CN112945027A - Bullet core preparation method and composite bullet core - Google Patents
Bullet core preparation method and composite bullet core Download PDFInfo
- Publication number
- CN112945027A CN112945027A CN202110120121.XA CN202110120121A CN112945027A CN 112945027 A CN112945027 A CN 112945027A CN 202110120121 A CN202110120121 A CN 202110120121A CN 112945027 A CN112945027 A CN 112945027A
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- China
- Prior art keywords
- core
- entropy alloy
- bullet
- amorphous filler
- mold cavity
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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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- 239000002131 composite material Substances 0.000 title claims abstract description 19
- 238000002360 preparation method Methods 0.000 title claims abstract description 8
- 239000000945 filler Substances 0.000 claims abstract description 21
- 229910045601 alloy Inorganic materials 0.000 claims abstract description 20
- 239000000956 alloy Substances 0.000 claims abstract description 20
- 239000000463 material Substances 0.000 claims abstract description 20
- 239000000843 powder Substances 0.000 claims abstract description 16
- 239000008188 pellet Substances 0.000 claims abstract description 9
- 239000012634 fragment Substances 0.000 claims abstract description 6
- 238000000034 method Methods 0.000 claims description 12
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims description 8
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 claims description 6
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims description 5
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 claims description 5
- 229910052802 copper Inorganic materials 0.000 claims description 5
- 239000010949 copper Substances 0.000 claims description 5
- 229910052726 zirconium Inorganic materials 0.000 claims description 5
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 claims description 4
- 229910052804 chromium Inorganic materials 0.000 claims description 4
- 239000011651 chromium Substances 0.000 claims description 4
- 238000010438 heat treatment Methods 0.000 claims description 4
- 229910052742 iron Inorganic materials 0.000 claims description 4
- JFALSRSLKYAFGM-UHFFFAOYSA-N uranium(0) Chemical compound [U] JFALSRSLKYAFGM-UHFFFAOYSA-N 0.000 claims description 4
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 claims description 3
- 229910052782 aluminium Inorganic materials 0.000 claims description 3
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 3
- 229910017052 cobalt Inorganic materials 0.000 claims description 3
- 239000010941 cobalt Substances 0.000 claims description 3
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 claims description 3
- 238000001816 cooling Methods 0.000 claims description 3
- 229910052759 nickel Inorganic materials 0.000 claims description 3
- 239000010936 titanium Substances 0.000 claims description 3
- 229910052719 titanium Inorganic materials 0.000 claims description 3
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 claims description 2
- 229910052721 tungsten Inorganic materials 0.000 claims description 2
- 239000010937 tungsten Substances 0.000 claims description 2
- 238000004519 manufacturing process Methods 0.000 claims 6
- 229920001971 elastomer Polymers 0.000 claims 2
- 239000000806 elastomer Substances 0.000 claims 2
- 230000000149 penetrating effect Effects 0.000 abstract description 10
- 230000001066 destructive effect Effects 0.000 abstract description 3
- 238000000465 moulding Methods 0.000 abstract description 3
- 230000009286 beneficial effect Effects 0.000 description 2
- 229910000851 Alloy steel Inorganic materials 0.000 description 1
- 229910000711 U alloy Inorganic materials 0.000 description 1
- 239000011133 lead Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000035515 penetration Effects 0.000 description 1
- 238000006467 substitution reaction 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
- F42B33/00—Manufacture of ammunition; Dismantling of ammunition; Apparatus therefor
-
- 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
- F42B12/02—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
- F42B12/04—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of armour-piercing type
Abstract
The invention relates to the technical field of ammunition preparation, and particularly discloses an ammunition core preparation method and a composite ammunition core, wherein the ammunition core preparation method comprises the following steps: placing a plurality of high density pellets, chips or powder into a mold cavity; and adding amorphous filler or high-entropy alloy into the die cavity, so that the amorphous filler or the high-entropy alloy fills gaps among the shots, fragments or powder, and the high-density shots, fragments or powder contains at least one energetic element. When the armor piercing bullet impacts a target object, the energetic material generates sparks at the impact moment and releases a large amount of heat to melt the surface of the target object, and finally the penetrating effect is achieved. Furthermore, the amorphous filler is added into the die, so that the molding of the composite bullet core can be realized, the density of the armor-piercing bullet can be increased, and the destructive power and the penetrating power of the armor-piercing bullet are improved.
