CN107014248A - A kind of elastomeric construction formula fast aeration decoy aircraft - Google Patents
A kind of elastomeric construction formula fast aeration decoy aircraft Download PDFInfo
- Publication number
- CN107014248A CN107014248A CN201710337171.7A CN201710337171A CN107014248A CN 107014248 A CN107014248 A CN 107014248A CN 201710337171 A CN201710337171 A CN 201710337171A CN 107014248 A CN107014248 A CN 107014248A
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- CN
- China
- Prior art keywords
- decoy aircraft
- decoy
- ammunition
- aircraft
- long body
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- 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.)
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Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B1/00—Explosive charges characterised by form or shape but not dependent on shape of container
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B25/00—Fall bombs
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B30/00—Projectiles or missiles, not otherwise provided for, characterised by the ammunition class or type, e.g. by the launching apparatus or weapon used
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
The present invention relates to a kind of elastomeric construction formula fast aeration decoy aircraft.It is characterized in that whole decoy aircraft is before unaerated opening, its contour structures plays three-dimensional-structure in long, and long body is divided into three parts：Long body front section is unaerated decoy aircraft collection magazine part, the part is made up of magazine shell, the decoy aircraft of unaerated folding, the work barrel being arranged in decoy aircraft, and the work barrel includes gas and occurs control circuit and gas generator and high-explosive projectile and high-explosive projectile ignition radar composition；Long body stage casing heat insulating part；Long body back segment ammunition propulsive units, the part is made up of ammunition housing, propulsion ammunition；The long body stage casing heat insulating part is mainly the heat for producing ammunition propulsive units and obstructed.A kind of elastomeric construction formula fast aeration decoy aircraft of the present invention has simple, the novel advantage of structure that is skillfully constructed, and reaches target overhead time short speed block, and with short production cycle, cost is low.
Description
Technical field
The invention belongs to weapons field, a kind of elastomeric construction formula fast aeration decoy aircraft is related specifically to.
Background technology
In modern war, system sky and the relation that air defense is a pair of lances and shield.As attack a side often through guided missile,
Cannon, bomber, fighter plane are attacked enemy, and the side defended then passes through radar, air defence missile, cannon, fighter plane
Interception strike is carried out Deng guided missile, bomber, fighter plane to attacker etc., serious damage will certainly be just caused as attacker
Lose.Although can be scouted in advance to the deployment such as enemy radar, guided missile, cannon, fighter plane as attacker, enemy is used as
Corresponding hidden camouflage can be done, it is difficult to accomplish very accurate information.To reduce the loss of attack, each state, which has all done, largely grinds
Study carefully, the specific example of a battle the most successful will count strike Middle East state of Israel.Before formal attack, Israel is using a large amount of cheap unmanned planes
Middle East state overhead is flown to as bait, the state is greatly nervous, open radar, launch a guided missile, artillery shooting takes off progress
Air battle etc., while the substantial amounts of guided missile of enemy, shell is consumed, enemy also exposes target of deploying troops on garrison duty.During formal attack, with color
The target of deploying troops on garrison duty that row are exposed using cruise missile, ground-to-ground missile, air-to-ground guided missile to the state has carried out accurate destructive beat
Hit, achieve extraordinary combat success, and Israel only have lost some cheap unmanned planes.But unmanned plane reaches target overhead
Time long speed it is slow, the production cycle is long, and cost is also of a relatively high, the problem of cost is high when substantial amounts of unmanned plane goes into battle
It is more prominent.How to overcome slow as the time long speed in bait machine arrival target overhead with unmanned plane, the production cycle is long, cost
High the problem of, reaches target overhead time short speed block there is provided one kind, and with short production cycle, the low elastomeric construction formula of cost is quickly filled
Gas decoy aircraft, just into the Main Topics of the present invention.
The content of the invention
The purpose of the present invention, seeks to overcome and existing reaches target overhead time long speed as bait machine with unmanned plane
Slowly, the production cycle is long, and the problem of cost is high reaches target overhead time short speed block there is provided one kind, and with short production cycle, cost is low
Elastomeric construction formula fast aeration decoy aircraft.
