CN105444622A - Burster block of composite structure and manufacturing method of burster block - Google Patents
Burster block of composite structure and manufacturing method of burster block Download PDFInfo
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- CN105444622A CN105444622A CN201510783938.XA CN201510783938A CN105444622A CN 105444622 A CN105444622 A CN 105444622A CN 201510783938 A CN201510783938 A CN 201510783938A CN 105444622 A CN105444622 A CN 105444622A
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Abstract
The invention relates to a burster block of a composite structure and a manufacturing method of the burster block. The burster block comprises a protection layer, a ceramic layer, an energy absorption layer and a supporting layer, wherein the protection layer, the ceramic layer, the energy absorption layer and the supporting layer are sequentially stacked from outside to inside and bonded together through bonding agents. The surface density of the whole block is 50-80 kg/m<2>. The supporting layer is a fiber metal composite material laminated plate which is formed by alternately applying at least three metal plates and at least two layers of fiber prepreg in a combined mode. According to the burster block of the composite structure, the fiber metal composite material laminated plate serves as the supporting layer, shock resistance and multi-hit resistance of the fiber metal composite material laminated plate are far superior to those of a pure fiber reinforced resin composite material laminated plate or a metal plate, good rigid supporting can be provided for the ceramic layer, the high hardness characteristic of ceramic is given into play, bullets are broken to the greatest extent, impact energy is dispersed, and the protection capacity is greatly improved. The burster block of the composite structure can be widely applied to the field of light bulletproof armors.
Description
Technical field
The present invention relates to a kind of bulletproof armour plate and manufacture method thereof, particularly relate to a kind of composite construction armour and manufacture method thereof.
Background technology
At present, the target of high performance ballistic plate armour to resist the larger velocity shock of bullet under areal density.Traditional Ceramic Composite armour is usually made panel with harder pottery, is made backboard with the good metal of toughness or fiber-resin composite, first by panel and backboard shaping separately, and then utilize adhesive panel and backboard to be bonded together.Traditional Ceramic Composite armour utilizes the high strength of ceramic panel, high rigidity is forced and to deform during projectile impact and cracked, then caught fragment by backboard.But also there is following problem in traditional ceramics bullet proof composite plating: 1. because pottery is fragile material, armour is when being subject to bullet high speed impact, ceramic wafer is as direct out surface, by very easily occur after bullet impact ceramic wafer cracked, come off, cause armour to lose efficacy, thus affect its anti-repeatedly striking capabilities; 2. armour is when being subject to bullet high speed impact, and the fabric energy-absorbing distortion in fiber-resin composite backboard, ftractures with the abutting edge of ceramic wafer, ceramic panel is lost and supports and cause ballistic performance to decline.If use metal as backboard, armour weight increases, and when being subject to projectile strike, deformability is more weak, and the support effect of counter plate is bad, affects the overall bulletproof ability of composite plate.
Such as, US Patent No. 3859892 discloses a kind of composite ceramics armour plate, and using pottery as panel, glass fiber reinforced plastics laminates makes backboard; This composite armor panel is when being subject to the high speed impact of bullet, because do not have the backboard of high strength as support, ceramic panel is difficult to keep shape complete and cannot continue as user and provide protection, affects the ballistic performance of composite armor panel.Chinese patent CN204007335U discloses the compound soft armor of a kind of superhigh intensity, pliable and tough, lightweight, comprise burster course and base plate, it is characterized in that being provided with corundum ceramic layer successively from top to bottom between burster course and base plate, high-density fiber layer and high tenacity ceramic layer, described high-density fiber layer is the inorganic fibers layer containing the air gap through high pressure shape, high tenacity ceramic layer is zirconia-based ceramics, and described base plate is metal hard armour material; Although the energy of bullet absorbs mainly through ceramic layer, due to the large (6.0g/cm of zirconia ceramics density
3), cause armour plate entirety to lay particular stress on, and under the high speed impact of bullet, metal level base plate is difficult to provide good support, thus affects the ballistic performance of composite armour.
