CN103727844A - Resilient bomb-resisting mixed composite material - Google Patents
Resilient bomb-resisting mixed composite material Download PDFInfo
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- CN103727844A CN103727844A CN201310332257.2A CN201310332257A CN103727844A CN 103727844 A CN103727844 A CN 103727844A CN 201310332257 A CN201310332257 A CN 201310332257A CN 103727844 A CN103727844 A CN 103727844A
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Abstract
The invention discloses a resilient bomb-resisting mixed composite material. The resilient bomb-resisting mixed composite material is characterized by structurally comprising five layers, namely, a surface layer, a collision layer, an energy absorption layer, a built-in resilient layer and a resistance layer. The surface layer is made of adamantine spar or silicon carbide or boron carbide elements. The collision layer is made of TC4 titanium alloy or a fibrous composite. The energy absorption layer is made of through-hole foam metallic aluminum or silicone rubber foam sheets. The built-in resilient layer is made of silicone rubber or natural rubber and permeates the bottom of the energy absorption layer. The resistance layer is made of the TC4 titanium alloy or the fibrous composite. The five layers are bonded through an adhesive agent, wherein the surface density ranges from 60Kg/m<2> to 90Kg/m<2>. The bomb-resisting material with the composite structure has the advantages of being low in volume weight, high in bomb resistance and capable of resisting multiple bombs, thereby being capable of being used as a protective material for resisting armor-piercing incendiaries with small and medium calibers being 7.62mm or above and being used as the deck of a naval ship and a shield.
Description
Technical field
Patent of the present invention relates to a kind of bullet resistant material, especially relates to a kind of anti-bullet hybrid composite with resilience function.
Background information
In modern war, bulletproof armour material is basis of indispensable existence, is one of key technology of military weapon.Take air force as example, along with the continuous enhancing of ground air defense strength, the military secret of attacking is over the ground faced with powerful ground firepower, so must equip advanced bulletproof armour material, to improve its anti-bullet survival ability.From the Li Sheng of armour material, develop, from traditional metal material (steel, aluminium), advanced ceramic material, composite (Polymers, Metal Substrate, ceramic base) till now, armour material is always towards light weight, efficient future development, the light weight of armor system, efficiently most important concerning improving military secret, tank and armored vehicle and combatant's mobility, attack, battlefield viability.Metal is the material of modern armoring main use, from ordinary steel plate armour, develops into glass hard steel plate armour, Dual Hardness Steel composite armour and even titanium alloy armor, and its protective capacities improves constantly.Metal bullet resistant material plays an important role for the protection of tank, warship, panzer etc. and protects for the nearly body of military secret and human body, because density is larger, therefore can affect tactical qualities performance.The bulletproof ceramic, bulletproof composite material occurring be subsequently with its lighter quality and the excellent ratio of performance to price, and in various fields, replaced metal armor gradually.
Multiple layer combination protection is as the application of existing nearly decades of energy-absorbing decompressor, both at home and abroad the performance of multilayer proofing result is is also analyzed and researched from different perspectives, as Guruprasad etc., everybody has proposed a kind of novel energy absorption device, under Explosion Loading, its performance has been carried out analyzing and has discussed; The people such as Holmquist, carrying out in the research of material constitutive model, analyze the problem of bullet penetration multilayer dielectricity, the impact of the damage and failure of mainly having considered multilayer dielectricity target on penetration; The fade performance in multilayer dielectricity characterizes by means of numerical simulation shock wave for Gupta and Ding, has proposed exploratory decision method.Because the propagation problem of stress wave in multilayer dielectricity exists the coupling of load and medium, and the difficult point, the particularly dynamic response under impact loading for foamed material such as the more complicated boundary value condition of multiple layer combination medium self.
Application number is that 201010147708.1 patent discloses a kind of flame-retardant high-resilience foam material, it is characterized in that mixing by PPG, crosslinking agent, varies catalyst and modification MDI the polyurethane foamed material forming.Although it has resilience equally, but cannot better resist the impact of bullet.And select the anti-bullet hybrid materials of resilience, and by absorbing energy layer and the combination of built-in bounce-back layer, and reinforced bonding between layers, more can give full play to the excellent properties of material.
Application number is that 99101874.5 patent discloses a kind of good low-repulsion that has, as the low resilience urethane foam that rushes technical ability absorbing material, acoustic material and packing.But this material is more single, cannot meet the requirement for ballistic performance in military project.
