CN114166078A - Double-stealth air-to-air missile - Google Patents
Double-stealth air-to-air missile Download PDFInfo
- Publication number
- CN114166078A CN114166078A CN202111365785.9A CN202111365785A CN114166078A CN 114166078 A CN114166078 A CN 114166078A CN 202111365785 A CN202111365785 A CN 202111365785A CN 114166078 A CN114166078 A CN 114166078A
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- CN
- China
- Prior art keywords
- air
- missile
- stealth
- cartridge case
- compressed air
- 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.)
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- 238000001514 detection method Methods 0.000 claims abstract description 8
- 239000000446 fuel Substances 0.000 claims abstract description 7
- 239000002737 fuel gas Substances 0.000 claims abstract description 7
- 239000002828 fuel tank Substances 0.000 claims abstract description 5
- 239000002360 explosive Substances 0.000 claims abstract description 4
- 239000007921 spray Substances 0.000 claims description 10
- 239000011358 absorbing material Substances 0.000 claims description 3
- 230000007774 longterm Effects 0.000 claims description 3
- 239000000463 material Substances 0.000 claims description 3
- 238000000034 method Methods 0.000 claims description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims description 2
- 230000009977 dual effect Effects 0.000 claims 2
- 238000004519 manufacturing process Methods 0.000 abstract description 2
- 239000007789 gas Substances 0.000 description 2
- 238000002485 combustion reaction Methods 0.000 description 1
- 230000001105 regulatory effect Effects 0.000 description 1
Images
Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B5/00—Cartridge ammunition, e.g. separately-loaded propellant charges
- F42B5/26—Cartridge cases
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
- F42B10/60—Steering arrangements
- F42B10/66—Steering by varying intensity or direction of thrust
- F42B10/668—Injection of a fluid, e.g. a propellant, into the gas shear in a nozzle or in the boundary layer at the outer surface of a missile, e.g. to create a shock wave in a supersonic flow
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B12/00—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
- F42B12/72—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the material
- F42B12/76—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the material of the casing
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B12/00—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
- F42B12/72—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the material
- F42B12/76—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the material of the casing
- F42B12/80—Coatings
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Fluid Mechanics (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
The invention relates to a double-stealth air-to-air missile which comprises a missile body (1). The projectile body (1) comprises a projectile shell, an explosive, a detection device and a control device. The rear shell case (2) of the shell case stores compressed air (3) in the inner cavity, and the rear end of the shell case is provided with a vectoring nozzle (4). The electromagnetic wave stealth technology is adopted, and the normal-temperature compressed air (3) is used for replacing high-temperature fuel gas generated by burning fuel of a jet engine on a traditional air-air missile, so that the obvious infrared characteristic of the traditional air-air missile is eliminated, the jet engine, a fuel tank and fuel on the traditional air-air missile are also saved, and the manufacturing cost is greatly reduced; the 'fast' and 'hidden' are mutually matched and cooperated, the power is greatly increased, the enemy aircraft can be efficiently killed, and the aircraft can be effectively self-protected, thereby achieving two purposes at one time; the rear cartridge case (2) is also a container for compressed air (3), so that the weight is reduced. The double stealth technology is not complex, but can be taken first by first adoption.
Description
Technical Field
The invention relates to a double-stealth air-to-air missile, in particular to a double-stealth air-to-air missile with stealth electromagnetic waves and infrared rays.
Background
The current air-to-air missile generally realizes electromagnetic wave stealth and radar is difficult to detect, but because the jet engine of the missile sprays high-temperature gas, the infrared characteristics are very obvious, infrared detection equipment is easy to discover, and enemy aircrafts can still avoid in advance.
In order to improve the hit rate of the air-to-air missile, besides the electromagnetic wave stealth technology is continuously adopted, the infrared characteristics of the air-to-air missile need to be eliminated by a mutual method, so that the infrared stealth is realized.