Summary of the invention
For the problems referred to above, the object of this invention is to provide a kind of new composite construction armour and manufacture method thereof, the surface density of armour is 50-80kg/m
2, in lower surface density (i.e. weight per unit area) situation, there is higher ballistic performance, can anti-7.62mm armor-piercing incendiary and 12.7mm armor-piercing incendiary, effectively can improve the ballistic performance of composite armour and the maneuverability of mobile device.
For achieving the above object; the present invention takes following technical scheme: a kind of composite construction armour; it is characterized in that; this armour comprises the protective layer, ceramic layer, absorbing energy layer and the supporting layer that from outward appearance to inner essence stack gradually; between each layer by adhesive bond together, whole plate surface density is 50-80kg/m
2; Wherein, described supporting layer is alternately lay by least 3 pieces of metallic plates and at least 2 layers of fiber prepreg material the fibre metal composite laminated plate be composited.
Described protective layer is high-performance fiber woven fabric or without latitude cloth, wherein, described high-performance fiber is at least one in carbon fiber, aramid fiber, superhigh molecular weight polyethylene fibers; The surface density of described protective layer is 0.1-0.4kg/m
2, thickness is 0.2-1.0mm.
The material of described ceramic layer is aluminium oxide, carborundum or boron carbide; Described ceramic layer is a monolithic ceramic, or for column or polygonal potsherd is bonding forms; The thickness of described ceramic layer is 10-20mm.
Described absorbing energy layer is by the high-performance fiber woven fabric through infiltrating resin treatment or the laminate made without latitude cloth, wherein, described high-performance fiber is at least one in carbon fiber, aramid fiber, superhigh molecular weight polyethylene fibers, described resin is polyethylene, polypropylene, acrylate, phenolic resins or Pioloform, polyvinyl acetal, and described resin content accounts for described woven fabric or the 15-22% without latitude cloth laminate gross weight; The surface density of described absorbing energy layer is 2-8kg/m
2, thickness is 2-8mm.
Described binding agent is thermosetting or thermoplastic resin.
Described metallic plate is suppressed by least one in titanium alloy, magnesium alloy, aluminium alloy or magnesium lithium alloy and is formed; The thickness of metallic plate described in monolithic is 0.1-2.0mm.
Described fiber prepreg material is the high-performance fiber infiltrating process through resin, described high-performance fiber is at least one in carbon fiber, aramid fiber or superhigh molecular weight polyethylene fibers, described resin is the one in epoxy resin, phenolic resins or polyimides, and described resin content accounts for the 50-60% of described fiber prepreg material gross weight; Described in individual layer, the thickness of fiber prepreg material is 0.1-0.3mm.
A manufacture method for composite construction armour, comprises the following steps:
1) according to the design needs of composite construction armour, the protective layer, ceramic layer, absorbing energy layer and the supporting layer that need size and thickness is prepared respectively; Wherein, the preparation method of supporting layer, comprises the following steps:
The first step: according to supporting layer need select the type of metallic plate and fiber prepreg material material, size, thickness and quantity;
Second step: adopt blasting craft to carry out surface treatment to metallic plate;
3rd step: the metallic plate after surface treatment and fiber prepreg material are carried out laying according to the mode that metallic plate/fiber prepreg material multilayer replaces, metallic plate at least 3 pieces, at least 2 layers, fiber prepreg material, sprays setting agent sizing between layers, thus makes fibre metal composite laminated plate precast body;
4th step: be positioned on press by fibre metal composite laminated plate precast body obtained for the 3rd step, adopts the solidification of gradient increased temperature supercharge method, hot-formingly obtains fibre metal composite laminated plate, i.e. supporting layer;
2) by step 1) protective layer, ceramic layer, absorbing energy layer and the supporting layer laying successively prepared, between each layer with the adhesive bond of thermosetting or thermoplastic resin together, then through hot pressing, curing molding, thus obtain composite construction armour.
