WO2016108621A1 - 방탄패널 - Google Patents
방탄패널 Download PDFInfo
- Publication number
- WO2016108621A1 WO2016108621A1 PCT/KR2015/014487 KR2015014487W WO2016108621A1 WO 2016108621 A1 WO2016108621 A1 WO 2016108621A1 KR 2015014487 W KR2015014487 W KR 2015014487W WO 2016108621 A1 WO2016108621 A1 WO 2016108621A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- impregnated
- fabric
- aramid
- phenol resin
- ceramic plate
- Prior art date
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Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41H—ARMOUR; ARMOURED TURRETS; ARMOURED OR ARMED VEHICLES; MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL
- F41H1/00—Personal protection gear
- F41H1/02—Armoured or projectile- or missile-resistant garments; Composite protection fabrics
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B18/00—Layered products essentially comprising ceramics, e.g. refractory products
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B27/00—Layered products comprising a layer of synthetic resin
- B32B27/38—Layered products comprising a layer of synthetic resin comprising epoxy resins
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B27/00—Layered products comprising a layer of synthetic resin
- B32B27/42—Layered products comprising a layer of synthetic resin comprising condensation resins of aldehydes, e.g. with phenols, ureas or melamines
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B7/00—Layered products characterised by the relation between layers; Layered products characterised by the relative orientation of features between layers, or by the relative values of a measurable parameter between layers, i.e. products comprising layers having different physical, chemical or physicochemical properties; Layered products characterised by the interconnection of layers
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41H—ARMOUR; ARMOURED TURRETS; ARMOURED OR ARMED VEHICLES; MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL
- F41H5/00—Armour; Armour plates
- F41H5/02—Plate construction
- F41H5/04—Plate construction composed of more than one layer
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41H—ARMOUR; ARMOURED TURRETS; ARMOURED OR ARMED VEHICLES; MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL
- F41H5/00—Armour; Armour plates
- F41H5/02—Plate construction
- F41H5/04—Plate construction composed of more than one layer
- F41H5/0414—Layered armour containing ceramic material
- F41H5/0428—Ceramic layers in combination with additional layers made of fibres, fabrics or plastics
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
- B32B2262/02—Synthetic macromolecular fibres
- B32B2262/0261—Polyamide fibres
- B32B2262/0269—Aromatic polyamide fibres
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2307/00—Properties of the layers or laminate
- B32B2307/50—Properties of the layers or laminate having particular mechanical properties
- B32B2307/558—Impact strength, toughness
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2363/00—Epoxy resins
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2377/00—Polyamides
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2571/00—Protective equipment
- B32B2571/02—Protective equipment defensive, e.g. armour plates, anti-ballistic clothing
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- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2237/00—Aspects relating to ceramic laminates or to joining of ceramic articles with other articles by heating
- C04B2237/30—Composition of layers of ceramic laminates or of ceramic or metallic articles to be joined by heating, e.g. Si substrates
- C04B2237/32—Ceramic
- C04B2237/34—Oxidic
- C04B2237/343—Alumina or aluminates
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- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2237/00—Aspects relating to ceramic laminates or to joining of ceramic articles with other articles by heating
- C04B2237/30—Composition of layers of ceramic laminates or of ceramic or metallic articles to be joined by heating, e.g. Si substrates
- C04B2237/32—Ceramic
- C04B2237/36—Non-oxidic
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2237/00—Aspects relating to ceramic laminates or to joining of ceramic articles with other articles by heating
- C04B2237/30—Composition of layers of ceramic laminates or of ceramic or metallic articles to be joined by heating, e.g. Si substrates
- C04B2237/32—Ceramic
- C04B2237/36—Non-oxidic
- C04B2237/365—Silicon carbide
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- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2237/00—Aspects relating to ceramic laminates or to joining of ceramic articles with other articles by heating
- C04B2237/30—Composition of layers of ceramic laminates or of ceramic or metallic articles to be joined by heating, e.g. Si substrates
- C04B2237/32—Ceramic
- C04B2237/36—Non-oxidic
- C04B2237/368—Silicon nitride
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S428/00—Stock material or miscellaneous articles
- Y10S428/911—Penetration resistant layer
Definitions
- the present invention relates to a bulletproof panel, and more specifically, a laminate of a ceramic plate and a phenol resin-impregnated aramid fabric constituting the bulletproof panel is firmly adhered by an epoxy resin-impregnated fabric so that peeling thereof does not occur in a high temperature environment.
- the present invention relates to a bulletproof panel with greatly improved performance and workability.