Description
Technical Field
The invention relates to the technical field of ammunition preparation, in particular to a bullet core preparation method and a composite bullet core.
Background
The armor-piercing projectile is a typical kinetic energy projectile, and penetrates through an armored projectile depending on the strength, weight and speed of the projectile, and the modern armor-piercing projectile has a sharp projectile head and a slender projectile body, is made of steel alloy, lean uranium alloy and the like, and has extremely high strength. In modern war, the stronger the penetrating ability of the armor-piercing projectile, the greater the threat to the enemy, and therefore, how to improve the penetrating ability of the armor-piercing projectile has been the research focus of researchers.
Disclosure of Invention
One object of the present invention is to provide a method for preparing an elastic core and a composite elastic core, which can effectively improve the penetrating performance of a armor-piercing projectile.
To achieve the above object, in a first aspect, there is provided a method for preparing an elastic core, comprising:
placing a plurality of pellets, chips or powder into a mold cavity;
and adding amorphous filler into the die cavity, so that the amorphous filler or the high-entropy alloy fills gaps among the shots, fragments or powder.
Optionally, before the placing the plurality of shots, pieces, or powder into the mold cavity, the method further includes:
providing a mold having a mold cavity, a pellet, chip or powder made of a high density material, and an amorphous filler or high entropy alloy made of an amorphous material.
Optionally, after the amorphous filler or the high-entropy alloy is added into the mold cavity, so that the amorphous filler or the high-entropy alloy fills gaps between the shots, fragments, or powders, the method further includes:
and vacuumizing the die cavity and heating.
Optionally, after the mold cavity is vacuumized and heated, the method further includes:
and cooling to solidify the amorphous filler or the high-entropy alloy to obtain the composite elastic core.
Optionally, the mold cavity is of a spherical configuration.
Optionally, the high-density material is tungsten and/or depleted uranium.
Optionally, the amorphous material is a material such as aluminum, cobalt, chromium, zirconium, iron, nickel, copper, titanium and the like and a high-entropy alloy composed of the material.
In a second aspect, a composite core is provided, which is made by the above method.
In a third aspect, a armor-piercing projectile is provided, comprising a shell and the composite core.
The invention has the beneficial effects that: when the armor piercing bullet impacts a target object, sparks are generated by the bullet at the impact moment, a large amount of heat is released, the surface of the target object is melted, and finally the penetrating effect is achieved. Furthermore, amorphous filler or high-entropy alloy is added into the die, so that the molding of the composite bullet core can be realized, the density of the armor-piercing bullet can be increased, and the destructive power and the penetrating power of the armor-piercing bullet are improved.
Drawings
In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings used in the description of the embodiments or the prior art 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 for those skilled in the art, other drawings can be obtained according to these drawings without inventive exercise.
Fig. 1 is a flow chart of a method for making a core according to an embodiment.
Detailed Description
In order to make the objects, features and advantages of the present invention more obvious and understandable, the technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present invention, and it is apparent that the embodiments described below 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 the description of the present invention, it is to be understood that when an element is referred to as being "connected" to another element, it can be directly connected to the other element or intervening elements may also be present. When a component is referred to as being "disposed on" another component, it can be directly on the other component or intervening components may also be present.
Furthermore, the terms "long", "short", "inner", "outer", and the like indicate orientations or positional relationships based on those shown in the drawings, and are only for convenience of describing the present invention, but do not indicate or imply that the referred devices or elements must have the specific orientations, be configured to operate in the specific orientations, and thus are not to be construed as limitations of the present invention.
The technical scheme of the invention is further explained by the specific implementation mode in combination with the attached drawings.
Example one
This example provides a composite core made by the core making method of example two, and the armor-piercing projectile made from the composite core has excellent penetration performance and can efficiently penetrate through an object.
Example two
The embodiment provides a method for preparing the core, which is used for preparing the composite core in the first embodiment and has the same functions and beneficial effects.
