CN105172256A - Preparation method for bulletproof plates different in lamination proportion of reinforcing materials - Google Patents
Preparation method for bulletproof plates different in lamination proportion of reinforcing materials Download PDFInfo
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- CN105172256A CN105172256A CN201510578771.3A CN201510578771A CN105172256A CN 105172256 A CN105172256 A CN 105172256A CN 201510578771 A CN201510578771 A CN 201510578771A CN 105172256 A CN105172256 A CN 105172256A
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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
- B32B9/00—Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00
- B32B9/005—Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00 comprising one layer of ceramic material, e.g. porcelain, ceramic tile
- B32B9/007—Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00 comprising one layer of ceramic material, e.g. porcelain, ceramic tile comprising carbon, e.g. graphite, composite carbon
-
- 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
- B32B27/34—Layered products comprising a layer of synthetic resin comprising polyamides
-
- 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
- B32B9/00—Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00
- B32B9/04—Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00 comprising such particular substance as the main or only constituent of a layer, which is next to another layer of the same or of a different material
-
- 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
- B32B2262/10—Inorganic fibres
- B32B2262/101—Glass fibres
-
- 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
- B32B2307/30—Properties of the layers or laminate having particular thermal properties
- B32B2307/306—Resistant to heat
-
- 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
- B32B2307/30—Properties of the layers or laminate having particular thermal properties
- B32B2307/306—Resistant to heat
- B32B2307/3065—Flame resistant or retardant, fire resistant or retardant
-
- 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
- B32B2307/554—Wear resistance
-
- 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
-
- 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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- Engineering & Computer Science (AREA)
- Ceramic Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Laminated Bodies (AREA)
Abstract
The invention discloses a preparation method for bulletproof plates different in lamination proportion of reinforcing materials. By taking glass fiber fabric, carbon fiber fabric and aramid fiber fabric as the reinforcing materials and a thermoplastic resin polyamide membrane as a matrix, compression molding is performed through compression molding equipment to prepare the high performance fiber-reinforced bulletproof plates; the surface density of the glass fiber fabric is 0.855 to 0.936kg/m<2>, the surface density of the carbon fiber fabric is 1.866 to 2.069kg/m<2>, and the surface density of the aramid fiber fabric is 0.768 to 0.988 kg/m<2>. The bulletproof plates prepared by the preparation method disclosed by the invention have the characteristics of being low in cost, light in weight and good in energy absorption, and the bulletproof plates play a bulletproof roll through tensile failure of fibers, layering of the bulletproof plates, debinding of the fibers and resin and back convexes generated by the materials.
Description
Technical field
The present invention relates to a kind of is reinforcing material with high-performance fiber, and thermoplastic polyamide resin film is the preparation method of the shellproof sheet material of matrix, the preparation method of the shellproof sheet material of the different lamination ratio of especially a kind of reinforcing material.
Background technology
Although the armours such as single carbon fiber, aramid fiber have excellent ballistic performance, the armour of combined type can alleviate the surface density of shellproof sheet material greatly, promotes the ballistic performance of shellproof sheet material.The ballistic performance of armour not only with the shape of bullet, the rigidity of bullet is relevant, the more important thing is that the intensity of the reinforcing material adopted with armour is relevant with frame mode.Form combined type ballistic composite at the reinforcing material central filler thermoplastic polyamide resin film of armour, not only increase ballistic performance, and anti-seismic performance improves.The protective plate of the different structure of different reinforcing material can be used as physical protection plate armour, tank, panzer etc.Wherein glass fibre, carbon fiber, aramid fiber have that light weight is high-strength, the feature of high-modulus, stability, adopt the superimposed premium properties that effectively can play different reinforcing material of different proportion, alleviate the weight of armour, improve the barrier propterty of armour, particularly resist the destruction of to kill and wound etc. of the penetrability of bullet, the explosivity of bomb and fragment.Using glass fabric, carbon fibre fabric, high-strength polyethylene fabric as reinforcing material, thermoplastic polyamide resin film is as matrix, die press technology for forming is adopted to prepare the armour of glass fibre, carbon fiber and the different lamination ratios of aramid fiber, the premium properties of this structure armour can be given full play to, meet the protection requirements of people to high-strength light armour.
