
- 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.)
- Granted
Links
Landscapes
- Buildings Adapted To Withstand Abnormal External Influences (AREA)
- Tires In General (AREA)
Abstract
The invention discloses a kind of aerial thunder of countering intrusions aircraft and its working methods, when discovery has intruder, flight controller controls rocket engine starting, after rocket launching, the real time position for the intruder that rocket radar is locked according to radar, take rocket to specified region, the flight controller control ejector of rocket pops up the aerial thunder in loading storehouse；Aerial thunder scatters out self-contained seed thunder within the scope of setting time after pop-up；Liquid helium in each cavity of seed thunder becomes gaseous state helium, and seed thunder is made to suspend in the sky；So far, seed thunder is successfully deployed to specified region in the air；When intruder enters specified region, seed thunder is inhaled into the engine of intruder；All coverings of seed thunder are broken by the blade of engine；Telescopic manganese steel item is stretched over longest state, damages the engine blade of rotation, and explosive demolishs engine.
Description
Technical field
This disclosure relates to the aerial thunder and its working method of a kind of countering intrusions aircraft.
Background technique
The statement of this part is only to improve background technique relevant to the disclosure, not necessarily constitutes the prior art.
Currently, aircraft in modern war, is already most effective operation tool.
(1) control of the air is fought for, there is control of the air, could effectively be screened over the ground, to sea.
(2) aircraft can directly attack aerial target, ground target etc. or long-range strike.
(3) aircraft can also realize that quick troops, equipment deliver.The effect of aircraft, other weapons, equipment can not replace.
Currently, the effective means that various countries resist enemy's aircraft is very limited:
(1) mode is intercepted in the air, and departing aeroplane to enemy plane machine gun, destroyed by the mode for dropping guided missile；
(2) ground forces intercept enemy's aircraft method, are destroyed with antiaircraft machine gun, antiaircraft gun, surface-to-air ballistic missile to enemy plane
Formula intercepts.
The interception of aircraft first has to find that enemy's aircraft, stealth aircraft are difficult to find radar in advance.Technology is difficult at present
Reach effective discovery to aircraft, it is even more impossible to effectively intercept.
Current various countering intrusions aircraft systems the problem is that: system expensive, technical difficulty is big, inefficiency.
Summary of the invention
In order to solve the deficiencies in the prior art, present disclose provides a kind of aerial thunder of countering intrusions aircraft and its work sides
Method can be realized enemy's aircraft and step on thunder in the sky, destroyed by the thunder；
In a first aspect, present disclose provides a kind of aerial thunders of countering intrusions aircraft；
A kind of aerial thunder of countering intrusions aircraft, including several seed thunders；Each seed thunder includes from outside to inside several
Layer: shape among outer layer metal shell, outer layer gas bag wall, middle layer gas bag wall and internal layer gas bag wall, outer layer gas bag wall and middle layer gas bag wall
At the first cavity, the second cavity is formed among middle layer gas bag wall and internal layer gas bag wall, forms third cavity on the inside of internal layer gas bag wall；
Filled with liquid helium air parcel in first, second, and third cavity；Innermost layer gas bag pars intramuralis is equipped with explosive and telescopic manganese steel
Item；The outer layer metal shell includes symmetrical two shells, and the edge of two shells passes through buckle closure；
The aerial thunder is mounted in the loading storehouse of rocket, and when discovery has intruder, flight controller controls rocket
Engine start, after rocket launching, the real time position for the intruder that rocket radar is locked according to radar, rocket flight is to specified
The flight controller control ejector in region, rocket pops up the aerial thunder in loading storehouse；Aerial thunder setting time after pop-up
Self-contained seed thunder is scattered out in range；Liquid helium air parcel in each cavity of seed thunder becomes gaseous state helium,
First, second, and third cavity is full of by gaseous state helium；Outer layer metal shell blocks under the action of helium atmosphere expansive force
Button releases snap-fit relationship, and outer layer metal shell falls off on the outside of outer layer gas bag wall；Seed thunder suspends in the sky；So far, seed thunder
It is routed to specified region in the air；
When intruder enters specified region, seed thunder is inhaled into the engine of intruder；The institute of seed thunder
There is gas bag wall to be broken by the blade of engine；Telescopic manganese steel item is stretched over longest state, damages the engine leaf of rotation
Piece, explosive demolish engine.