Adopt the concrete technology of gradient increased temperature supercharge method cured fiber metal composite layer plywood to be in described 4th step: first by fibre metal composite laminated plate precast body from room temperature to be heated to 80 DEG C lower than the speed of 5 DEG C/min, constant temperature 20 ~ 30min; Be warming up to 100 ~ 140 DEG C with identical heating rate again, insulation 2 ~ 3h, whole pressure process controls at 15 ~ 20MPa; Finally be cooled to room temperature to take out, thus obtain smooth fibre metal composite laminated plate.
The present invention is owing to taking above technical scheme, it has the following advantages: 1, composite construction armour of the present invention, adopt fiber prepreg material and metallic plate by the fibre metal composite laminated plate of certain process combining as supporting layer, fibre metal composite laminated plate had both had the feature that fiber-resin composite specific strength is high, specific modulus is large, also had the excellent fracture toughness of metallic plate and shock resistance simultaneously.For the fibre metal composite laminated plate of carbon fiber and magnesium lithium alloy compound, fibre metal composite laminated plate density is about 1.50g/cm
3, tensile strength>=1100MPa, stretch modulus>=78.0GPa, and titanium alloy metallic plate density is 4.43g/cm
3, tensile strength>=900MPa; Under identical faces density, the tensile strength of fibre metal composite laminated plate is about 4 times of titanium alloy metallic plate, can provide good rigid support for ceramic layer and absorbing energy layer, reduces the distortion of composite construction armour, improves protective capacities.Therefore, under identical faces density, fibre metal composite laminated plate has high specific stiffness, specific strength and higher fracture toughness as supporting layer, its shock resistance and anti-repeatedly blow performance are far away higher than simple fiber-resin composite laminate or metallic plate, good rigid support can be provided for ceramic layer, make pottery play its high rigidity characteristic, to greatest extent broken bullet, distributing shocks energy, thus greatly improve protective capacities.2, composite construction armour of the present invention, can be widely used in the armoring field of lightweight bulletproof, for vehicle etc. provides available protecting.
Accompanying drawing explanation
Fig. 1 is structural representation of the present invention;
Fig. 2 is the structural representation of supporting layer of the present invention.
Detailed description of the invention
Below in conjunction with drawings and Examples, the present invention is described in detail.
As shown in Figure 1 and Figure 2, composite construction armour provided by the invention, it comprises the protective layer 1, ceramic layer 2, absorbing energy layer 3 and the supporting layer 4 that from outward appearance to inner essence stack gradually, is bonded together between each layer by binding agent 5, and whole plate surface density is 50-80kg/m
2; Wherein, supporting layer 4 is alternately lay by least 3 pieces of metallic plates 6 and at least 2 layers of fiber prepreg material 7 the fibre metal composite laminated plate be composited.
In above-described embodiment, protective layer 1 is high-performance fiber woven fabric or without latitude cloth, wherein, high-performance fiber can be at least one in carbon fiber, aramid fiber, superhigh molecular weight polyethylene fibers; The surface density of protective layer 1 is 0.1-0.4kg/m
2, thickness is 0.2-1.0mm.
In above-described embodiment, the material of ceramic layer 2 can be aluminium oxide, carborundum or boron carbide, and ceramic layer 2 can be a monolithic ceramic, or for column or polygonal potsherd is bonding forms; The thickness of ceramic layer 2 is 10-20mm.
In above-described embodiment, absorbing energy layer 3 is by the high-performance fiber woven fabric through infiltrating resin treatment or the high-performance fiber woven fabric made without latitude cloth or without latitude cloth laminate, wherein, high-performance fiber can be at least one in carbon fiber, aramid fiber, superhigh molecular weight polyethylene fibers, resin can be polyethylene, polypropylene, acrylate, phenolic resins or Pioloform, polyvinyl acetal, and resin content accounts for woven fabric or the 15-22% without latitude cloth laminate gross weight; The surface density of absorbing energy layer 3 is 2-8kg/m
2, thickness is 2-8mm.