In order to realize the above object, the present invention is achieved through the following technical solutions.A kind of elastomeric construction formula is fast
Fast inflatable decoy aircraft, it is characterised in that whole decoy aircraft is before unaerated opening, and its contour structures is in long body type knot
Structure, long body is divided into three parts：Long body front section is unaerated decoy aircraft collection magazine part, and the part is outside magazine
Shell, the decoy aircraft of unaerated folding, the work barrel being arranged in decoy aircraft composition, the work barrel are controlled including gas
Circuit and gas generator and high-explosive projectile and high-explosive projectile processed ignite radar composition；Long body stage casing heat insulating part；Long body back segment
Ammunition propulsive units, the part is made up of ammunition housing, propulsion ammunition；The long body stage casing heat insulating part is mainly by ammunition
The heat that propulsive units is produced is obstructed, to prevent heat transfer to unaerated decoy aircraft collection magazine part.
Further, above-described inflatable decoy aircraft is answered by the lax ultrathin non-woven fabrics of evaporation aluminium film and hole
What the film closed was made, to there is enough intensity, the one of the evaporation aluminium film faces outwardly to increase the back wave of chamber radar wave.
Further, above-described gas generator is multi-stage ignition formula gas generator, and its inflation of lighting a fire is by gas
Body generation control circuit uses multi-stage ignition formula gas generator and produced when being expanded with preventing that disposable igniting is rapid come what is controlled
Heat excessively assemble and damage inflatable decoy aircraft, in order to prevent inflatable decoy aircraft inner gas pressure too high and cause rupture,
Inflatable decoy aircraft is provided with pressure-reducing valve.
Further, above-described elastomeric construction formula fast aeration decoy aircraft can be divided into airborne releasing type and heavy caliber
Guide vane is provided with Canon launching formula, the ammunition housing of the ammunition propulsive units of airborne releasing type, to prevent ammunition igniting from pushing away
The whole nondirectional unrest of body flies when entering.
Further, the magazine shell of above-described unaerated decoy aircraft collection magazine part, at least two panels or
Circular arc housing more than two panels is spliced.
Further, above-described gas occurs to control circuit to be long-range wireless remote control ignition control circuit or timing point
Fire control circuit.
A kind of elastomeric construction formula fast aeration decoy aircraft of the present invention so works：In the air by opportunity of combat to mesh
Mark spatial domain to deliver or in ground large caliber gun to target spatial domain launch, when reaching target spatial domain, controlled by gas
Circuit processed makes multi-stage ignition formula gas generator light a fire step by step to the inflation of inflatable decoy aircraft, and unaerated under the influence of air pressure is lured
The magazine shell division of bait aircraft collection magazine part is scattered, and multi-stage ignition formula gas generator continues to light a fire to filling in the short time
Gas decoy aircraft is inflated, and inflatable decoy aircraft is full of after gas, just forms decoy aircraft in target spatial domain, when substantial amounts of bait flies
When machine occurs suddenly in the spatial domain of enemy, radar start or missile emplacements launching trajectory or the cannon position hair of enemy just can be lured into
Shell or field takeoff aircraft etc. are penetrated, enemy firepower is largely consumed, enemy's exposure is deployed troops on garrison duty and is easy to us to attack exactly enemy,
When enemy, which takes off, enters the investigative range of high-explosive projectile ignition radar close to inflatable decoy aircraft, high-explosive projectile is ignited radar and connect
Receive reflection electromagnetic wave and just ignite high-explosive projectile and injure and shoot down enemy plane, war victory is obtained with minimum cost.
A kind of elastomeric construction formula fast aeration decoy aircraft that technical scheme more than can be seen that the present invention has
It is skillfully constructed simple, the novel advantage of structure, and target overhead time short speed block is reached, with short production cycle, cost is low.
In order to better illustrate the present invention, it is described further in conjunction with specific embodiment and its accompanying drawing.
Brief description of the drawings
Fig. 1 is the outside drawing of airborne releasing type of the invention.
The A-A that Fig. 2 is Fig. 1 cuts open cut-away view.
Fig. 3 is the position view of work barrel internally after present invention inflation.
Fig. 4 is the schematic top plan view after inflatable decoy aircraft inflation of the present invention.
Fig. 5 is the front schematic view after inflatable decoy aircraft inflation of the present invention.
Fig. 6 is the side schematic view after inflatable decoy aircraft inflation of the present invention.
Fig. 7 is the outside drawing of large caliber gun emission-type of the present invention.