- Bulletproof products are products for protecting the human body from bullets and shells, and the bulletproof performance of bulletproof products depends greatly on the materials used.
- high density polyethylene has a specific gravity of 0.98 lower than that of water, and thus is widely used as a bulletproof material.
- high-density polyethylene has a limitation in obtaining excellent ballistic performance, because deformation may occur greatly when subjected to physical shock during use, and has a weak property in heat.
- the wholly aromatic polyamide fibers include para-aramid fibers and meta-aramid fibers having a structure in which the benzene rings are linearly connected through an amide group (-CONH). do.
- Para-aramid fibers have excellent properties such as high strength, high elasticity, and low shrinkage, and are 5mm thick thin yarns, and have a strong strength enough to lift two tons of cars.
- Bulletproof composites are usually prepared by using aramid fibers to produce aramid fabrics and immersed in the resin and dried to produce aramid fabric prepreg and aramid fabric prepreg laminated in several layers and then cured Complete
- a bulletproof panel including a ceramic plate (hereinafter referred to as "ceramic bulletproof panel") has been manufactured by laminating a plurality of high strength fabrics such as aramid fabric and the like on a ceramic plate.
- the bulletproof mechanism of the ceramic bulletproof panel is currently not fully understood, but when fragments of bullets or projectiles collide with the initial ceramic plate, the ceramic plate is broken into pieces and most of the kinetic energy is distributed to these pieces of ceramic fragments. It is known that the pointed tip is deformed into a mushroom shape, or divided into several pieces, and it does not pass while consuming the remaining energy in the laminated bulletproof fiber while progressing in the state of increasing the contact surface.
- Korean Patent No. 10-0926746 discloses a thermoplastic adhesive film (D) and aramid fabric such as ethylene-vinylacetate copolymer film on one surface of a ceramic plate (A) as shown in FIG. 2.
- a ceramic bulletproof panel having a structure in which a bulletproof fabric F such as the above is laminated repeatedly several times in sequence.
- FIG. 2 is a schematic cross-sectional view of a conventional ceramic bulletproof panel.
- thermoplastic adhesive film (D) serves to bond the ceramic plate (A) and the bulletproof fabric (F) or the bulletproof fabric (F) and the bulletproof fabric (F).
- the ceramic plate (A) and the bulletproof fabric (F) or the bulletproof fabric (F) and the bulletproof fabric (F) bonded by the thermoplastic adhesive film (D) have weak adhesive strengths of 100 ° C. or more. The phenomenon of peeling in a high temperature environment occurs severely, there was a problem that the ballistic performance is reduced.
- thermoplastic adhesive film (D) has to be inserted after cutting each of the bulletproof fabrics (F), there is also a problem in that workability is greatly reduced.
- An object of the present invention is to provide a bulletproof panel having excellent bulletproof performance without peeling off a laminate (C) of a ceramic plate (A) and a phenol resin-impregnated aramid fabric constituting the bulletproof panel even under a high temperature environment.
- Another object of the present invention is to provide a bulletproof panel that can significantly improve the workability in the manufacturing process can be omitted by inserting the conventional thermoplastic adhesive film between the bulletproof fabric.
- a plurality of phenol resin-impregnated aramid fabrics (C1, C2, C3) are laminated to prepare a laminate (C) of the phenol resin-impregnated aramid fabrics.
- An epoxy resin impregnated fabric (B) is inserted between the laminate (C) of the phenol resin-impregnated aramid fabric and the ceramic plate (A) to firmly adhere them to produce a bulletproof panel.
- the phenol resin impregnated aramid fabric (C1, C2, C3) refers to an aramid fabric impregnated with one resin selected from phenol resin and phenol / polyvinyl butyral mixed resin.
- the epoxy resin-impregnated fabric (B) is located between the ceramic plate (A) and the laminate (C) of the phenol resin-impregnated aramid fabric and improves the adhesive force therebetween, the ceramic plate (A) and the phenol under high temperature environment.
- the laminated body (C) of the resin-impregnated aramid fabric is not peeled off, and the antiballistic performance is greatly improved.
- the present invention does not need to insert a thermoplastic adhesive film between the phenolic resin-impregnated aramid fabric (C1, C2, C3) as in the prior art, greatly improves workability.
- FIG. 1 is a cross-sectional view of an example of a bulletproof panel according to the present invention.
- FIG. 2 is a cross-sectional view of a conventional bulletproof panel.