Referring to fig. 1, the method for preparing the bullet core comprises the following steps:
s10: providing a mold having a mold cavity, a pellet, chip or powder made of a high density material, and an amorphous filler or high entropy alloy made of an amorphous material;
s20: placing a plurality of pellets, chips or powder into a mold cavity;
s30: adding amorphous filler or high-entropy alloy into the die cavity, so that the amorphous filler fills gaps among the shots, fragments or powder;
s40: vacuumizing the die cavity and heating;
s50: and cooling to solidify the amorphous filler or the high-entropy alloy to obtain the composite elastic core.
When the armor piercing bullet impacts a target object, the energetic material generates sparks at the impact moment and releases a large amount of heat to melt the surface of the target object, and finally the penetrating effect is achieved.
Furthermore, amorphous filler or high-entropy alloy is added into the die, so that the molding of the composite bullet core can be realized, the density of the armor-piercing bullet can be increased, and the destructive power and the penetrating power of the armor-piercing bullet are improved.
Optionally, the die cavity is of a spherical structure, and the composite core is also of a spherical structure.
Specifically, the spherical structure can ensure that the composite bullet core uniformly heats in all directions during impact, and the uniformity of the penetrating power of all parts of the armor-piercing bullet is improved.
In this embodiment, the high-density material is an energetic material and/or depleted uranium, or the like.
Specifically, the energetic material and the depleted uranium have higher densities, and can release a large amount of heat when impact occurs, so that the armor piercing capability of the armor piercing bullet can be effectively improved.
Optionally, the amorphous material is an energetic material such as zirconium, copper, iron, chromium or lead, and further may be a high-entropy alloy composed of materials such as aluminum, cobalt, chromium, zirconium, iron, nickel, copper and titanium.
It is understood that zirconium and copper have better formability and are advantageous for producing spherical cores.
When an element or layer is referred to as being "on" … … "," engaged with "… …", "connected to" or "coupled to" another element or layer, it can be directly on, engaged with, connected to or coupled to the other element or layer, or intervening elements or layers may also be present. In contrast, when an element or layer is referred to as being "directly on … …," "directly engaged with … …," "directly connected to" or "directly coupled to" another element or layer, there may be no intervening elements or layers present. Other words used to describe the relationship of elements should be interpreted in a similar manner (e.g., "between … …" and "directly between … …", "adjacent" and "directly adjacent", etc.). As used herein, the term "and/or" includes any and all combinations of one or more of the associated listed items. Although the terms first, second, third, etc. may be used herein to describe various elements, components, regions, layers and/or sections, these elements, components, regions, layers and/or sections should not be limited by these terms. These terms may be only used to distinguish one element, component, region or section from another element, component, region or section. Unless clearly indicated by the context, use of terms such as the terms "first," "second," and other numerical values herein does not imply a sequence or order. Thus, a first element, component, region, layer or section discussed below could be termed a second element, component, region, layer or section without departing from the teachings of the example embodiments.
Spatially relative terms, such as "inner," "outer," "below," "under," "lower," "above," "upper," and the like, may be used herein for ease of description to describe a relationship between one element or feature and one or more other elements or features as illustrated in the figures. Spatially relative terms may be intended to encompass different orientations of the device in addition to the orientation depicted in the figures. For example, if the device in the figures is turned over, elements described as "below" or "beneath" other elements or features would then be oriented "above" the other elements or features. Thus, the example term "below … …" can encompass both an orientation of facing upward and downward. The device may be otherwise oriented, such as by rotation through 90 degrees or other orientations, and is explained with the spatially relative descriptors herein.
The above examples are only intended to illustrate the technical solution of the present invention, but not to limit it; although the present invention has been described in detail with reference to the foregoing embodiments, it will be understood by those of ordinary skill in the art that: the technical solutions described in the foregoing embodiments may still be modified, or some technical features may be equivalently replaced; and such modifications or substitutions do not depart from the spirit and scope of the corresponding technical solutions of the embodiments of the present invention.
Claims (8)
1. A method of making an elastic core, comprising:
placing a plurality of pellets, chips or powder into a mold cavity;
and adding amorphous filler or high-entropy alloy into the die cavity, so that the amorphous filler or the high-entropy alloy fills gaps among the shots, fragments or powder.