In figure：1- ammunition propulsive unitses；2- unaerateds decoy aircraft collection magazine part；3- leading portion magazine shells；4- fills
Gas decoy aircraft；5- work barrels；6- multi-stage ignition formula gas generators；7- long-range wireless remote control ignition control circuits；8- height is quick-fried
Bullet ignites radar；9- guide vanes；10- ignites radar igniter；The igniter of 11- gas generators；12- pressure-reducing valves；The long bullets of 13-
Body stage casing heat insulating part；14- high-explosive projectiles.
Embodiment
As can be seen that the present invention is before unaerated opening in each accompanying drawing more than, its contour structures plays three-dimensional-structure in length, long
Body is divided into three parts：Long body front section is unaerated decoy aircraft collection magazine part 2, the part by magazine shell 3,
The inflatable decoy aircraft 4 of unaerated folding, the work barrel 5 being arranged in decoy aircraft are constituted, and the work barrel 5 includes long-range nothing
Line remote control ignition controls circuit 7 and multi-stage ignition formula gas generator 6 and high-explosive projectile 14 and high-explosive projectile ignition radar 8 to constitute；It is long
Body stage casing heat insulating part 13；Long body back segment ammunition propulsive units 1, the part is made up of ammunition housing, propulsion ammunition；It is described
Long body stage casing heat insulating part is mainly the heat that produces ammunition propulsive units and obstructed, to prevent heat transfer to not filling
The collection magazine of gas decoy aircraft 4 part.Described inflatable decoy aircraft 4 is by the lax ultrathin nonwoven of evaporation aluminium film and hole
What the film that cloth is composited was made, to there is enough intensity, the one of the evaporation aluminium film faces outwardly to strengthen the anti-of radar wave
Ejected wave.Its inflation of lighting a fire is controlled by long-range wireless remote control ignition control circuit 7, using multi-stage ignition formula gas generator
The heat produced when being expanded with preventing that disposable igniting is rapid is excessively assembled and damages inflatable decoy aircraft 4, in order to prevent inflation
The inner gas pressure of decoy aircraft 4 is too high and causes rupture, and inflatable decoy aircraft 4 is provided with pressure-reducing valve 12.Figure 1 above is elastomeric construction
The airborne releasing type of formula fast aeration decoy aircraft, Fig. 7 is elastomeric construction formula fast aeration decoy aircraft large caliber gun emission-type,
Guide vane 9 is provided with the ammunition housing of the ammunition propulsive units of airborne releasing type, to prevent whole bullet during ammunition igniting propulsion
The nondirectional unrest of body flies.The magazine shell 3 of unaerated decoy aircraft collection magazine part is four four points as shown in Figure 1 and Figure 7
One of circular arc housing be spliced.
A kind of elastomeric construction formula fast aeration decoy aircraft of the present invention so works：In the air by opportunity of combat to mesh
Spatial domain is marked to deliver or in ground large caliber gun to target spatial domain launch, it is distant by long distance wireless when reaching target spatial domain
Control ignition control circuit 7 makes the igniter 11 of multi-stage ignition formula gas generator 6 light a fire step by step to inflate inflatable decoy aircraft 4,
The division of magazine shell 3 of the collection magazine of unaerated decoy aircraft 4 part is scattered under the influence of air pressure, multi-stage ignition in the short time
Formula gas generator 6 continues to light a fire to be inflated to inflatable decoy aircraft 4, and inflatable decoy aircraft 4 is full of after gas, just in target spatial domain shape
Into decoy aircraft 4, when substantial amounts of decoy aircraft 4 occurs suddenly in the spatial domain of enemy, the radar start of enemy just can be lured into
Or missile emplacements launching trajectory or cannon position fire shells or field takeoff aircraft etc., largely consume enemy firepower, make enemy
Exposure, which is deployed troops on garrison duty, is easy to us to attack exactly enemy, is ignited when enemy takes off close to inflatable decoy aircraft 4 into high-explosive projectile
During the investigative range of radar, when high-explosive projectile ignition radar receives reflection electromagnetic wave, just draw the igniting of ignition radar igniter 10
Quick-fried high-explosive projectile, which is injured, shoots down enemy plane, and war victory is obtained with minimum cost.
A kind of elastomeric construction formula fast aeration decoy aircraft that technical scheme more than can be seen that the present invention has
It is skillfully constructed simple, the novel advantage of structure, and target overhead time short speed block is reached, with short production cycle, cost is low.