Summary of the invention
The object of the invention there are provided the preparation method of the shellproof sheet material of the different lamination ratio of a kind of reinforcing material, the armour of the higher hardness that the present invention obtains can make bullet distortion, deflection, reduce bullet to the Penetration Depth of composite, the local deformation of armour, layering, the fracture of fiber and unsticking withdrawing will consume the kinetic energy of bullet further.In addition adopt compression-moulding methods production efficiency higher, product size is accurate, any surface finish, and every procedure of forming process all controls than being easier to, and pressing reliable in quality, weapons, aircraft, guided missile are widely applied.
In order to achieve the above object, technical scheme of the present invention is:
The preparation method of the shellproof sheet material of the different lamination ratio of a kind of reinforcing material, with glass fabric (being purchased from Nanjing Glass Fibre Research and Design Institute), carbon fibre fabric (being purchased from toray company), aramid fabric (being purchased from the farsighted Chemical Co., Ltd. in Changzhou) for reinforcing material, the feature making full use of this order of fabric construction, globality and compactness makes it have very high mechanical strength effect in longitude and latitude both direction, (is purchased from thermoplastic polyamide resin film
dong Sheng business corporation of Shenzhen) be matrix, utilize the characteristic of the resistance to impact of thermoplastic polyamide resin film, heat resistance, rub resistance, anti-flammability, by compression molding device compression molding, obtained high-performance fiber strengthens armour; The surface density of described glass fabric is: 0.855 ~ 0.936kg/m
2, the surface density of carbon fibre fabric is: 1.866 ~ 2.069kg/m
2, the surface density of aramid fabric is: 0.768 ~ 0.988kg/m
2.
The number of plies of described reinforcing material is 16 ~ 18 layers, and described base thermoplastic's resin PA membrane number of plies is the number of plies-1 of reinforcing material.
Described glass fabric, carbon fibre fabric, aramid fabric tissue adopt plain weave construction.
The clamp time of described compression molding device is 15min ~ 30min; Molding temperature is 100 DEG C ~ 120 DEG C; Molding pressure is 5MPa ~ 15MPa.
The invention has the beneficial effects as follows: the preparation method of the shellproof sheet material of the different lamination ratio of a kind of reinforcing material of the present invention, with glass fabric, carbon fibre fabric, aramid fabric for reinforcing material.Adopt the feature of this order of fabric construction, globality and compactness to give the bearing capacity of a lot of excellent characteristic of bulletproof composite board as better structural stability and Geng Gao, make it have very high mechanical strength in longitude and latitude both direction.Thermoplastic polyamide resin film matrix has very high combination property in addition, resistance to impact, heat resistance, rub resistance and have certain anti-flammability.Thus the polyamide armour of glass fabric, carbon fibre fabric, aramid fabric enhancing, take full advantage of the good characteristic of various material, obtain dissimilar armour by the different lamination ratios changing reinforcing material, ensure that armour has the advantages that cost is low, quality is light, energy-absorbing is good simultaneously.This armour is mainly by the tension failure of fiber, the layering of armour, and the back of the body that the unsticking of fiber and resin and material produce is convex and play shellproof effect.In addition adopt compression molding compression-moulding methods production efficiency higher, product size is accurate, any surface finish, and every procedure of forming process all controls than being easier to, and pressing reliable in quality, weapons, aircraft, guided missile have obtained extensive use.
Detailed description of the invention
Embodiment 1
The preparation method of the shellproof sheet material of the different lamination ratio of a kind of reinforcing material of the present embodiment, with high-performance fiber fabric glass fibre fabric (being purchased from Nanjing Glass Fibre Research and Design Institute)
, carbon fibre fabric (being purchased from toray company), aramid fabric (being purchased from the farsighted Chemical Co., Ltd. in Changzhou) be reinforcing material, the feature making full use of this order of fabric construction, globality and compactness makes it have very high mechanical strength effect in longitude and latitude both direction, and thermoplastic polyamide resin film (is purchased from
dong Sheng business corporation of Shenzhen) resistance to impact, heat resistance, rub resistance, the anti-flammability characteristic of matrix, by compression molding device compression molding, obtained high-performance fiber strengthens armour.