In above-described embodiment, binding agent 5 is thermosetting or thermoplastic resin, can be epoxy resin or polyurethane resin.
In above-described embodiment, metallic plate 6 is suppressed by least one in the alloy in lightweight such as titanium alloy, magnesium alloy, aluminium alloy or magnesium lithium alloy and is formed; The thickness of single piece of metal plate 6 is 0.1-2.0mm.
In above-described embodiment, fiber prepreg material 7 is the high-performance fiber infiltrating process through resin, high-performance fiber can be at least one in carbon fiber, aramid fiber or superhigh molecular weight polyethylene fibers, resin can be the one in epoxy resin, phenolic resins or polyimides, and resin content accounts for the 50-60% of fiber prepreg material gross weight; The thickness of single layer fibre prepreg 7 is 0.1-0.3mm.
The present invention is by composite protection layer 1 before ceramic layer 2, and after minimizing ceramic layer 2 is subject to the fragmentation of bullet high speed impact, fragment is scattered; By composite endergonic layer 3 after ceramic layer 2, utilize the distortion energy absorption characteristics of high-performance fiber excellence, the abrasion of buffering bullet penetrates the continuation penetration after pottery, improves armour to the absorbability of broken bullet dump energy; By composite supporting layer 4 after absorbing energy layer 3, utilize the high specific stiffness of supporting layer 4 fibre metal composite laminated plate, specific strength and higher fracture toughness, and pass through the interface debonding of laminate storeroom, absorb the shock wave energy of bullet, make composite construction armour take into account lightweight and high ballistic performance, battlefield survival and the mobility of personnel and vehicle etc. are greatly improved.
The manufacture method of composite construction armour of the present invention, comprises the following steps:
1) according to the design needs of composite construction armour, the protective layer 1, ceramic layer 2, absorbing energy layer 3 and the supporting layer 4 that need size and thickness is prepared respectively.
Wherein, the preparation method of the fibre metal composite laminated plate of supporting layer 4 comprises the following steps:
The first step: according to supporting layer 4 need select the type of metallic plate 6 and fiber prepreg material 7 material, size, thickness and quantity.
Second step: adopt blasting craft to carry out surface treatment to metallic plate 6.First metallic plate 6 is placed in the acetone soln water bath processing 20 ~ 30min of 50 ~ 60 DEG C, to make oil removal treatment; Then metallic plate 6 taking-up clear water is rinsed; Adopt Pneumatic abrasive blaster, use granularity to be 150 object bauxite fine sands, under the spray gun air pressure of 0.6 ~ 1MPa, evenly purge metallic plate 6 surface, duration 20 ~ 30s, until the sub-light shape of metallic plate 6 surface presentation.
3rd step: the metallic plate 6 after surface treatment and fiber prepreg material 7 are carried out laying according to the mode that metallic plate/fiber prepreg material multilayer replaces, metallic plate 6 at least 3 pieces, 7 at least 2 layers, fiber prepreg material, spray the sizing of a small amount of setting agent between layers, thus make fibre metal composite laminated plate precast body.
4th step: be positioned on press by fibre metal composite laminated plate precast body obtained for the 3rd step, adopts the solidification of gradient increased temperature supercharge method, hot-formingly obtains fibre metal composite laminated plate.Concrete technology is: first by fibre metal composite laminated plate precast body from room temperature to be heated to 80 DEG C lower than the speed of 5 DEG C/min, constant temperature 20 ~ 30min; Be warming up to 100 ~ 140 DEG C with identical heating rate again, insulation 2 ~ 3h, whole pressure process controls at 15 ~ 20MPa; Finally be cooled to room temperature to take out, thus obtain smooth fibre metal composite laminated plate, i.e. supporting layer 4.
