CN111156864A - Bullet bottom separation mass-reducing range-extending cannonball - Google Patents
Bullet bottom separation mass-reducing range-extending cannonball Download PDFInfo
- Publication number
- CN111156864A CN111156864A CN202010121090.5A CN202010121090A CN111156864A CN 111156864 A CN111156864 A CN 111156864A CN 202010121090 A CN202010121090 A CN 202010121090A CN 111156864 A CN111156864 A CN 111156864A
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- CN
- China
- Prior art keywords
- solid
- bomb
- solid motor
- projectile
- bullet
- 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.)
- Pending
Links
- 238000000926 separation method Methods 0.000 title claims abstract description 13
- 239000007787 solid Substances 0.000 claims abstract description 51
- 230000007246 mechanism Effects 0.000 claims abstract description 19
- 238000002485 combustion reaction Methods 0.000 claims abstract description 4
- 230000009467 reduction Effects 0.000 claims description 2
- 238000000034 method Methods 0.000 abstract description 14
- 230000008569 process Effects 0.000 abstract description 9
- 238000005507 spraying Methods 0.000 abstract description 2
- 239000007921 spray Substances 0.000 description 5
- 239000007789 gas Substances 0.000 description 4
- 230000009471 action Effects 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 239000002737 fuel gas Substances 0.000 description 2
- 239000003721 gunpowder Substances 0.000 description 2
- 239000003380 propellant Substances 0.000 description 2
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 1
- 229910052802 copper Inorganic materials 0.000 description 1
- 239000010949 copper Substances 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 238000007789 sealing Methods 0.000 description 1
Images
Classifications
-
- 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
- F42B10/32—Range-reducing or range-increasing arrangements; Fall-retarding means
- F42B10/38—Range-increasing arrangements
-
- 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
Landscapes
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
本发明公开一种弹底分离减质增程炮弹，依次包括战斗部、固体发动机以及分离弹底机构；固体发动机包括固体发动机壳体、固体发动机药筒、用于喷出燃烧产物的喷管以及固发点火器；固体发动机药筒设置于固体发动机壳体内部；分离弹底机构包括弹底、底排壳体和底排点火器。本发明利用底排装药和固体发动机装药产生的燃气将分离弹底机构与弹丸分离，固体发动机继续推动剩余的有效载荷飞行；通过分离弹底机构有效得减少了弹丸飞行过程中的消极质量，到达在同等装药条件下弹丸飞行的距离更远的目的。这种分离弹底的设计方法有效地减少了弹丸空中飞行过程的消极质量，且方法简单，便于实现，具有安全可靠，使用要求低。
The invention discloses a bottom-separated mass-reduced and extended-range artillery shell, which sequentially includes a warhead, a solid motor and a bottom-separating mechanism; the solid motor comprises a solid motor casing, a solid motor cartridge, a nozzle for spraying combustion products, and The solid engine igniter; the solid engine cartridge is arranged inside the solid engine casing; the bomb bottom separation mechanism comprises a bomb bottom, a bottom row casing and a bottom row igniter. The invention utilizes the gas generated by the bottom row charge and the solid motor charge to separate the separation bomb bottom mechanism from the projectile, and the solid motor continues to drive the remaining payload to fly; the separation of the bomb bottom mechanism effectively reduces the negative mass during the flight of the projectile , to achieve the purpose of the projectile flying farther under the same charge condition. The design method of separating the bottom of the bomb effectively reduces the negative quality of the projectile in the air flight process, and the method is simple, easy to implement, safe and reliable, and has low requirements for use.
Description
Technical Field
The invention relates to the field of middle trajectory, in particular to a projectile with separated projectile bottom and reduced mass and increased range.
Background
The projectile bottom structure of the artillery projectile mainly has the main functions of bearing high overload during launching, protecting a projectile damage part from being damaged by high chamber pressure, and therefore, the structure is thicker and heavier; and the bullet bottom is also provided with a copper sealing bullet belt generally, and the mass of the bullet bottom becomes a negative mass which consumes the flying kinetic energy of the bullet when the bullet flies. That is, the projectile bottom does not play any positive role in the projectile flying process after the projectile leaves the bore, but rather reduces the flying speed of the projectile to a certain extent due to the weight of the projectile bottom. In order to pursue the end-point damage effect with a longer range, bottom row drag reduction and fixed emission range extension are common technical means, however, according to public data, the purpose of range extension achieved by a design method for reducing negative quality is not found.
Disclosure of Invention
The invention aims to provide a projectile with separated projectile bottom and reduced mass and increased range, which aims to solve the problems in the prior art, effectively reduce the negative mass of a projectile in the process of flying through a projectile bottom separating mechanism and achieve the aim of further increasing the flying distance of the projectile under the same charging condition.