2. The method of making a core bullet as in claim 1 further comprising, prior to said placing a plurality of pellets, chips or powders into said mold cavity:
providing a mold having a mold cavity, a pellet, chip or powder made of a high density material, and an amorphous filler or high entropy alloy made of an amorphous material.
3. The method of making a core bullet as claimed in claim 2, wherein said adding an amorphous filler to said mold cavity, such that said amorphous filler or high entropy alloy fills the gaps between each of said pellets, chips or powders, further comprises:
and vacuumizing the die cavity and heating.
4. The method of making a core bullet as set forth in claim 3, further including, after said evacuating said mold cavity and heating said mold cavity:
and cooling to solidify the amorphous filler or the high-entropy alloy to obtain the composite elastic core.
5. The method of making a core bullet as in claim 2 wherein said cavities are spherically shaped.
6. Method for the preparation of a core bullet according to claim 2 wherein said high density material is tungsten and/or depleted uranium.
7. The method of claim 2 wherein said amorphous material is a high entropy alloy of aluminum, cobalt, chromium, zirconium, iron, nickel, copper, titanium, or the like.
8. A composite core for an elastomer, characterized in that it is produced by the method for producing an elastomer core according to any one of claims 1 to 7.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202110120121.XA CN112945027A (en) | 2021-01-28 | 2021-01-28 | Bullet core preparation method and composite bullet core |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202110120121.XA CN112945027A (en) | 2021-01-28 | 2021-01-28 | Bullet core preparation method and composite bullet core |
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| Publication Number | Publication Date |
|---|---|
| CN112945027A true CN112945027A (en) | 2021-06-11 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN202110120121.XA Pending CN112945027A (en) | 2021-01-28 | 2021-01-28 | Bullet core preparation method and composite bullet core |
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Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4981512A (en) * | 1990-07-27 | 1991-01-01 | The United States Of America As Represented By The Secretary Of The Army | Methods are producing composite materials of metal matrix containing tungsten grain |
| US6010580A (en) * | 1997-09-24 | 2000-01-04 | California Institute Of Technology | Composite penetrator |
| US20030029347A1 (en) * | 2001-06-04 | 2003-02-13 | Lloyd Richard M. | Kinetic energy rod warhead with optimal penetrators |
| US20050066850A1 (en) * | 2003-06-19 | 2005-03-31 | Leblanc Russell P. | Non-lead composition and method of manufacturing non-lead projectiles and projectile cores therewith |
| US20170080498A1 (en) * | 2010-11-10 | 2017-03-23 | True Velocity, Inc. | Method of making a projectile by metal injection molding |
| CN109022988A (en) * | 2018-09-21 | 2018-12-18 | 四川煜兴新型材料科技有限公司 | A kind of preparation method of tungsten base high-specific-gravity alloy material |
| CN109022989A (en) * | 2018-09-21 | 2018-12-18 | 成都理工大学 | A kind of preparation method of high-entropy alloy Binder Phase tungsten base high-specific-gravity alloy |
-
2021
- 2021-01-28 CN CN202110120121.XA patent/CN112945027A/en active Pending
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4981512A (en) * | 1990-07-27 | 1991-01-01 | The United States Of America As Represented By The Secretary Of The Army | Methods are producing composite materials of metal matrix containing tungsten grain |
| US6010580A (en) * | 1997-09-24 | 2000-01-04 | California Institute Of Technology | Composite penetrator |
| US20030029347A1 (en) * | 2001-06-04 | 2003-02-13 | Lloyd Richard M. | Kinetic energy rod warhead with optimal penetrators |
| US20050066850A1 (en) * | 2003-06-19 | 2005-03-31 | Leblanc Russell P. | Non-lead composition and method of manufacturing non-lead projectiles and projectile cores therewith |
| US20170080498A1 (en) * | 2010-11-10 | 2017-03-23 | True Velocity, Inc. | Method of making a projectile by metal injection molding |
| CN109022988A (en) * | 2018-09-21 | 2018-12-18 | 四川煜兴新型材料科技有限公司 | A kind of preparation method of tungsten base high-specific-gravity alloy material |
| CN109022989A (en) * | 2018-09-21 | 2018-12-18 | 成都理工大学 | A kind of preparation method of high-entropy alloy Binder Phase tungsten base high-specific-gravity alloy |
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| PB01 | Publication | ||
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| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20210611 |
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