Further, the outer layer gas bag wall forms one and is in metal-back inside and is in outer on the outside of intermediate gas bag wall
Layer gas bag；The outer layer gas bag is enclosed；
Similarly, the middle layer gas bag wall forms one and is on the inside of outer layer gas bag wall and is on the outside of internal layer gas bag wall
Layer gas bag；The middle layer gas bag is enclosed；
Similarly, the internal layer gas bag wall forms an internal layer gas bag being on the inside of the gas bag wall of middle layer；The internal layer gas bag
It is enclosed.
The liquid helium air parcel, including a closed film, closed film inside is liquid helium.When temperature reaches setting
When value, liquid helium becomes gaseous state helium, and gaseous state helium is for filling the first, second, and third cavity.
Further, the material of the outer layer gas bag wall, middle layer gas bag wall and internal layer gas bag wall, including in following material
At least one material: latex, polyurethane and composite nano materials.
Further, seed thunder suspends in the sky, is the aeration quantity by presetting helium, make the gravity of seed thunder with
The aerostatic buoyancy in aerial specified region is consistent.
Further, the outer layer gas bag wall, middle layer gas bag wall or internal layer gas bag wall are equipped with balanced valve, and balanced valve is used for
The pressure of gas inside and outside Balance Air containment wall.
The molecular weight of helium: 4.003, density: 0.12491 grams per liter (g/L3), fusing point: -272.3 DEG C, boiling point: -
268.934℃.The specific gravity 1.22kg/m of air3
Further, the manganese steel item, including three section manganese steel metallic conduits, three section manganese steel metallic conduits are socketed in one each other
It rises, compressed spring is equipped in the innermost layer metallic conduit of three section manganese steel metallic conduits；When manganese steel item is in innermost layer gas bag pars intramuralis
When, three section manganese steel metallic conduits and compressed spring are in compressive state, after being adsorbed onto engine interior by aircraft engine,
Under the shock of engine blade, gas bag wall rupture, manganese steel item is automatically springed open by compressive state under the drive of compressed spring, is flicked
Afterwards, it is in extended state.
The manganese steel item of extended state is due to becoming large-sized, it is easier to cause to damage to the engine blade of aircraft.
The consistent in density of density and specified regional atmospheric layer in each cavity filled with helium, enables seed thunder to suspend
In the sky.
Aerial thunder refers to after being deployed to specified region in the air, suspends in the sky, similar to snow in the air, so being referred to as sky
Middle thunder.
Manganese steel item: three sections of scalable manganese steel casings compositions, seed thunder is in contraction state: due to pressure, volumetric constraint, three
Suit mode of the section manganese steel sleeved compression at one section.
There are two types of manganese steel item extension modes: the first is when compressing force has cancelled, and three sections of manganese steel casing are upheld；It is for second
When manganese steel item is inhaled into engine, manganese steel casing is stretched.
The explosive is equipped with explosive fuse, and the explosive fuse is connect with explosive, is ignited using pressure trigger or noise
Device.It is quickly rotated for aircraft engine impeller, immense pressure is generated to inhalation (inhalatio), engine generates very very noisy.
Explosive fuse, comprising: pressure trigger or noise trigger.
Explosive: using the explosive of high brisance, light weight, power is big.It is enough to demolish aircraft engine part part, causes
Engine is set to lose the job ability.