In order to achieve the purpose, the invention provides the following scheme:
the invention provides a bullet bottom separation mass-reducing range-extending cannonball, which sequentially comprises a warhead, a solid engine and a separation bullet bottom mechanism; the solid engine comprises a solid engine shell, a solid engine cartridge, a spray pipe for spraying combustion products and a solid-state igniter; the solid engine cartridge is disposed inside the solid engine housing.
The separating bottom ejection mechanism comprises a bottom ejection, a bottom row shell and a bottom row igniter; the outlet of the spray pipe and the bottom row shell are both arranged in the bullet bottom; the bottom row shell is internally provided with a grain containing propellant; one side of the solid engine shell is fixedly connected to the warhead, and the other side of the solid engine shell is connected with the bottom end of the bullet bottom.
Preferably, the base row housing is disposed between the nozzle and the bullet base.
Preferably, the other side of the solid engine shell is sleeved or bonded at the bottom end of the bullet bottom.
Preferably, a bearing is arranged between the solid engine shell and the bullet bottom, and the bearing is fixedly arranged on the solid engine shell. In the process of launching the shell, the separation bullet bottom mechanism rotates at a high speed, and the bullet and the separation bullet bottom mechanism are connected through the bearing, so that the bullet rotates at a low speed under the action of inertia, the rotating speed of a bullet muzzle is effectively reduced, and the control on the bullet in the later period is facilitated. Preferably, the bottom end of the solid engine housing is in interference fit with the bottom end of the bullet bottom.
Preferably, the outer side of the bullet bottom is provided with a bullet belt which can bear high-temperature and high-pressure gas impact, the bullet belt is embedded into rifling during launching, gunpowder gas is sealed, the bullet rotates at a high speed, and stable flight of the bullet is guaranteed.
The invention discloses the following technical effects: the bottom discharge charge and the fuel gas generated by the charge of the solid engine are utilized to separate the bottom separating mechanism from the projectile, and the solid engine continues to push the rest of the payload to fly; the negative mass of the projectile in the flying process is effectively reduced by separating the projectile bottom mechanism, and the aim of further flying distance of the projectile under the same charging condition is fulfilled. The design method for separating the projectile bottom effectively reduces the negative mass of the projectile in the air flight process, is simple and convenient to realize, and has the advantages of safety, reliability and low use requirement.
Drawings
In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings needed to be used in the embodiments will be briefly described below, and it is obvious that the drawings in the following description are only some embodiments of the present invention, and it is obvious for those skilled in the art to obtain other drawings without inventive exercise.
FIG. 1 is a schematic diagram of the projectile of the present invention;
FIG. 2 is a schematic structural diagram of the second embodiment.
Wherein, 1 is bullet bottom, 2 is hair-fixing igniter, 3 is bottom row igniter, 4 is bottom row casing, 5 is spray tube, 6 is solid engine, 7 is hair-fixing cartridge case, 8 is warhead, 9 is bearing.
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.
In order to make the aforementioned objects, features and advantages of the present invention comprehensible, embodiments accompanied with figures are described in further detail below.
Example one
Referring to fig. 1, the present embodiment provides a projectile with separated bullet bottom and reduced mass range, which sequentially comprises a warhead 8, a solid engine and a separated bullet bottom mechanism; the solid engine comprises a solid engine housing 6, a solid engine cartridge 7, a nozzle 5 for ejecting combustion products and a solid ignition igniter 2; a solid engine cartridge 7 is arranged inside the solid engine housing 6.
The separating bullet bottom mechanism comprises a bullet bottom 1, a bottom row shell 4 and a bottom row igniter 3; the outlet of the spray pipe 5 and the bottom row shell 4 are both arranged in the bullet bottom 1; the bottom row shell 4 is arranged between the spray pipe 5 and the bullet bottom 1. The bottom row shell 4 is internally provided with a grain for containing propellant; one side of the solid engine shell 6 is fixedly connected to the warhead 8, the other side of the solid engine shell 6 is sleeved on the inner side end of the bullet bottom 1, and the bottom end of the solid engine shell 6 is in interference fit with the bottom end of the bullet bottom 1, so that the integrity of the bullet is guaranteed. The outside of the bullet bottom 1 is provided with a bullet belt which can bear high-temperature and high-pressure gas impact, the bullet belt is embedded into rifling during launching, gunpowder gas is sealed, the bullet rotates at a high speed, and stable flight of the bullet is guaranteed.
The bottom discharge charge and the fuel gas generated by the charge of the solid engine are utilized to separate the bottom separating mechanism from the projectile, and the solid engine continues to push the rest of the payload to fly; the negative mass of the projectile in the flying process is effectively reduced by separating the projectile bottom mechanism, and the aim of further flying distance of the projectile under the same charging condition is fulfilled. The design method for separating the projectile bottom effectively reduces the negative mass of the projectile in the air flight process, is simple and convenient to realize, and has the advantages of safety, reliability and low use requirement.