Be specially: be first 0.896kg/m by surface density
2fiberglass scrim, surface density are 1.986kg/m
2carbon fiber plain cloth and surface density be 0.798kg/m
2aramid fiber plain cloth and thermoplastic polyamide resin film be cut into the size of 20 ㎝ × 20 ㎝.Then by reinforcing material according to fiberglass scrim: carbon fiber plain cloth: the ratio laying successively of aramid fiber plain cloth=6:6:6.Wherein six layers of glass fabric is placed on the front of armour, then six layers of carbon fibre fabric are placed successively, finally six layers of aramid fabric, the number of plies of reinforcing material is made to be 18 layers, the thermoplastic polyamide resin of the laying between layers film of reinforcing material, then the number of plies of thermoplastic polyamide resin film is 17 layers.Finally reinforcing material good for laying and resin film entirety are carried out compression molding on XLB25-L vulcanizing press.The clamp time of described XLB25-L vulcanizing press is 15min; Molding temperature is 105 DEG C; Molding pressure is 5MPa; Obtained glass fibre, carbon fiber and aramid fiber armour.
The preparation method of the shellproof sheet material of the different lamination ratio of a kind of reinforcing material of the present embodiment, with glass fabric, carbon fibre fabric, aramid fabric is reinforcing material, make full use of this order of fabric construction, the feature of globality and compactness makes it have very high mechanical strength and thermoplastic polyamide resin film matrix resistance to impact in longitude and latitude both direction, heat resistance, the advantage of rub resistance, dissimilar armour is obtained by the different lamination ratios changing reinforcing material, ensure that armour has cost low simultaneously, quality is light, the feature that energy-absorbing is good.This armour is mainly by the tension failure of fiber, the layering of armour, and the back of the body that the unsticking of fiber and resin and material produce is convex and play shellproof effect.In addition adopt compression molding compression-moulding methods production efficiency higher, product size is accurate, any surface finish, and every procedure of forming process all controls than being easier to, and pressing reliable in quality, weapons, aircraft, guided missile are widely applied.
Embodiment 2
The preparation method of the shellproof sheet material of the different lamination ratio of a kind of reinforcing material of the present embodiment, with high-performance fiber fabric glass fibre fabric (being purchased from Nanjing Glass Fibre Research and Design Institute)
, carbon fibre fabric (being purchased from toray company), aramid fabric (being purchased from the farsighted Chemical Co., Ltd. in Changzhou) be reinforcing material, the feature making full use of this order of fabric construction, globality and compactness makes it have very high mechanical strength effect in longitude and latitude both direction, and thermoplastic polyamide resin film (is purchased from
dong Sheng business corporation of Shenzhen) resistance to impact, heat resistance, rub resistance, anti-flammability characteristic, by compression molding device compression molding, obtained high-performance fiber strengthens armour.
Be specially: be first 0.912kg/m by surface density
2fiberglass scrim, surface density are 2.010kg/m
2carbon fiber plain cloth and surface density be 0.946kg/m
2aramid fiber plain cloth and thermoplastic polyamide resin film be cut into the size of 20 ㎝ × 20 ㎝.Then by reinforcing material according to fiberglass scrim: carbon fiber plain cloth: the ratio laying successively of aramid fiber plain cloth=4:8:6.Wherein four-layer glass fiber plain cloth is placed on the front of armour, then eight layers of carbon fibre fabric are placed successively, finally six layers of aramid fabric, the number of plies of reinforcing material is made to be 18 layers, the thermoplastic polyamide resin of the laying between layers film of reinforcing material, then the number of plies of thermoplastic polyamide resin film is 17 layers.The reinforcing material good by laying and the superimposed XLB25-L of the being placed on vulcanizing press of resin film carry out compression molding.The clamp time of described XLB25-L vulcanizing press is 20min; Molding temperature is 110 DEG C; Molding pressure is 7.5MPa; Obtained glass fibre, carbon fiber and aramid fiber armour.