Second aspect, the disclosure additionally provide a kind of working method of the aerial thunder of countering intrusions aircraft；
A kind of working method of the aerial thunder of countering intrusions aircraft, comprising:
When discovery has intruder, flight controller controls rocket engine and starts, after rocket launching, rocket radar root
Ejector is controlled according to the flight controller of the real time position of the intruder of radar locking, rocket flight to specified region, rocket
By the aerial thunder pop-up in loading storehouse；Aerial thunder scatters self-contained seed thunder within the scope of setting time after pop-up
It goes；Liquid helium air parcel in each cavity of seed thunder becomes gaseous state helium, and first, second, and third cavity is by gaseous state
Helium is full of；Outer layer metal shell buckles under the action of helium atmosphere expansive force releases snap-fit relationship, and outer layer metal shell is from outer layer
It falls off on the outside of gas bag wall；Seed thunder suspends in the sky；So far, seed thunder is routed to specified region in the air；
When intruder enters specified region, seed thunder is inhaled into the engine of intruder；The institute of seed thunder
There is gas bag wall to be broken by the blade of engine；Telescopic manganese steel item is stretched over longest state, damages the engine leaf of rotation
Piece, explosive demolish engine.
Compared with prior art, the beneficial effect of the disclosure is:
Aircraft enters into the minefield in the sky, and confined explosion occurs for aircraft.Destroy aircraft.Since minefield area of space is big, than
Existing weapons can more smash the flying objects such as aircraft.Especially stealth aircraft, reflection of radar wave face be small, weapon is not easy to aim at, and hits
Rate is low.The hit rate to stealth aircraft can be improved in the thunder.
Detailed description of the invention
The accompanying drawings constituting a part of this application is used to provide further understanding of the present application, and the application's shows
Meaning property embodiment and its explanation are not constituted an undue limitation on the present application for explaining the application.
The anti-Aircraft Air thunder structural schematic diagram that Fig. 1 is promoted with rocket mode；
Fig. 2 is the electric connecting relation schematic diagram of rocket；
Fig. 3 seed thunder structural schematic diagram；
Schematic diagram after the expansion of Fig. 4 seed thunder helium gas inside.
Specific embodiment
It is noted that described further below be all exemplary, it is intended to provide further instruction to the application.Unless another
It indicates, all technical and scientific terms used herein has usual with the application person of an ordinary skill in the technical field
The identical meanings of understanding.
It should be noted that term used herein above is merely to describe specific embodiment, and be not intended to restricted root
According to the illustrative embodiments of the application.As used herein, unless the context clearly indicates otherwise, otherwise singular
Also it is intended to include plural form, additionally, it should be understood that, when in the present specification using term "comprising" and/or " packet
Include " when, indicate existing characteristics, step, operation, device, component and/or their combination.
The classification of thunder: land mine steps on thunder --- and it is designed for enemy soldier, is embedded in underground and draws after soldier tramples on
It is quick-fried, it wound soldier.Antitank mine -- it is directed to tank, when being designed as encountering tank track pressure, is ignited.Destroy tank track
For core point.Submarine mine: the thunder designed for naval vessels in water destroys for the purpose of naval vessels.The aerial thunder of anti-aircraft: for entering in the air
The thunder invading aircraft and designing destroys for the purpose of airflight object.
Be directed to the weakness of aircraft engine: air inflow is huge, the characteristics of being easily damaged, to design aerial thunder:
Aircraft is equipped with air intake duct, provides air exclusively for engine, provides oxygen.Channel is huge, smooth, straight-through to start
Machine.Aircraft engine powerful, compact-sized, light-weight, thrust is big.The powerful and choux pastry heart of aircraft is dirty: engine one
The plane collision of bird and high-speed flight, can be such that aircraft damages.One piece of coin can destroy an aircraft engine.
Fanjet, vector engine are the power devices of modern aircraft, need powerful air stream, provide for engine
Oxygen.If the engine air capacity of " extra large sparrow hawk " is 196 Kilograms Per Seconds, the engine of the winged leopard of China needs throughput, then be 2 ×
92 Kilograms Per Seconds, U.S. F-15's is 2 × 121 Kilograms Per Seconds.The specific gravity 1.22kg/m of air3, engine needs air stream
100m3/ the second.
Floating force with helium (helium is stable, safe) relative to atmosphere, as the power for carrying warhead.Allow whole ratio
Weight and the atmosphere consistent in density, the aerial thunder of countering intrusions aircraft are made of a large amount of seed thunders, the aerial thunder quilt of countering intrusions aircraft
After being emitted to specified altitude assignment, specified region, with explosive manner, a large amount of seed thunders are spread huge space multistory range.