2) by step 1) protective layer 1, ceramic layer 2, absorbing energy layer 3 and supporting layer 4 laying successively prepared; be bonded together with the binding agent 5 of thermosetting or thermoplastic resin between each layer; again through hot pressing, curing molding, thus obtain composite construction armour of the present invention.
Provide composite construction armour and the effect thereof of two kinds of concrete structures below, to further illustrate composite construction armour of the present invention.
Embodiment one:
A kind of composite construction armour, is of a size of the flat board of 300 × 300mm.Protective layer is aramid fiber laid fabric, and thickness is 0.2mm, and surface density is 2.88kg/m
2; Ceramic layer is the whole plate of boron carbide that 15mm is thick, and surface density is 37.65kg/m
2; Absorbing energy layer is aramid fiber laid fabric, and thickness is 5mm, and surface density is 7.2kg/m
2; Supporting layer be carbon fiber prepreg, magnesium alloy metal plate by the fibre metal composite laminated plate of process combining of the present invention, fibre metal composite laminated plate density is 1.64g/cm
3, surface density is 3.28kg/m
2, tensile strength>=810MPa, stretch modulus>=82.0GPa; Wherein, magnesium alloy metal plate is five pieces, and monolithic magnesium alloy metal plate thickness is 0.2mm, carbon fiber prepreg four layers, and individual layer carbon fiber prepreg thickness is 0.15mm.By epoxy resin bonding between protective layer, ceramic layer, absorbing energy layer, supporting layer four kinds of laminates, curing molding, form composite construction armour, whole plate thickness is 22mm, and quality is 4.59kg, and surface density is 51kg/m
2.This kind of composite construction armour, quality is light, and ballistic performance is good, effectively can prevent running through of other small bore cartridges such as formula 53 formula 7.62mm armor-piercing incendiary, 12.7mm armor-piercing incendiary, reduces back side shoot mark height and keeps ceramic wafer entirety not cracked.
Embodiment two:
A kind of composite construction armour, is of a size of the flat board of 300 × 300mm.Protective layer is carbon fiber-free weft fabric, and thickness is 0.2mm, and surface density is 3kg/m
2; Ceramic layer is the whole plate of aluminium oxide ceramics of thick 18mm, and surface density is 52.4kg/m
2; Absorbing energy layer be superhigh molecular weight polyethylene fibers without latitude cloth, thickness is 7mm, and surface density is 6.44kg/m
2; Supporting layer be carbon fiber prepreg, magnesium lithium alloy metallic plate by the fibre metal composite laminated plate of process combining of the present invention, fibre metal composite laminated plate density is 1.50g/cm
3, surface density is 6kg/m
2, tensile strength>=1100MPa, stretch modulus>=78.0GPa; Wherein, magnesium lithium alloy metallic plate is five pieces, and monolithic magnesium lithium alloy plate thickness is 0.2mm, carbon fiber prepreg four layers, and individual layer carbon fiber prepreg thickness is 0.15mm.By epoxy resin bonding between protective layer, ceramic layer, absorbing energy layer, supporting layer four kinds of laminates, curing molding, form composite construction armour, whole plate thickness is 27mm, and quality is 6.1kg, and surface density is 67kg/m
2.This kind of composite construction armour, quality is light, and ballistic performance is good, effectively can prevent running through of other small bore cartridges such as 53 formula 7.62mm armor-piercing incendiaries, 12.7mm armor-piercing incendiary, reduces back side shoot mark height and keeps ceramic wafer entirety not cracked.
The various embodiments described above are only for illustration of the present invention, and wherein the structure, connected mode etc. of each parts all can change to some extent, and every equivalents of carrying out on the basis of technical solution of the present invention and improvement, all should not get rid of outside protection scope of the present invention.