The preparation method of the shellproof sheet material of the different lamination ratio of a kind of reinforcing material of the present embodiment, with glass fabric, carbon fibre fabric, aramid fabric is reinforcing material, make full use of this order of fabric construction, the feature of globality and compactness makes it have very high mechanical strength and thermoplastic polyamide resin film matrix resistance to impact in longitude and latitude both direction, heat resistance, the advantage of rub resistance, dissimilar armour is obtained by the different lamination ratios changing reinforcing material, ensure that armour has cost low simultaneously, quality is light, the feature that energy-absorbing is good.This armour is mainly by the tension failure of fiber, the layering of armour, and the back of the body that the unsticking of fiber and resin and material produce is convex and play shellproof effect.In addition adopt compression-moulding methods production efficiency higher, product size is accurate, any surface finish, and every procedure of forming process all controls than being easier to, and pressing reliable in quality, weapons, aircraft, guided missile are widely applied.
Embodiment 3
The preparation method of the shellproof sheet material of the different lamination ratio of a kind of reinforcing material of the present embodiment, with high-performance fiber fabric glass fibre fabric (being purchased from Nanjing Glass Fibre Research and Design Institute)
, carbon fibre fabric (being purchased from toray company), aramid fabric (being purchased from the farsighted Chemical Co., Ltd. in Changzhou) be reinforcing material, the feature making full use of this order of fabric construction, globality and compactness makes it have very high mechanical strength effect in longitude and latitude both direction, and thermoplastic polyamide resin film (is purchased from
dong Sheng business corporation of Shenzhen) resistance to impact, heat resistance, rub resistance, anti-flammability advantage, by compression molding device compression molding, obtained high-performance fiber strengthens armour.
Be specially: be first 0.936kg/m by surface density
2fiberglass scrim, surface density are 2.069kg/m
2carbon fiber plain cloth and surface density be 0.988kg/m
2aramid fiber plain cloth and thermoplastic polyamide resin film be cut into the size of 20 ㎝ × 20 ㎝.Then by reinforcing material according to fiberglass scrim: carbon fiber plain cloth: the ratio laying successively of aramid fiber plain cloth=2:8:6.Wherein layer glass fiber plain cloth is placed on the front of armour, then eight layers of carbon fibre fabric are placed successively, be finally the number of plies of six layers of aramid fabric reinforcing material it is 16 layers, the thermoplastic polyamide resin of the laying between layers film of reinforcing material, then the number of plies of thermoplastic polyamide resin film is 15 layers.The reinforcing material good by laying and the superimposed XLB25-L of the being placed on vulcanizing press of resin film carry out compression molding.The clamp time of described XLB25-L vulcanizing press is 25min; Molding temperature is 115 DEG C; Molding pressure is 10MPa; Obtained glass fibre, carbon fiber and aramid fiber armour.
The preparation method of the shellproof sheet material of the different lamination ratio of a kind of reinforcing material of the present embodiment, with glass fabric, carbon fibre fabric, aramid fabric is reinforcing material, make full use of this order of fabric construction, the feature of globality and compactness makes it have very high mechanical strength in longitude and latitude both direction and utilize thermoplastic polyamide resin film matrix resistance to impact, heat resistance, the advantage of rub resistance, dissimilar armour is obtained by the different lamination ratios changing reinforcing material, ensure that armour has cost low simultaneously, quality is light, the feature that energy-absorbing is good.This armour is mainly by the tension failure of fiber, the layering of armour, and the back of the body that the unsticking of fiber and resin and material produce is convex and play shellproof effect.In addition adopt compression-moulding methods production efficiency higher, product size is accurate, any surface finish, and every procedure of forming process all controls than being easier to, and pressing reliable in quality, weapons, aircraft, guided missile are widely applied.