As depicted in figs. 1 and 2, a kind of aerial thunder of countering intrusions aircraft, including several seed thunders；Each seed thunder includes
Several layers from outside to inside: outer layer metal shell, outer layer gas bag wall, middle layer gas bag wall and internal layer gas bag wall, as shown in figure 3, outer layer
The first cavity is formed among gas bag wall and middle layer gas bag wall, and the second cavity is formed among middle layer gas bag wall and internal layer gas bag wall, it is interior
Third cavity is formed on the inside of layer gas bag wall；Filled with liquid helium air parcel in first, second, and third cavity；In innermost layer gas bag wall
Portion is equipped with explosive and telescopic manganese steel item；The outer layer metal shell includes symmetrical two shells, and the edge of two shells is logical
Cross buckle closure；
The aerial thunder is mounted in the loading storehouse of rocket, and when discovery has intruder, flight controller controls rocket
Engine start, after rocket launching, the real time position for the intruder that rocket radar is locked according to radar, rocket flight is to specified
The flight controller control ejector in region, rocket pops up the aerial thunder in loading storehouse；Aerial thunder setting time after pop-up
Self-contained seed thunder is scattered out in range；Liquid helium air parcel in each cavity of seed thunder becomes gaseous state helium,
First, second, and third cavity is full of by gaseous state helium；Outer layer metal shell blocks under the action of helium atmosphere expansive force
Button releases snap-fit relationship, and outer layer metal shell falls off on the outside of outer layer gas bag wall；Seed thunder suspends in the sky；So far, seed thunder
It is routed to specified region in the air；
When intruder enters specified region, seed thunder is inhaled into the engine of intruder；The institute of seed thunder
There is gas bag wall to be broken by the blade of engine；Telescopic manganese steel item is stretched over longest state, damages the engine leaf of rotation
Piece, explosive demolish engine.
During mine-laying, Consideration:
(1) height of intruder, seed thunder overall weight and helium buoyancy reach flat in the airspace of aircraft flight height
Weighing apparatus.
(2) because of different battle skies, Various Seasonal, temperature, humidity influence the specific gravity of air, inclined in atmospheric density
When low normal value, mine-laying height is higher than predetermined altitude, and the weight of seed thunder is greater than buoyancy, will be slow sinking.When in air
When the higher normal value of density, mine-laying height is lower than predetermined altitude, and the weight of seed thunder is less than buoyancy, will be slow rising.
(3) air flows, and can also be floating with effect to seed thunder specific region, when mine-laying, considers the change of atmosphere zone wind direction
Change, estimated according to enemy plane arrival time, highly estimated, wind speed is estimated, determine in wind direction reverse direction, at a certain distance from mine-laying, seed
Grain thunder is slowly moved to the region for needing mine-laying under wind blows.
When intruder enters specified region, seed thunder is inhaled into the engine of intruder；The institute of seed thunder
There is spherical surface to be broken by the blade of engine；Telescopic manganese steel item has been extended to longest state, damages the engine leaf of rotation
Piece, explosive demolish engine.
The spherical surface is elastic force film, contains a small amount of solid-state or liquid helium in every layer.After being released, external pressure is released
It puts, helium expands rapidly, is full of each layer.When due to design, using seed thunder after helium expansion, float in the sky, neither rise,
Also do not decline.The tension selection of balloon wall is appropriate, and whole kernel thunder specific gravity is consistent with the atmosphere specific gravity, it is ensured that aerial thunder is stablized
In the sky.
After aircraft enters minefield, engine absorbs atmosphere, while seed thunder is sucked engine, and it is fried that seed thunder carries high energy
Medicine explodes in engine.Engine is destroyed, aircraft is also just destroyed.Seed thunder has hard metal stick, rises to engine blade broken
Bad effect.
Air speed is high, hits seed thunder, sets off an explosion, damage aircraft part.Disequilibrium makes complete machine crash.