- Bulletproof panel according to the invention is shown in Figure 1 (i) a ceramic plate (A); (ii) a laminate (C) of at least one phenolic resin impregnated aramid fabric on which phenolic resin impregnated aramid fabrics (C1, C2, C3) are laminated; And (iii) an epoxy resin impregnated fabric (B) located between the ceramic plate (A) and the laminate (C) of the phenol resin impregnated aramid fabric, in which an epoxy resin is impregnated into the fabric.
- FIG. 1 is a schematic cross-sectional view of the present invention.
- the phenol resin impregnated aramid fabric (C1, C2, C3) refers to an aramid fabric impregnated with one resin selected from phenol resin and phenol / polyvinyl butyral mixed resin.
- the phenol resin impregnated aramid fabric (C1, C2, C3) may be an aramid fabric impregnated with a phenol resin, or may be an aramid fabric impregnated with a phenol / polyvinyl butyral mixed resin.
- the phenol resin-impregnated aramid fabric (C1, C2, C3) is an aramid fabric impregnated with phenol / polyvinyl butyral mixed resin
- the mixing ratio of phenol resin: polyvinyl butyral resin is 50 to 65% by weight: 50 to It is 35 weight%
- the molecular weight of the said phenol resin is 300-3,000
- the molecular weight of the said polyvinyl butyral resin is 30,000-120,000, More preferably, it is 80,000-120,000, It is good for workability improvement and antiballistic performance improvement.
- an aramid fabric impregnated with a phenol / polyvinyl butyral mixed resin as the phenol resin-impregnated aramid fabric (C1, C2, C2). Do. The reason is that the polyvinyl butyral resin is relatively hard to be broken by the impact rather than the phenol resin.
- a high-strength fabric such as aramid fabric, carbon fiber fabric, glass fiber fabric, or the like may be used.
- the laminate (C) of the epoxy resin impregnated fabric (B) and the phenolic resin impregnated aramid fabric may be stacked on only one side of the ceramic plate (A) as shown in FIG. 1, or may be stacked on both sides of the ceramic plate. It may be.
- a bulletproof panel of the present invention in which a laminate (C) of the epoxy resin impregnated fabric (B) and the phenol resin impregnated aramid fabric is laminated on only one surface of the ceramic plate (A) to manufacture bulletproof articles such as bulletproof clothing
- the ceramic plate (A) part is positioned at the front of the bulletproof article and the laminates of epoxy resin impregnated fabric (B) and phenolic resin impregnated aramid fabric (C) are located at the rear of the bulletproof article.
- the fragments of the ceramic plate A broken by the impact are prevented from being crushed, and at the same time, the rear deformation of the bulletproof product is minimized during the impact.
- the bulletproof panel of the present invention in which the laminates (C) of the epoxy resin impregnated fabric (B) and the phenolic resin impregnated aramid fabric are laminated on both sides of the ceramic plate (A), the bullet is directly directed to the ceramic plate (A). It prevents the collision and effectively prevents the fragments of the broken ceramic plate (A) from being impacted upon impact, while minimizing the rear deformation during the impact.
- the ceramic plate comprises any one or more of alumina, silicon carbide, silicon nitride, boron carbide, tungsten carbide or tungsten boride, and produced by the method of high temperature sintering, high temperature high pressure sintering, gel casting or reaction sintering. do.
- phenol resin-impregnated aramid fabric prepreg is prepared by impregnating aramid fabric with phenol resin or phenol / polyvinyl butyral mixed resin.
- the epoxy resin is impregnated into the fabric to prepare an epoxy resin impregnated fabric prepreg.
- a bulletproof panel is manufactured by pressure molding for 20 to 200 minutes at a pressure of 100 ⁇ 200 bar and a temperature of 120 ⁇ 200 °C.
- the epoxy resin impregnated fabric prepreg laminated in the mold for bulletproof panel manufacturing is cured after pressure molding to become an epoxy resin impregnated fabric (B), and a laminate (C) of ceramic plate (A) and phenolic resin impregnated fabric. Tighten between them firmly.
- the epoxy resin-impregnated fabric (B) is located between the ceramic plate (A) and the laminate (C) of the phenol resin-impregnated aramid fabric and improves the adhesive force therebetween, the ceramic plate (A) and the phenol under high temperature environment.
- the laminated body (C) of the resin-impregnated aramid fabric is not peeled off, and the antiballistic performance is greatly improved.
- the present invention does not need to insert a thermoplastic adhesive film between the phenolic resin-impregnated aramid fabric (C1, C2, C3) as in the prior art, greatly improves workability.