Embodiment 4
The preparation method of the shellproof sheet material of the different lamination ratio of a kind of reinforcing material of the present embodiment, with high-performance fiber fabric glass fibre fabric (being purchased from Nanjing Glass Fibre Research and Design Institute)
, carbon fibre fabric (being purchased from toray company), aramid fabric (being purchased from the farsighted Chemical Co., Ltd. in Changzhou) be reinforcing material, the feature making full use of this order of fabric construction, globality and compactness makes it have very high mechanical strength effect in longitude and latitude both direction, and thermoplastic polyamide resin film (is purchased from
dong Sheng business corporation of Shenzhen) resistance to impact, heat resistance, rub resistance, anti-flammability advantage, by compression molding device compression molding, obtained high-performance fiber strengthens armour.
Be specially: be first 0.936kg/m by surface density
2fiberglass scrim, surface density are 2.069kg/m
2carbon fiber plain cloth and surface density be 0.988kg/m
2aramid fiber plain cloth and thermoplastic polyamide resin film be cut into the size of 20 ㎝ × 20 ㎝.Then by reinforcing material according to fiberglass scrim: carbon fiber plain cloth: the ratio laying successively of aramid fiber plain cloth=2:9:6.Wherein layer glass fiber plain cloth is placed on the front of armour, then nine layers of carbon fibre fabric are placed successively, finally six layers of aramid fabric, the number of plies of its reinforcing material is made to be 17 layers, the thermoplastic polyamide resin of the laying between layers film of reinforcing material, then the number of plies of thermoplastic polyamide resin film is 16 layers.The reinforcing material good by laying and the superimposed XLB25-L of the being placed on vulcanizing press of resin film carry out compression molding.The clamp time of described XLB25-L vulcanizing press is 30min; Molding temperature is 120 DEG C; Molding pressure is 15MPa; Obtained glass fibre, carbon fiber and aramid fiber armour.
The preparation method of the shellproof sheet material of the different lamination ratio of a kind of reinforcing material of the present embodiment, with glass fabric, carbon fibre fabric, aramid fabric is reinforcing material, make full use of this order of fabric construction, the feature of globality and compactness makes it have very high mechanical strength and thermoplastic polyamide resin film matrix resistance to impact in longitude and latitude both direction, heat resistance, the characteristic of rub resistance, dissimilar armour is obtained by the different lamination ratios changing reinforcing material, ensure that armour has cost low simultaneously, quality is light, the feature that energy-absorbing is good.This armour is mainly by the tension failure of fiber, the layering of armour, and the back of the body that the unsticking of fiber and resin and material produce is convex and play shellproof effect.In addition adopt compression molding compression-moulding methods production efficiency higher, product size is accurate, any surface finish, and every procedure of forming process all controls than being easier to, and pressing reliable in quality, weapons, aircraft, guided missile are widely applied.
Claims (4)
1. the preparation method of the shellproof sheet material of the different lamination ratio of reinforcing material, it is characterized in that: with glass fabric, carbon fibre fabric, aramid fabric for reinforcing material, with thermoplastic polyamide resin film for matrix, by compression molding device compression molding, obtained high-performance fiber strengthens armour; The surface density of described glass fabric is: 0.855 ~ 0.936kg/m
2, the surface density of carbon fibre fabric is: 1.866 ~ 2.069kg/m
2, the surface density of aramid fabric is: 0.768 ~ 0.988kg/m
2.
2. the preparation method of the shellproof sheet material of the different lamination ratio of a kind of reinforcing material as claimed in claim 1, it is characterized in that: the number of plies of described reinforcing material is 16 ~ 18 layers, described base thermoplastic's resin PA membrane number of plies is the number of plies-1 of reinforcing material.
3. the preparation method of the shellproof sheet material of the different lamination ratio of a kind of reinforcing material as claimed in claim 1, is characterized in that: described glass fabric, carbon fibre fabric, aramid fabric tissue adopt plain weave construction.
4. the preparation method of the shellproof sheet material of the different lamination ratio of a kind of reinforcing material as claimed in claim 1, is characterized in that: the clamp time of described compression molding device is 15min ~ 30min; Molding temperature is 100 DEG C ~ 120 DEG C; Molding pressure is 5MPa ~ 15MPa.