As shown in Figure 1, countering intrusions Aircraft Air thunder structure: rocket propulsion -- complete to transport aerial thunder to formulation airspace
Effect.Fuel compartment: storage rocket engine fuel.Flight controller: receiving command centre's order, decomposes order, sends out to rocket
Motivation issues operating instruction.Control operation posture, the speed of service, operation area.Radar detection provides foundation for operation area.
Aerial thunder warhead: fuse, explosive, seed thunder.Fuse: ignition charge.Explosive: seed thunder is spread to broad area.Seed
Thunder: aircraft engine is destroyed.
Seed thunder: multilayer gas bag structure, each layer contain set amount helium.The innermost layer of seed thunder is warhead: 1 gram of height
Imitate explosive, 1 grammes per square metre manganese steel item.
Multilayer gas bag wall use latex, polyurethane or composite nano materials, thickness, elastic force, gas tension satisfaction set
Provisioning request: seed thunder overall weight and helium buoyancy reach balance in the airspace of aircraft flight height.Because different battle skies,
Various Seasonal changes the buoyancy of air, thus according to material thickness, the expansive force of gas, the elastic force of film, according to gas
It waits, the theater of war, the aeration quantity of helium has appropriate adjustment, meets the constraint condition of factors.
The outer layer gas bag wall, middle layer gas bag wall or internal layer gas bag wall are equipped with balanced valve, and buoyancy is greater than gravity, seed thunder
Rise, balanced valve is opened, leak source gas.If gravity is greater than buoyancy, the outside one layer of release of internal layer gas.Volume increases, and floats
Power increases, and reaches balance.
Seed thunder volume, weight: helium characteristic: the molecular weight of helium: 4.003, density: 0.12491 grams per liter (g/
L3), fusing point: -272.3 DEG C；Boiling point: -268.934 DEG C.The specific gravity 1.22kg/m of air3。
It is assumed that: explosive: 1 gram；Manganese steel item: 1 gram；Gas bag wall: 1 gram, helium weight: 0.12491*x, x indicate that seed thunder is swollen
Volume after swollen；
Seed thunder weight: explosive+manganese steel item+gas bag wall material matter+helium=1+1+1+0.12491*x；
Buoyancy of the seed thunder to air: weight=1.22*x of air is arranged；
When floating: seed thunder weight is equal to seed thunder to the buoyancy of air；
Then have: seed thunder weight: w=1+1+1+0.12491x；
Seed thunder is to the buoyancy for arranging air: F=1.22*x；
The showy condition of seed thunder: w=F
It is obtained by above formula: x=2.7395
In view of a small amount of auxiliary material of seed thunder, such as fuse and other items weight, explosive, manganese steel item, gas bag wall material matter all occupy few
Measure volume.Choosing 3 liters of helium is the showy buoyancy of seed thunder.The weight of helium: 0.37473 gram, if seed thunder is wrapped using three layers,
Every layer of impartial dress helium, then each layer of filling: 0.12491 gram, i.e. 1 liter of helium.
It is spherical after the expansion of seed thunder.In the sky when raney portion, due to being condensed in manganese steel item are as follows: 3---5 centimetres of strip.
Therefore: seed thunder is shrinking strip of the dress for 3--5 centimetres.Shell has metal material package.Shell is two-piece type cylinder buckle
Formula structure, after seed thunder is ejected, external pressure is cancelled, and gas expansion makes seed thunder shell fall off.Structure is as shown in Figure 3
Fuse: pressure or big noise apparatus to cause bursting can be used.It is quickly rotated for aircraft engine impeller, to inhalation (inhalatio)
Immense pressure is generated, engine generates very very noisy.The trigger of explosive can be designed to that pressure ignites mode or very noisy draws
Quick-fried mode.
Explosive: the explosive of high brisance, light weight, power are big.It is enough to demolish aircraft engine part part, causes to send out
Motivation is lost the job ability.