- the phenol resin-impregnated aramid fabric prepregs were prepared by impregnating 20% by weight of a phenol solution in which a phenol resin having a molecular weight of 3,000 was dissolved in a methanol solvent in an aramid fabric having a density of 450 g / m 2 and a fineness of 3,000 deniers of warp and weft.
- an epoxy resin impregnated fabric prepreg was prepared by impregnating 40 wt% of an epoxy resin solution into a polyester fabric having a density of 200 g / m 2.
- the ceramic plate A of width 250mm, length 300mm, and thickness 6mm was prepared.
- a bulletproof panel was manufactured by press molding at a pressure of 180 bar and a temperature of 180 ° C. for 100 minutes.
- the phenol resin-impregnated aramid fabric prepregs were prepared by impregnating 20% by weight of a phenol solution in which a phenol resin having a molecular weight of 3,000 was dissolved in a methanol solvent in an aramid fabric having a density of 450 g / m 2 and a fineness of 3,000 deniers of warp and weft.
- an epoxy resin impregnated fabric prepreg was prepared by impregnating 40 wt% of an epoxy resin solution into a polyester fabric having a density of 200 g / m 2.
- the ceramic plate A of width 250mm, length 300mm, and thickness 6mm was prepared.
- a bulletproof panel was manufactured by press molding at a pressure of 180 bar and a temperature of 180 ° C. for 100 minutes.
- Phenol / Poly was dissolved in methanol solvent in a weight ratio of 60:40 by weight ratio of phenol resin having a molecular weight of 3,000 and polyvinyl butyral resin having a molecular weight of 9,000 in aramid fabric having a density of 450 g / m 2 and a fineness of 3,000 deniers of warp and weft.
- Phenolic resin impregnated aramid fabric prepregs were prepared by impregnating 20% by weight of vinylbutyral solution.
- an epoxy resin impregnated fabric prepreg was prepared by impregnating 40 wt% of an epoxy resin solution into a polyester fabric having a density of 200 g / m 2.
- the ceramic plate A of width 250mm, length 300mm, and thickness 6mm was prepared.
- a bulletproof panel was manufactured by press molding at a pressure of 180 bar and a temperature of 180 ° C. for 100 minutes.
- an aramid fabric (F) having a density of 450 g / m 2 and a fineness of warp and weft of 3,000 deniers and an adhesive film (D) composed of an ethylene-vinylacetate copolymer were repeatedly laminated 10 times in succession.
- an aramid fabric (F) having a density of 450 g / m 2 and a fineness of warp and weft of 3,000 deniers and an adhesive film (D) composed of an ethylene-vinylacetate copolymer were repeatedly stacked seven times in succession.
- an aramid fabric (F) having a density of 450 g / m 2 and a fineness of warp and weft of 3,000 deniers was laminated five times in turn, and then an adhesive film (D) consisting of an ethylene-vinylacetate copolymer was laminated.
- One sheet of ceramic plate (250 mm long, 300 mm long, 6 mm thick) was laminated thereon, and then a bulletproof panel was manufactured by press molding at a pressure of 180 bar and a temperature of 180 ° C. for 100 minutes.
- the average speed (in m / s) indirectly indicating the degree of ballistic resistance of a composite fabric was obtained when it completely penetrated with Cal. 22 caliber fragments (FSP) in accordance with MIL-STD-662F.
- the speed of time was measured from the averaged value.
- the back strain measured the maximum diameter (mm) of the projected part of the composite fabric backside by impact at a speed of 426 ⁇ 15 m / s using a 9 mm FMJ according to the NIJ LEVEL IIIA specification.
- the present invention is useful as a bulletproof material for producing a body armor, a bulletproof helmet, and the like.
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Ceramic Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Laminated Bodies (AREA)
Abstract
Description
구분 | 평균속도(V0)[m/s] | 후면변형[㎜] |
실시예 1 | 881 | 32 |
실시예 2 | 875 | 34 |
실시예 3 | 890 | 32 |
비교실시예 1 | 837 | 39 |
비교실시예 2 | 832 | 41 |
비교실시예 3 | 846 | 43 |
Claims (5)
- (i) 세라믹 플레이트(A); (ii) 페놀수지 함침 아라미드 직물(C1, C2, C3)들이 적층되어 있는 적어도 하나의 페놀수지 함침 아라미드 직물의 적층체(C); 및 (iii) 상기 세라믹 플레이트(A)와 페놀수지 함침 아라미드 직물의 적층체(C) 사이에 위치하며 직물에 에폭시 수지가 함침되어 있는 에폭시 수지 함침 직물(B);을 포함하는 것을 특징으로 하는 방탄패널.