Enumerated above is only two kinds of embodiments, and also some other embodiments can not be enumerated, Fan Yiben
The modification modification extension that invention protection domain is made is improved, and belongs to protection scope of the present invention.
Claims (6)
1. a kind of elastomeric construction formula fast aeration decoy aircraft, it is characterised in that whole decoy aircraft before unaerated opening,
Its contour structures plays three-dimensional-structure in long, and long body is divided into three parts：Long body front section is collected for unaerated decoy aircraft
Magazine part, the part is made up of magazine shell, the decoy aircraft of unaerated folding, the work barrel being arranged in decoy aircraft,
The work barrel includes gas and occurs control circuit and gas generator and high-explosive projectile and high-explosive projectile ignition radar composition；Long body
Stage casing heat insulating part；Long body back segment ammunition propulsive units, the part is made up of ammunition housing, propulsion ammunition；The long body
Stage casing heat insulating part is mainly the heat for producing ammunition propulsive units and obstructed.
2. a kind of elastomeric construction formula fast aeration decoy aircraft according to claim 1, it is characterised in that described inflation
Decoy aircraft is made up of the lax ultrathin non-woven fabric compounded film of evaporation aluminium film and hole, the evaporation aluminium film
One faces outwardly to strengthen the back wave of radar wave.
3. a kind of elastomeric construction formula fast aeration decoy aircraft according to claim 1, it is characterised in that described gas
Generator is multi-stage ignition formula gas generator, and its inflation of lighting a fire is by gas occurs to control circuit to control, inflatable decoy
Aircraft is provided with pressure-reducing valve.
4. a kind of elastomeric construction formula fast aeration decoy aircraft according to claim 1, it is characterised in that described body
Structural formula fast aeration decoy aircraft can be divided into airborne releasing type and large caliber gun emission-type, and the ammunition of airborne releasing type is promoted
Guide vane is provided with partial ammunition housing.
5. a kind of elastomeric construction formula fast aeration decoy aircraft according to claim 1, it is characterised in that described does not fill
Circular arc housing more than magazine shell, at least two panels or the two panels of gas decoy aircraft collection magazine part is spliced.
6. a kind of elastomeric construction formula fast aeration decoy aircraft according to claim 1, it is characterised in that described gas
Generation controls circuit to be long-range wireless remote control ignition control circuit or timing ignition control circuit.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710337171.7A CN107014248A (en) | 2017-05-14 | 2017-05-14 | A kind of elastomeric construction formula fast aeration decoy aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710337171.7A CN107014248A (en) | 2017-05-14 | 2017-05-14 | A kind of elastomeric construction formula fast aeration decoy aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107014248A true CN107014248A (en) | 2017-08-04 |
Family
ID=59448960
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710337171.7A Pending CN107014248A (en) | 2017-05-14 | 2017-05-14 | A kind of elastomeric construction formula fast aeration decoy aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107014248A (en) |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2050585U (en) * | 1989-03-31 | 1990-01-03 | 陆勇荣 | Soft bullets |
| US6745696B1 (en) * | 1999-03-25 | 2004-06-08 | Rafael-Armament Development Authority Ltd. | Armor piercing projectile |
| CN1634748A (en) * | 2003-12-27 | 2005-07-06 | 陈绍勇 | Radar preventing and infrared preventing bomb type inflated simulated airplane for protecting airplane |
| CN206739996U (en) * | 2017-05-14 | 2017-12-12 | 福州幻科机电科技有限公司 | A kind of elastomeric construction formula fast aeration decoy aircraft |
-
2017
- 2017-05-14 CN CN201710337171.7A patent/CN107014248A/en active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2050585U (en) * | 1989-03-31 | 1990-01-03 | 陆勇荣 | Soft bullets |
| US6745696B1 (en) * | 1999-03-25 | 2004-06-08 | Rafael-Armament Development Authority Ltd. | Armor piercing projectile |
| CN1634748A (en) * | 2003-12-27 | 2005-07-06 | 陈绍勇 | Radar preventing and infrared preventing bomb type inflated simulated airplane for protecting airplane |
| CN206739996U (en) * | 2017-05-14 | 2017-12-12 | 福州幻科机电科技有限公司 | A kind of elastomeric construction formula fast aeration decoy aircraft |
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| PB01 | Publication | ||
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Application publication date: 20170804 |