Afloat seed thunder structural schematic diagram, as shown in figure 4, seed thunder shape journey balloon-like after expansion, interlayer contain
A small amount of helium gas.Purpose is to increase seed thunder usability, by explosion, inevitably scratches crust or several layers of skin.As long as but having one
Layer is intact.Seed thunder equally completes task.Explosive: high explosive and fuse composition, the part of main complete coupled engines are destroyed
Effect.
Manganese steel item: being made of three sections, is initially located in three sections and is inserted in state.As gas bag stretches, metal strip trails.Have one
A bolt after stretching, extension, cannot retract.5 to 10 millimeters of every section, after stretching, extension, total length: 15 to 30 millimeters.Once by aircraft engine
Air intake duct is sucked, into engine, engine blade is scratched, damage.Cause engine damage.Engine damage, aircraft without
Method flight, or even crash.High-speed aircraft knocks seed thunder, and a manganese steel item, one gram of explosive are also enough to damage aircraft locally.
The aerial thunder of countering intrusions aircraft: stealth aircraft can not pass through aerial minefield.The position of stealth aircraft, flight path are hidden
It covers, precision strike can not be implemented.It is extremely low to hit hit rate.Using anti-Aircraft Air thunder, large space regional blockade, at it by flying
Walking along the street line, mine-laying in advance.
The aerial thunder of countering intrusions aircraft: fighter plane, bomber formation carry out tactical mining.Effect is more preferable.
The aerial thunder of countering intrusions aircraft carries out big airspace in aircraft route and shifts to an earlier date mine-laying, and can cut up the enemy forces aircraft engine
Machine.Seed thunder floats in the sky.Aerial thunder can use the mine-laying of rocket mode.
The aerial thunder of countering intrusions aircraft is able to achieve to the destruction of the engine of aircraft, can more effective stealth aircraft, aircraft it is big
It forms into columns and invades.
The foregoing is merely preferred embodiment of the present application, are not intended to limit this application, for the skill of this field
For art personnel, various changes and changes are possible in this application.Within the spirit and principles of this application, made any to repair
Change, equivalent replacement, improvement etc., should be included within the scope of protection of this application.
Claims (8)
1. a kind of aerial thunder of countering intrusions aircraft, characterized in that including several seed thunders；Each seed thunder includes from outside to inside
Several layers: outer layer metal shell, outer layer gas bag wall, middle layer gas bag wall and internal layer gas bag wall, outer layer gas bag wall and middle layer gas bag wall
Centre forms the first cavity, and the second cavity is formed among middle layer gas bag wall and internal layer gas bag wall, and the is formed on the inside of internal layer gas bag wall
Three cavitys；Filled with liquid helium air parcel in first, second, and third cavity；Innermost layer gas bag pars intramuralis is equipped with explosive and scalable
Manganese steel item；The outer layer metal shell includes symmetrical two shells, and the edge of two shells passes through buckle closure；
The aerial thunder is mounted in the loading storehouse of rocket, and when discovery has intruder, flight controller controls rocket motor
Machine starts, after rocket launching, the real time position for the intruder that rocket radar is locked according to radar, and rocket flight to specified area
The flight controller control ejector in domain, rocket pops up the aerial thunder in loading storehouse；Aerial thunder setting time model after pop-up
It encloses and interior scatters out self-contained seed thunder；Liquid helium air parcel in each cavity of seed thunder becomes gaseous state helium, institute
The first, second, and third cavity is stated to be full of by gaseous state helium；Outer layer metal shell buckles under the action of helium atmosphere expansive force
Snap-fit relationship is released, outer layer metal shell falls off on the outside of outer layer gas bag wall；Seed thunder suspends in the sky；So far, seed thunder quilt
It is deployed to specified region in the air；
When intruder enters specified region, seed thunder is inhaled into the engine of intruder；All gas of seed thunder
Containment wall is broken by the blade of engine；Telescopic manganese steel item is stretched over longest state, damages the engine blade of rotation, fries
Medicine demolishs engine.
2. a kind of aerial thunder of countering intrusions aircraft as described in claim 1, characterized in that the outer layer gas bag wall, middle layer gas
At least one of containment wall and the material, including following material of internal layer gas bag wall material: latex, polyurethane and composite Nano material
Material.