- 제1항에 있어서, 상기 페놀수지 함침 아라미드 직물(C1, C2, C3)은 페놀수지 및 페놀/폴리비닐부티랄 혼합수지 중에서 선택된 1종의 수지가 함침되어 있는 아라미드 직물인 것을 특징으로 하는 방탄패널.
- 제1항 또는 제2항에 있어서, 페놀수지 함침 아라미드 직물의 적층체(C)에는 페놀수지 함침 아라미드 직물(C1, C2, C3) 2~30매가 적층되어 있는 것을 특징으로 하는 방탄패널.
- 제1항 또는 제2항에 있어서, 상기 세라믹 플레이트의 일면에만 상기 에폭시 수지 함침 직물(B)과 페놀수지 함침 아라미드 직물의 적층체(C)가 위치하는 것을 특징으로 하는 방탄패널.
- 제1항 또는 제2항에 있어서, 상기 세라믹 플레이트의 양면 모두에 상기 에폭시 수지 함침 직물(B)과 페놀수지 함침 아라미드 직물의 적층체(C)가 위치하는 것을 특징으로 하는 방탄패널.
Priority Applications (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP15875715.3A EP3242106A4 (en) | 2014-12-31 | 2015-12-30 | Bulletproof panel |
CN201580071833.XA CN107110628A (zh) | 2014-12-31 | 2015-12-30 | 防弹面板 |
JP2017530738A JP2017538911A (ja) | 2014-12-31 | 2015-12-30 | 防弾パネル |
US15/538,293 US20170343322A1 (en) | 2014-12-31 | 2015-12-30 | Bulletproof panel |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
KR1020140195170A KR20160081396A (ko) | 2014-12-31 | 2014-12-31 | 방탄패널 |
KR10-2014-0195170 | 2014-12-31 |
Publications (1)
Publication Number | Publication Date |
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WO2016108621A1 true WO2016108621A1 (ko) | 2016-07-07 |
Family
ID=56284672
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/KR2015/014487 WO2016108621A1 (ko) | 2014-12-31 | 2015-12-30 | 방탄패널 |
Country Status (6)
Country | Link |
---|---|
US (1) | US20170343322A1 (ko) |
EP (1) | EP3242106A4 (ko) |
JP (1) | JP2017538911A (ko) |
KR (1) | KR20160081396A (ko) |
CN (1) | CN107110628A (ko) |
WO (1) | WO2016108621A1 (ko) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN108759570A (zh) * | 2018-06-21 | 2018-11-06 | 江苏安卡新材料科技有限公司 | 一种防弹板及其制作方法 |
JP6904500B1 (ja) * | 2019-11-01 | 2021-07-14 | 住友ベークライト株式会社 | 湿式摩擦材用接着剤組成物 |
KR102417193B1 (ko) | 2020-11-16 | 2022-07-06 | 주식회사 신성소재 | 방탄소재용 프리프레그 및 그 제조방법 |
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- 2014-12-31 KR KR1020140195170A patent/KR20160081396A/ko not_active Application Discontinuation
-
2015
- 2015-12-30 WO PCT/KR2015/014487 patent/WO2016108621A1/ko active Application Filing
- 2015-12-30 CN CN201580071833.XA patent/CN107110628A/zh active Pending
- 2015-12-30 US US15/538,293 patent/US20170343322A1/en not_active Abandoned
- 2015-12-30 EP EP15875715.3A patent/EP3242106A4/en not_active Withdrawn
- 2015-12-30 JP JP2017530738A patent/JP2017538911A/ja active Pending
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US7930965B2 (en) * | 2006-11-08 | 2011-04-26 | Plasan Sasa Ltd. | Armor |
JP2009264692A (ja) * | 2008-04-28 | 2009-11-12 | Kyocera Chemical Corp | 複合防弾板 |
US20120088068A1 (en) * | 2009-03-30 | 2012-04-12 | Kolon Industries, Inc. | Aramid composite and method for producing the same |
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Also Published As
Publication number | Publication date |
---|---|
EP3242106A1 (en) | 2017-11-08 |
US20170343322A1 (en) | 2017-11-30 |
KR20160081396A (ko) | 2016-07-08 |
EP3242106A4 (en) | 2018-07-25 |
JP2017538911A (ja) | 2017-12-28 |
CN107110628A (zh) | 2017-08-29 |
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