Claims (9)
1. a composite construction armour, is characterized in that, this armour comprises the protective layer, ceramic layer, absorbing energy layer and the supporting layer that from outward appearance to inner essence stack gradually, and, whole plate surface density is 50-80kg/m between each layer by adhesive bond together
2; Wherein, described supporting layer is alternately lay by least 3 pieces of metallic plates and at least 2 layers of fiber prepreg material the fibre metal composite laminated plate be composited.
2. a kind of composite construction armour as claimed in claim 1, is characterized in that, described protective layer is high-performance fiber woven fabric or without latitude cloth, wherein, described high-performance fiber is at least one in carbon fiber, aramid fiber, superhigh molecular weight polyethylene fibers; The surface density of described protective layer is 0.1-0.4kg/m
2, thickness is 0.2-1.0mm.
3. a kind of composite construction armour as claimed in claim 1 or 2, is characterized in that, the material of described ceramic layer is aluminium oxide, carborundum or boron carbide; Described ceramic layer is a monolithic ceramic, or for column or polygonal potsherd is bonding forms; The thickness of described ceramic layer is 10-20mm.
4. a kind of composite construction armour as claimed in claim 1 or 2, it is characterized in that, described absorbing energy layer is by the high-performance fiber woven fabric through infiltrating resin treatment or the laminate made without latitude cloth, wherein, described high-performance fiber is at least one in carbon fiber, aramid fiber, superhigh molecular weight polyethylene fibers, described resin is polyethylene, polypropylene, acrylate, phenolic resins or Pioloform, polyvinyl acetal, and described resin content accounts for described woven fabric or the 15-22% without latitude cloth laminate gross weight; The surface density of described absorbing energy layer is 2-8kg/m
2, thickness is 2-8mm.
5. a kind of composite construction armour as claimed in claim 1 or 2, is characterized in that, described binding agent is thermosetting or thermoplastic resin.
6. a kind of composite construction armour as claimed in claim 1 or 2, is characterized in that, described metallic plate is suppressed by least one in titanium alloy, magnesium alloy, aluminium alloy or magnesium lithium alloy and formed; The thickness of metallic plate described in monolithic is 0.1-2.0mm.
7. a kind of composite construction armour as claimed in claim 1 or 2, it is characterized in that, described fiber prepreg material is the high-performance fiber infiltrating process through resin, described high-performance fiber is at least one in carbon fiber, aramid fiber or superhigh molecular weight polyethylene fibers, described resin is the one in epoxy resin, phenolic resins or polyimides, and described resin content accounts for the 50-60% of described fiber prepreg material gross weight; Described in individual layer, the thickness of fiber prepreg material is 0.1-0.3mm.
8. a manufacture method for the composite construction armour according to any one of claim 1 to 7, comprises the following steps:
1) according to the design needs of composite construction armour, the protective layer, ceramic layer, absorbing energy layer and the supporting layer that need size and thickness is prepared respectively; Wherein, the preparation method of supporting layer, comprises the following steps:
The first step: according to supporting layer need select the type of metallic plate and fiber prepreg material material, size, thickness and quantity;
Second step: adopt blasting craft to carry out surface treatment to metallic plate;
3rd step: the metallic plate after surface treatment and fiber prepreg material are carried out laying according to the mode that metallic plate/fiber prepreg material multilayer replaces, metallic plate at least 3 pieces, at least 2 layers, fiber prepreg material, sprays setting agent sizing between layers, thus makes fibre metal composite laminated plate precast body;
4th step: be positioned on press by fibre metal composite laminated plate precast body obtained for the 3rd step, adopts the solidification of gradient increased temperature supercharge method, hot-formingly obtains fibre metal composite laminated plate, i.e. supporting layer;
2) by step 1) protective layer, ceramic layer, absorbing energy layer and the supporting layer laying successively prepared, between each layer with the adhesive bond of thermosetting or thermoplastic resin together, then through hot pressing, curing molding, thus obtain composite construction armour.