Disclosure of Invention
The invention aims to solve the technical problem of providing a double-stealth air-air missile which is stealthy in both electromagnetic waves and infrared rays.
In order to solve the technical problem, the technical scheme of the invention is as follows:
a double-stealth air-to-air missile comprises a missile body.
The bomb body comprises a bomb shell, explosive, a detection device and a control device.
The cartridge case is not provided with a jet engine, a fuel tank and fuel, has an electromagnetic wave stealth structure, is sprayed with an electromagnetic wave absorbing material on the outer surface, cannot be detected by an enemy radar, and has an electromagnetic wave stealth characteristic.
The rear cartridge case of the cartridge case is a rear cartridge case.
The back shell casing is made of high-strength material, its inner surface can bear pressure greater than 100 atm, its inner cavity can store high-pressure normal-temp. compressed air, and its rear end is equipped with vector jet pipe.
The pressure of the compressed air is greater than 100 atmospheres.
The compressed air stored in the inner cavity of the rear cartridge case is ejected at high speed through the vectoring nozzle under the control of the control device to push the projectile body to advance at high speed or change the direction rapidly; the control device also controls the flow of compressed air through the vectoring nozzle to regulate the velocity of the projectile.
The vector spray pipe sprays normal temperature air, so that the infrared characteristics of high-temperature fuel gas sprayed by the traditional missile jet engine are eliminated, and enemy infrared detection equipment cannot detect the high-temperature fuel gas, so that the vector spray pipe has the infrared stealth characteristic.
The larger the volume of the inner cavity of the rear shell case is, the larger the pressure of the compressed air is, and the larger the flying speed is, the longer the flying time is, and the stronger the power is.
The water in the compressed air is removed to facilitate long-term storage.
After the structure is adopted, the double-stealth air-air missile uses normal-temperature compressed air to replace high-temperature gas generated by combustion of fuel of a jet engine on the traditional missile, so that the obvious infrared characteristic of the traditional air-air missile is eliminated, the jet engine, a fuel tank and fuel on the traditional air-air missile are also saved, and the manufacturing cost is greatly reduced. This is one of the great creations of the invention.
After the structure is adopted, the compressed air carried by the double-stealth air-air missile is ejected at a high speed, and the double-stealth air-air missile can be pushed to advance at a high speed or change the direction rapidly. Because the known electromagnetic wave stealth technology is adopted and the infrared stealth technology is adopted, the double stealth air-to-air missile thoroughly realizes double stealth. Wu Gong can only quickly and only insignificantly break. The 'fast' and 'hidden' of the double-stealth air-to-air missile are mutually matched and cooperated, the power is greatly increased, the enemy aircraft can be efficiently killed, and the double-stealth air-to-air missile can effectively protect the enemy aircraft. This is the second significant creation of the present invention.
After the structure is adopted, the rear shell of the double-stealth air-space missile is also used as a container of compressed air, so that the weight is reduced. This is the third significant creation of the present invention.
The double stealth technology is not complex, but firstly adopts the technology which can take the first plane, and the fighting force generated by the first plane can last for more than ten years.
Drawings
The following describes embodiments of the present invention in further detail with reference to the accompanying drawings.
FIG. 1 is a schematic illustration of a double stealth air-to-air missile hull, but with the rear hull and nozzle in section.
Detailed Description
As shown in figure 1, the double-stealth air-to-air missile comprises a missile body 1.
As shown in fig. 1, the projectile body 1 comprises a hull, an explosive, a detection device and a control device.
The cartridge case is not provided with a jet engine, a fuel tank and fuel, has an electromagnetic wave stealth structure, is sprayed with an electromagnetic wave absorbing material on the outer surface, cannot be detected by an enemy radar, and has an electromagnetic wave stealth characteristic.
As shown in fig. 1, the rear case of the case is a rear case 2.
As shown in fig. 1, the rear cartridge case 2, which is made of a high-strength material and whose inner surface can withstand a pressure of more than 100 atm, stores high-pressure normal-temperature compressed air 3 in its inner cavity, and is provided with a vectoring nozzle 4 at its rear end.