3. a kind of aerial thunder of countering intrusions aircraft as described in claim 1, characterized in that seed thunder suspends in the sky, is logical
The aeration quantity for presetting helium is crossed, keeps the gravity of seed thunder consistent with the aerial specified aerostatic buoyancy in region.
4. a kind of aerial thunder of countering intrusions aircraft as described in claim 1, characterized in that the outer layer gas bag wall, middle layer gas
Containment wall or internal layer gas bag wall are equipped with balanced valve, pressure of the balanced valve for gas inside and outside Balance Air containment wall.
5. a kind of aerial thunder of countering intrusions aircraft as described in claim 1, characterized in that the manganese steel item, including three section manganese
Steel metal pipeline, three section manganese steel metallic conduits connect together each other, in the innermost layer metallic conduit of three section manganese steel metallic conduits
Equipped with compressed spring；When manganese steel item is in innermost layer gas bag pars intramuralis, three section manganese steel metallic conduits and compressed spring are in compression
State, after being adsorbed onto engine interior by aircraft engine, under the shock of engine blade, the rupture of gas bag wall, manganese steel item
It is automatically springed open under the drive of compressed spring by compressive state, after flicking, is in extended state.
6. a kind of aerial thunder of countering intrusions aircraft as claimed in claim 5, characterized in that
There are two types of manganese steel item extension modes: the first is when compressing force has cancelled, and three sections of manganese steel casing are upheld；Second is manganese steel
When item is inhaled into engine, manganese steel casing is stretched.
7. a kind of aerial thunder of countering intrusions aircraft as described in claim 1, characterized in that
The explosive is equipped with explosive fuse, and the explosive fuse is connect with explosive, using pressure trigger or noise trigger.
8. a kind of working method of the aerial thunder of countering intrusions aircraft, characterized in that include:
When discovery has intruder, flight controller controls rocket engine and starts, and after rocket launching, rocket radar is according to thunder
Up to the real time position of the intruder of locking, the flight controller control ejector of rocket flight to specified region, rocket will be carried
Aerial thunder pop-up in object storehouse；Aerial thunder scatters out self-contained seed thunder within the scope of setting time after pop-up；Seed
Liquid helium air parcel in each cavity of grain thunder becomes gaseous state helium, and first, second, and third cavity is by gaseous state helium
It is full of；Outer layer metal shell buckles under the action of helium atmosphere expansive force releases snap-fit relationship, and outer layer metal shell is from outer layer gas bag
It falls off on the outside of wall；Seed thunder suspends in the sky；So far, seed thunder is routed to specified region in the air；
When intruder enters specified region, seed thunder is inhaled into the engine of intruder；All gas of seed thunder
Containment wall is broken by the blade of engine；Telescopic manganese steel item is stretched over longest state, damages the engine blade of rotation, fries
Medicine demolishs engine.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811559056.5A CN109813187B (en) | 2018-12-19 | 2018-12-19 | Air mine for anti-invasion airplane and working method thereof |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811559056.5A CN109813187B (en) | 2018-12-19 | 2018-12-19 | Air mine for anti-invasion airplane and working method thereof |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN109813187A true CN109813187A (en) | 2019-05-28 |
| CN109813187B CN109813187B (en) | 2021-05-04 |
Family
ID=66602241