Example two
Referring to fig. 2, the present embodiment provides a projectile with separated bullet bottom and reduced mass and increased range, and is different from the first embodiment in that a bearing 9 is arranged between a solid engine shell 6 and the bullet bottom 1, and the bearing 9 is fixedly arranged on the solid engine shell 6. In the process of launching the shell, the separation bullet bottom mechanism rotates at a high speed, the bullet and the separation bullet bottom mechanism are connected through the bearing, and the radial force borne by the bullet is small, so that the bullet rotates at a low speed under the action of inertia, the rotating speed of a bullet muzzle is effectively reduced, and the control of the bullet in the later period is facilitated.
In the description of the present invention, it is to be understood that the terms "longitudinal", "lateral", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", and the like, indicate orientations or positional relationships based on those shown in the drawings, are merely for convenience of description of the present invention, and do not indicate or imply that the referenced devices or elements must have a particular orientation, be constructed and operated in a particular orientation, and thus, are not to be construed as limiting the present invention.
The above-described embodiments are merely illustrative of the preferred embodiments of the present invention, and do not limit the scope of the present invention, and various modifications and improvements of the technical solutions of the present invention can be made by those skilled in the art without departing from the spirit of the present invention, and the technical solutions of the present invention are within the scope of the present invention defined by the claims.
Claims (6)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202010121090.5A CN111156864A (en) | 2020-02-26 | 2020-02-26 | Bullet bottom separation mass-reducing range-extending cannonball |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202010121090.5A CN111156864A (en) | 2020-02-26 | 2020-02-26 | Bullet bottom separation mass-reducing range-extending cannonball |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN111156864A true CN111156864A (en) | 2020-05-15 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202010121090.5A Pending CN111156864A (en) | 2020-02-26 | 2020-02-26 | Bullet bottom separation mass-reducing range-extending cannonball |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111735352A (en) * | 2020-07-13 | 2020-10-02 | 中北大学 | A coaxial parallel charge bottom-discharging drag-reducing projectile bottom-separating mass-reducing and extending-range projectiles |
| IL314183B1 (en) * | 2024-07-01 | 2025-08-01 | Imi Systems Ltd | Long range artillery projectile with auxiliary energetic material for rear casing ejection |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102155878A (en) * | 2010-12-20 | 2011-08-17 | 吉林保利科技中试有限公司 | 130 mm PL59A type base bleed and rocket composite range-enhanced high explosive projectile of howitzer |
| CN103363850A (en) * | 2013-08-06 | 2013-10-23 | 晋西工业集团有限责任公司 | Dispenser type lightning triggering rocket bomb |
| KR101449738B1 (en) * | 2014-07-24 | 2014-10-10 | 주식회사 풍산 | Projectile separation structure by multiple explosive shear breaking devices |
| CN211626279U (en) * | 2020-02-26 | 2020-10-02 | 中北大学 | Bullet bottom separation mass-reducing range-extending cannonball |
-
2020
- 2020-02-26 CN CN202010121090.5A patent/CN111156864A/en active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102155878A (en) * | 2010-12-20 | 2011-08-17 | 吉林保利科技中试有限公司 | 130 mm PL59A type base bleed and rocket composite range-enhanced high explosive projectile of howitzer |
| CN103363850A (en) * | 2013-08-06 | 2013-10-23 | 晋西工业集团有限责任公司 | Dispenser type lightning triggering rocket bomb |
| KR101449738B1 (en) * | 2014-07-24 | 2014-10-10 | 주식회사 풍산 | Projectile separation structure by multiple explosive shear breaking devices |
| CN211626279U (en) * | 2020-02-26 | 2020-10-02 | 中北大学 | Bullet bottom separation mass-reducing range-extending cannonball |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111735352A (en) * | 2020-07-13 | 2020-10-02 | 中北大学 | A coaxial parallel charge bottom-discharging drag-reducing projectile bottom-separating mass-reducing and extending-range projectiles |
| IL314183B1 (en) * | 2024-07-01 | 2025-08-01 | Imi Systems Ltd | Long range artillery projectile with auxiliary energetic material for rear casing ejection |
| IL314183B2 (en) * | 2024-07-01 | 2025-12-01 | Imi Systems Ltd | Long range artillery projectile with auxiliary energetic material for rear casing ejection |
| WO2026009212A1 (en) * | 2024-07-01 | 2026-01-08 | Imi Systems Ltd. | Long range artillery projectile with auxiliary energetic material for rear casing ejection |
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