Summary of the invention
For addressing the above problem, the present invention discloses the anti-bullet hybrid composite of a kind of resilience, it is characterized in that being comprised of five-layer structure, is respectively superficial layer, collision layer, absorbing energy layer, built-in bounce-back layer, resistant layer.Surface density is 60~90Kg/m2, can tackle the middle-size and small-size bore armor-piercing incendiaries such as 7.62mm, 12.7mm, 14.5mm, or with the similar shrapnel of its kinetic energy, or other middle-size and small-size bore bullets.Composite construction bullet resistant material of the present invention, each layer by binding agent strong bond, superficial layer 10 is comprised of corundum or carborundum or boron carbide element, ceramic component can be graininess, also can be tabular, that particle comprises be spherical, the cylindricality that both ends of the surface are parallel, the cylindricality that both ends of the surface are heaved, hollow cylindricality, the corundum ceramic post of preferentially selecting both ends of the surface to heave, the diameter of ceramics pole is 10~20mm; Collision layer 20 is comprised of TC4 titanium alloy or fibrous composite, for small-bore armor-piercing incendiary, preferentially selects carbon fibre composite or Kafra fiber composite, for medium caliber armor-piercing incendiary, preferentially selects TC4 titanium alloy; Absorbing energy layer 30 is comprised of through-hole foamed metal aluminium or silicon rubber foam plate, preferentially selects through-hole foamed metal aluminium; Built-in bounce-back layer 40 is comprised of silicon rubber or natural rubber, infiltrates absorbing energy layer through-hole foam base section, preferentially selects silicon rubber; Resistant layer 50 is comprised of TC4 titanium alloy or fibrous composite, for small-bore armor-piercing incendiary or surface density, require lower composite construction bullet resistant material, preferentially select carbon fiber or Kafra fiber composite, for medium caliber armor-piercing incendiary, preferentially select TC4 titanium alloy.The thickness of each layer is along with the bore of armor-piercing incendiary is different and each variant, superficial layer 10 thickness are 10~20mm, and collision layer 20 thickness are 2~5mm, and absorbing energy layer 30 thickness are 10~30mm, built-in bounce-back layer 40 thickness are 5~20mm, and resistant layer 50 thickness are 1~4mm.
Foamed aluminium has excellent physical property, chemical property and mechanical property and recuperability.It has high-damping shock stability and impact energy absorb rate, and the 5-10 that damping capacity is metallic aluminium doubly, when 50% modification occurs the foamed aluminium that porosity is 84%, can absorb energy more than 2.5MJ/M3C.And material large rubber-like viscoplasticity is injected into after foamed aluminium, the effect of its energy-absorbing bounce-back is more remarkable.
The invention has the advantages that: (1) high-strength light, can resist the impact of large load; (2) porous foam structure plate has the performances such as energy absorption, lightweight, shock-resistant, recuperability; (3) each material property supplements mutually, has avoided the shortcoming such as fragility of homogenous material, thereby has jointly brought into play its effect.
Accompanying drawing explanation
Fig. 1 resilience Ballistic Composites schematic diagram
In figure, 10 is superficial layer, and 20 is collision layer, and 30 is absorbing energy layer, and 40 is built-in bounce-back layer, and 50 is resistant layer.
The specific embodiment
Below in conjunction with specific embodiment, further illustrate the present invention, should understand these embodiment is only not used in and limits the scope of the invention for the present invention is described, after having read the present invention, those skilled in the art all fall within the application's claims to the modification of the various equivalent form of values of the present invention and limit.
Embodiment 1
The corundum ceramic post that superficial layer 10 is high 16mm, two ends are hemisphere face, surface density is 4.66g/cm
2; Collision layer 20 is for being the thick TC4 plate of 2mm, and surface density is 0.89g/cm
2; Absorbing energy layer 30 is the foam metal aluminium that 20mm is thick, and surface density is 0.62g/cm
2; Built-in bounce-back layer 40 is the silicon rubber that 10mm is thick, and surface density is 1.0g/cm
2; Resistant layer 50 is the thick TC4 titanium alloy sheet of 2mm, and surface density is 0.89g/cm
2.Compound rear whole plate surface density is 8.0~8.3g/cm
2, that is 80~83Kg/m
2, whole plate thickness is 47~49mm, and whole plate is that square is dull and stereotyped, and length and width are 150mm.
Embodiment 2
The corundum ceramic post that superficial layer 10 is high 16mm, two ends are hemisphere face, surface density is 4.66g/cm
2; Collision layer 20 is for to draw composite panel for the thick Kev of 3mm, and surface density is 0.3g/cm
2; Absorbing energy layer 30 is the silicon rubber foam plate that 20mm is thick, and surface density is 1.07g/cm
2; Built-in bounce-back layer 40 is the silicon rubber that 10mm is thick, and surface density is 1.0g/cm
2; Resistant layer 50 is drawn composite panel for the thick Kev of 2mm, and surface density is 0.2g/cm
2.Compound rear whole plate surface density is 7.2~7.4g/cm
2, that is 72~74Kg/m
2, whole plate thickness is 48~50mm, and whole plate is that square is dull and stereotyped, and length and width are 150mm.