The pressure of the compressed air 3 is greater than 100 atmospheres.
The compressed air 3 stored in the inner cavity of the rear cartridge case 2 is ejected at high speed through the vectoring nozzle 4 under the control of the control device to push the projectile body 1 to advance at high speed or change the direction rapidly; the control also controls the flow of compressed air 3 through the vectoring nozzle 4, regulating the velocity of the projectile 1.
The vector spray pipe 4 sprays normal temperature air, so that the infrared characteristics of high-temperature fuel gas sprayed by the traditional missile jet engine are eliminated, and enemy infrared detection equipment cannot detect the high-temperature fuel gas, so that the vector spray pipe has the infrared stealth characteristic.
The larger the volume of the inner cavity of the rear missile shell 2 is, the larger the pressure of the compressed air 3 is, and the larger the flying speed is, the longer the flying time is, and the stronger the power is.
The compressed air 3 is dehumidified to facilitate long-term storage.
The embodiments of the present invention are described in detail above with reference to the accompanying drawings. The present invention is not limited to the above-described embodiments, and various changes can be made without departing from the spirit of the present invention within the knowledge of those skilled in the art. Variations that do not depart from the gist of the invention are intended to be within the scope of the invention.
Claims (3)
1. A double-stealth air-to-air missile comprises a missile body (1);
the bomb body (1) comprises a bomb shell, an explosive, a detection device and a control device;
the method is characterized in that:
the cartridge case is not provided with a jet engine, a fuel tank and fuel, has an electromagnetic wave stealth structure, is sprayed with an electromagnetic wave absorbing material on the outer surface, cannot be detected by an enemy radar, and has an electromagnetic wave stealth characteristic;
the rear cartridge case of the cartridge case is a rear cartridge case (2);
the rear cartridge case (2) is made of high-strength materials, the inner surface of the rear cartridge case can bear pressure of more than 100 atmospheric pressure, high-pressure normal-temperature compressed air (3) is stored in an inner cavity of the rear cartridge case, and a vectoring nozzle (4) is installed at the rear end of the rear cartridge case;
the pressure of the compressed air (3) is greater than 100 atmospheres;
compressed air (3) stored in the inner cavity of the rear cartridge case (2) is ejected at high speed through the vectoring nozzle (4) under the control of the control device to push the projectile body (1) to advance at high speed or change the direction rapidly; the control device also controls the flow of compressed air (3) through the vectoring nozzle (4) to regulate the velocity of the projectile (1);
the vector spray pipe (4) sprays normal temperature air, so that the infrared characteristics of high-temperature fuel gas sprayed by the traditional missile jet engine are eliminated, and enemy infrared detection equipment cannot detect the high-temperature fuel gas, so that the vector spray pipe has the infrared stealth characteristic.
2. The dual stealth air-to-air missile of claim 1, wherein:
the larger the volume of the inner cavity of the rear missile shell (2) is, the larger the pressure of the compressed air (3) is, the larger the flying speed is, the longer the flying time is, and the stronger the power is.
3. The dual stealth air-to-air missile of claim 1, wherein:
the water in the compressed air (3) is removed to facilitate long-term storage.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202111365785.9A CN114166078A (en) | 2021-11-10 | 2021-11-10 | Double-stealth air-to-air missile |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202111365785.9A CN114166078A (en) | 2021-11-10 | 2021-11-10 | Double-stealth air-to-air missile |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN114166078A true CN114166078A (en) | 2022-03-11 |
Family
ID=80479485
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202111365785.9A Withdrawn CN114166078A (en) | 2021-11-10 | 2021-11-10 | Double-stealth air-to-air missile |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN114166078A (en) |
-
2021
- 2021-11-10 CN CN202111365785.9A patent/CN114166078A/en not_active Withdrawn
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| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
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| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20220311 |
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| WW01 | Invention patent application withdrawn after publication |