9. the manufacture method of a kind of composite construction armour as claimed in claim 8, it is characterized in that, adopt the concrete technology of gradient increased temperature supercharge method cured fiber metal composite layer plywood to be in described 4th step: first by fibre metal composite laminated plate precast body from room temperature to be heated to 80 DEG C lower than the speed of 5 DEG C/min, constant temperature 20 ~ 30min; Be warming up to 100 ~ 140 DEG C with identical heating rate again, insulation 2 ~ 3h, whole pressure process controls at 15 ~ 20MPa; Finally be cooled to room temperature to take out, thus obtain smooth fibre metal composite laminated plate.
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| CN106767171A (en) * | 2017-01-16 | 2017-05-31 | 江苏安卡新材料科技有限公司 | A kind of bulletproof composite sheet material and preparation method thereof |
| CN107255430A (en) * | 2017-08-02 | 2017-10-17 | 伍芳 | The armoring panel assembly of anti-rounds shooting |
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| CN109855473A (en) * | 2019-01-04 | 2019-06-07 | 西安交通大学 | A kind of bulletproof composite armour plate and preparation method thereof |
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| CN115468456A (en) * | 2022-08-31 | 2022-12-13 | 北京坤飞装备科技有限公司 | Composite bullet shielding layer for resisting multi-stage series penetration warhead powder charge damage |
Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2903895Y (en) * | 2006-04-10 | 2007-05-23 | 北京海淀天力新技术公司 | Light high strength bulletproof heart protection plate |
| CN105659795B (en) * | 2007-05-18 | 2011-02-16 | 北京玻钢院复合材料有限公司 | A kind of fit armour material of composite construction and forming method thereof |
| CN202770328U (en) * | 2012-01-11 | 2013-03-06 | 陈照峰 | A composite-structure bulletproof material board |
| CN103017609A (en) * | 2012-12-03 | 2013-04-03 | 中国人民解放军总后勤部军需装备研究所 | Composite bulletproof flashboard and preparation method and application thereof |
| CN103206897A (en) * | 2012-01-11 | 2013-07-17 | 陈照峰 | Bullet resistant material with composite structure and preparation method of bullet resistant material |
| CN203100561U (en) * | 2012-12-03 | 2013-07-31 | 中国人民解放军总后勤部军需装备研究所 | Composite bulletproof flashboard |
| CN103954175A (en) * | 2013-08-02 | 2014-07-30 | 太仓派欧技术咨询服务有限公司 | Energy-absorbing composite material bulletproof structure with air serving as deformation layer |
| CN203908411U (en) * | 2014-01-24 | 2014-10-29 | 常熟佳合高级陶瓷材料有限公司 | Novel composite bullet-proof ceramic inserting plate |
| CN205138327U (en) * | 2015-11-16 | 2016-04-06 | 中国人民解放军总后勤部军需装备研究所 | Composite construction armour |
-
2015
- 2015-11-16 CN CN201510783938.XA patent/CN105444622A/en active Pending
Patent Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2903895Y (en) * | 2006-04-10 | 2007-05-23 | 北京海淀天力新技术公司 | Light high strength bulletproof heart protection plate |
| CN105659795B (en) * | 2007-05-18 | 2011-02-16 | 北京玻钢院复合材料有限公司 | A kind of fit armour material of composite construction and forming method thereof |
| CN202770328U (en) * | 2012-01-11 | 2013-03-06 | 陈照峰 | A composite-structure bulletproof material board |
| CN103206897A (en) * | 2012-01-11 | 2013-07-17 | 陈照峰 | Bullet resistant material with composite structure and preparation method of bullet resistant material |
| CN103017609A (en) * | 2012-12-03 | 2013-04-03 | 中国人民解放军总后勤部军需装备研究所 | Composite bulletproof flashboard and preparation method and application thereof |
| CN203100561U (en) * | 2012-12-03 | 2013-07-31 | 中国人民解放军总后勤部军需装备研究所 | Composite bulletproof flashboard |
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