Above are only several specific embodiment of the present invention, but design concept of the present invention is not limited to this, allly utilizes this design to carry out the change of unsubstantiality to the present invention, all should belong to the behavior of invading the scope of protection of the invention.
Claims (4)
1. the anti-bullet hybrid composite of resilience, is characterized in that being comprised of five-layer structure, is respectively superficial layer, collision layer, absorbing energy layer, built-in bounce-back layer, resistant layer, bonding by binding agent between each layer.
2. according to described in claim 1, it is characterized in that absorbing energy layer is comprised of through-hole foamed metal aluminium or silicon rubber foam plate, porous foam thickness is 10-30mm, and its mesopore is through hole, and porosity is 63%-90%.
3. according to described in claim 1, it is characterized in that built-in bounce-back layer is comprised of silicon rubber or natural rubber, thickness is 5-20mm.
4. according to described in claim 3, it is characterized in that silicon rubber or natural rubber to infiltrate the base section of through-hole foam claimed in claim 2.
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Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN104142096A (en) * | 2014-07-17 | 2014-11-12 | 辽宁融达新材料科技有限公司 | Anti-violence protecting panel and container manufactured by using the same |
CN109357572A (en) * | 2018-10-31 | 2019-02-19 | 首钢集团有限公司 | Fire-retardant composite armour module |
CN109690283A (en) * | 2016-09-15 | 2019-04-26 | 霍尼韦尔国际公司 | The kinetic energy of low back face deformation ballistic composite absorbs |
CN114802779A (en) * | 2022-06-23 | 2022-07-29 | 中国飞机强度研究所 | Aircraft fuel tank with penetration and damage resisting protection effect and design method thereof |
CN117261372A (en) * | 2023-09-01 | 2023-12-22 | 中国海洋大学 | High-ballistic performance biological inspired sandwich panel and preparation method thereof |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN101334993A (en) * | 2008-08-04 | 2008-12-31 | 中国科学院力学研究所 | Noise absorbing compound material based on network construction and preparing method thereof |
CN101650148A (en) * | 2009-09-14 | 2010-02-17 | 哈尔滨飞机工业集团有限责任公司 | Ceramic/composite material interlayer protecting structure |
CN202770328U (en) * | 2012-01-11 | 2013-03-06 | 陈照峰 | A composite-structure bulletproof material board |
-
2013
- 2013-08-02 CN CN201310332257.2A patent/CN103727844A/en active Pending
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN101334993A (en) * | 2008-08-04 | 2008-12-31 | 中国科学院力学研究所 | Noise absorbing compound material based on network construction and preparing method thereof |
CN101650148A (en) * | 2009-09-14 | 2010-02-17 | 哈尔滨飞机工业集团有限责任公司 | Ceramic/composite material interlayer protecting structure |
CN202770328U (en) * | 2012-01-11 | 2013-03-06 | 陈照峰 | A composite-structure bulletproof material board |
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN104142096A (en) * | 2014-07-17 | 2014-11-12 | 辽宁融达新材料科技有限公司 | Anti-violence protecting panel and container manufactured by using the same |
CN109690283A (en) * | 2016-09-15 | 2019-04-26 | 霍尼韦尔国际公司 | The kinetic energy of low back face deformation ballistic composite absorbs |
CN109690283B (en) * | 2016-09-15 | 2022-07-12 | 霍尼韦尔国际公司 | Viscoelastic lightweight composite armor that resists backside deformation |
CN109357572A (en) * | 2018-10-31 | 2019-02-19 | 首钢集团有限公司 | Fire-retardant composite armour module |
CN109357572B (en) * | 2018-10-31 | 2020-08-25 | 首钢集团有限公司 | Flame retardant composite armor module |
CN114802779A (en) * | 2022-06-23 | 2022-07-29 | 中国飞机强度研究所 | Aircraft fuel tank with penetration and damage resisting protection effect and design method thereof |
CN114802779B (en) * | 2022-06-23 | 2022-09-16 | 中国飞机强度研究所 | Aircraft fuel tank with penetration and damage resisting protection effect and design method thereof |
CN117261372A (en) * | 2023-09-01 | 2023-12-22 | 中国海洋大学 | High-ballistic performance biological inspired sandwich panel and preparation method thereof |
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Application publication date: 20140416 |