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510578771.3A CN105172256A (en) | 2015-09-14 | 2015-09-14 | Preparation method for bulletproof plates different in lamination proportion of reinforcing materials |
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| Application Number | Priority Date | Filing Date | Title |
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| CN201510578771.3A CN105172256A (en) | 2015-09-14 | 2015-09-14 | Preparation method for bulletproof plates different in lamination proportion of reinforcing materials |
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Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105667019A (en) * | 2016-02-05 | 2016-06-15 | 山东中恒碳纤维科技发展有限公司 | Composite structure bulletproof armor capable of resisting machine gun ammunition penetration and manufacturing method thereof |
| CN105949764A (en) * | 2016-05-31 | 2016-09-21 | 苏州高甲防护科技有限公司 | Bulletproof inserting plate and preparation method |
| CN105948774A (en) * | 2016-04-13 | 2016-09-21 | 南通大学 | Preparation method for superhard carbon/carbon bulletproof material |
| CN111171557A (en) * | 2020-01-14 | 2020-05-19 | 株洲时代工程塑料科技有限责任公司 | Continuous fiber reinforced polyamide composite material and preparation method and application thereof |
| CN113276523A (en) * | 2021-02-03 | 2021-08-20 | 山东非金属材料研究所 | PBO fiber/aramid fiber reinforced composite material and preparation method thereof |
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| GB9024069D0 (en) * | 1990-11-06 | 1990-12-19 | Shrinemark Limited | Protective sheet material |
| CN1329985A (en) * | 2001-07-30 | 2002-01-09 | 中国兵器工业第五三研究所 | Components of composite bullet-resistant plate and its preparing process |
| CN103119391A (en) * | 2010-07-28 | 2013-05-22 | 霍尼韦尔国际公司 | Ballistic shield composites with enhanced fragment resistance |
| CN103770343A (en) * | 2014-01-20 | 2014-05-07 | 宁波大成新材料股份有限公司 | Production method of high-performance fiber composite product |
-
2015
- 2015-09-14 CN CN201510578771.3A patent/CN105172256A/en active Pending
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB9024069D0 (en) * | 1990-11-06 | 1990-12-19 | Shrinemark Limited | Protective sheet material |
| CN1329985A (en) * | 2001-07-30 | 2002-01-09 | 中国兵器工业第五三研究所 | Components of composite bullet-resistant plate and its preparing process |
| CN103119391A (en) * | 2010-07-28 | 2013-05-22 | 霍尼韦尔国际公司 | Ballistic shield composites with enhanced fragment resistance |
| CN103770343A (en) * | 2014-01-20 | 2014-05-07 | 宁波大成新材料股份有限公司 | Production method of high-performance fiber composite product |
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105667019A (en) * | 2016-02-05 | 2016-06-15 | 山东中恒碳纤维科技发展有限公司 | Composite structure bulletproof armor capable of resisting machine gun ammunition penetration and manufacturing method thereof |
| CN105667019B (en) * | 2016-02-05 | 2017-09-29 | 山东中恒碳纤维科技发展有限公司 | A kind of composite construction bulletproof armour for resisting machine gun bullet penetration and preparation method thereof |
| CN105948774A (en) * | 2016-04-13 | 2016-09-21 | 南通大学 | Preparation method for superhard carbon/carbon bulletproof material |
| CN105948774B (en) * | 2016-04-13 | 2020-06-26 | 南通大学 | Preparation method of superhard carbon/carbon bulletproof material |
| CN105949764A (en) * | 2016-05-31 | 2016-09-21 | 苏州高甲防护科技有限公司 | Bulletproof inserting plate and preparation method |
| CN111171557A (en) * | 2020-01-14 | 2020-05-19 | 株洲时代工程塑料科技有限责任公司 | Continuous fiber reinforced polyamide composite material and preparation method and application thereof |
| CN113276523A (en) * | 2021-02-03 | 2021-08-20 | 山东非金属材料研究所 | PBO fiber/aramid fiber reinforced composite material and preparation method thereof |
| CN113276523B (en) * | 2021-02-03 | 2022-08-05 | 山东非金属材料研究所 | PBO fiber/aramid fiber reinforced composite material and preparation method thereof |
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Application publication date: 20151223 |