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201811559056.5A Active CN109813187B (en) | 2018-12-19 | 2018-12-19 | Air mine for anti-invasion airplane and working method thereof |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN109813187B (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113218250A (en) * | 2021-03-05 | 2021-08-06 | 山东中泰新能源集团有限公司 | Method and facility for protecting safety of air-raid shelter |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3536010A (en) * | 1968-09-23 | 1970-10-27 | Bengt Robert Wilhelm Moldeus | Cartridges |
| CN1351702A (en) * | 1999-04-20 | 2002-05-29 | 西·瓦尔韦工程有限公司 | Apparatus for land, sea and air defence |
| JP2003227700A (en) * | 2002-02-06 | 2003-08-15 | Masayoshi Suzuki | Defensive projectile of missile or the like |
| CN101832740A (en) * | 2010-05-27 | 2010-09-15 | 朱恩灿 | Airspace defense method and air floating mine thereof |
| EP3141695A1 (en) * | 2015-09-09 | 2017-03-15 | Dominique Balleur | System and method for fracturing solid material |
| CN106931838A (en) * | 2017-02-20 | 2017-07-07 | 郭远军 | One kind inflation igniting integrated air blaster |
| CN107101538A (en) * | 2017-06-22 | 2017-08-29 | 中国人民解放军防化学院 | A kind of body encapsulated suitable for pressure |
-
2018
- 2018-12-19 CN CN201811559056.5A patent/CN109813187B/en active Active
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3536010A (en) * | 1968-09-23 | 1970-10-27 | Bengt Robert Wilhelm Moldeus | Cartridges |
| CN1351702A (en) * | 1999-04-20 | 2002-05-29 | 西·瓦尔韦工程有限公司 | Apparatus for land, sea and air defence |
| JP2003227700A (en) * | 2002-02-06 | 2003-08-15 | Masayoshi Suzuki | Defensive projectile of missile or the like |
| CN101832740A (en) * | 2010-05-27 | 2010-09-15 | 朱恩灿 | Airspace defense method and air floating mine thereof |
| EP3141695A1 (en) * | 2015-09-09 | 2017-03-15 | Dominique Balleur | System and method for fracturing solid material |
| CN106931838A (en) * | 2017-02-20 | 2017-07-07 | 郭远军 | One kind inflation igniting integrated air blaster |
| CN107101538A (en) * | 2017-06-22 | 2017-08-29 | 中国人民解放军防化学院 | A kind of body encapsulated suitable for pressure |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113218250A (en) * | 2021-03-05 | 2021-08-06 | 山东中泰新能源集团有限公司 | Method and facility for protecting safety of air-raid shelter |
Also Published As
| Publication number | Publication date |
|---|---|
| CN109813187B (en) | 2021-05-04 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US6626077B1 (en) | Intercept vehicle for airborne nuclear, chemical and biological weapons of mass destruction | |
| US8783185B2 (en) | Liquid missile projectile for being launched from a launching device | |
| US7322267B1 (en) | Enhanced light weight armor system with reactive properties | |
| EP2685206A2 (en) | Projectile-deployed countermeasure system and method | |
| CN105539788B (en) | A kind of underwater aircraft carrier | |
| CN207734492U (en) | Fire extinguisher bomb and its emission system | |
| Tilford | Air Power Lessons | |
| WO2008114261A2 (en) | Fence | |
| CN109813187A (en) | A kind of aerial thunder and its working method of countering intrusions aircraft | |
| US7546795B1 (en) | Enhanced light weight armor system with deflective operation | |
| CN102338596A (en) | Defense weapon for aerospace vehicle | |
| KR102033772B1 (en) | Munition | |
| US20190359330A1 (en) | Airborne space anti-missile system | |
| CN111981901B (en) | Portable self-spinning rocket projectile weapon | |
| RU2314482C1 (en) | Anti-submarine air bombs | |
| RU2781555C1 (en) | Kosteniuk aerostat salvo launch system (asls) | |
| RU2377493C2 (en) | Method of hitting vulnerable ground targets by supersonic missile and device to this effect | |
| CN209885080U (en) | Novel fire-fighting cannonball and launching system thereof | |
| RU2680919C1 (en) | Mobile active device for protection of different objects from unmanned controlled automotive weapons | |
| RU2590760C2 (en) | Missile and method for its operating | |
| US20190000022A1 (en) | Method and apparatus for elimination or reduction of the destructive force of spiraling wind storms | |
| Dullum | The rocket artillery reference book | |
| US20200346054A1 (en) | Airburst delivery system | |
| RO134057A2 (en) | Portable multi-tube ballistic system | |
| Bolonkin | AB-Net Method of Protection from Projectiles (city, military base, battle-front, etc.) |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant |