CN106380199A - 纤维增加碳化硅陶瓷防弹板的制作方法 - Google Patents

纤维增加碳化硅陶瓷防弹板的制作方法 Download PDF

Info

Publication number
CN106380199A
CN106380199A CN201610761357.0A CN201610761357A CN106380199A CN 106380199 A CN106380199 A CN 106380199A CN 201610761357 A CN201610761357 A CN 201610761357A CN 106380199 A CN106380199 A CN 106380199A
Authority
CN
China
Prior art keywords
fiber
silicon carbide
armour
powder
ceramics
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
CN201610761357.0A
Other languages
English (en)
Inventor
张国军
方宁象
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Zhejiang Li Tai Composite Ltd Co
Original Assignee
Zhejiang Li Tai Composite Ltd Co
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Zhejiang Li Tai Composite Ltd Co filed Critical Zhejiang Li Tai Composite Ltd Co
Priority to CN201610761357.0A priority Critical patent/CN106380199A/zh
Publication of CN106380199A publication Critical patent/CN106380199A/zh
Pending legal-status Critical Current

Links

Classifications

    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B35/00Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
    • C04B35/515Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics
    • C04B35/56Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics based on carbides or oxycarbides
    • C04B35/565Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics based on carbides or oxycarbides based on silicon carbide
    • C04B35/573Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics based on carbides or oxycarbides based on silicon carbide obtained by reaction sintering or recrystallisation
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B9/00Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00
    • B32B9/005Layered 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
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B9/00Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00
    • B32B9/04Layered 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
    • B32B9/047Layered 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 made of fibres or filaments
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B35/00Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
    • C04B35/515Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics
    • C04B35/56Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics based on carbides or oxycarbides
    • C04B35/563Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics based on carbides or oxycarbides based on boron carbide
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B35/00Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
    • C04B35/622Forming processes; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
    • C04B35/64Burning or sintering processes
    • C04B35/65Reaction sintering of free metal- or free silicon-containing compositions
    • C04B35/806
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B35/00Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
    • C04B35/71Ceramic products containing macroscopic reinforcing agents
    • C04B35/78Ceramic products containing macroscopic reinforcing agents containing non-metallic materials
    • C04B35/80Fibres, filaments, whiskers, platelets, or the like
    • C04B35/82Asbestos; Glass; Fused silica
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41HARMOUR; ARMOURED TURRETS; ARMOURED OR ARMED VEHICLES; MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL
    • F41H5/00Armour; Armour plates
    • F41H5/02Plate construction
    • F41H5/04Plate construction composed of more than one layer
    • F41H5/0414Layered armour containing ceramic material
    • F41H5/0428Ceramic layers in combination with additional layers made of fibres, fabrics or plastics
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2262/00Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
    • B32B2262/02Synthetic macromolecular fibres
    • B32B2262/0253Polyolefin fibres
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2262/00Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
    • B32B2262/02Synthetic macromolecular fibres
    • B32B2262/0261Polyamide fibres
    • B32B2262/0269Aromatic polyamide fibres
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2262/00Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
    • B32B2262/10Inorganic fibres
    • B32B2262/105Ceramic fibres
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2307/00Properties of the layers or laminate
    • B32B2307/50Properties of the layers or laminate having particular mechanical properties
    • B32B2307/558Impact strength, toughness
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2571/00Protective equipment
    • B32B2571/02Protective equipment defensive, e.g. armour plates, anti-ballistic clothing

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Ceramic Engineering (AREA)
  • Manufacturing & Machinery (AREA)
  • Materials Engineering (AREA)
  • Structural Engineering (AREA)
  • Organic Chemistry (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Inorganic Chemistry (AREA)
  • General Engineering & Computer Science (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)

Abstract

本发明是纤维增强碳化硅陶瓷加背板复合防弹板的制作方法,包括如下步骤:a、制粉:将碳化硅粉末、碳源、碳化硅纤维、添加剂等混合后造粒,得到纤维增强碳化硅陶瓷粉料;b、压制:将制得的纤维增强碳化硅陶瓷粉料模压,得到纤维增强碳化硅陶瓷生坯;c、烧结:将上述生坯放入真空烧结炉内渗硅反应烧结,烧结温度为1500~1800℃,烧结时间为5小时~25小时,得到纤维增强碳化硅陶瓷;d、复合:将纤维增强碳化硅陶瓷与纤维复合材料背板复合在一起,得到纤维增强碳化硅陶瓷加背板复合防弹板,其防弹性能满足NIJ0101.06 标准IV级要求,防弹性能优越。

Description

纤维增加碳化硅陶瓷防弹板的制作方法
技术领域:
本发明涉及陶瓷加背板复合防弹板领域,特别涉及纤维增加碳化硅陶瓷防弹板的制作方法。
背景技术:
随着防弹领域技术的发展,防弹板种类越来越多,由起初的钢板到现在的陶瓷加背板结构的复合防弹板等。
现有的陶瓷板加背板结构的复合防弹板由于陶瓷本身的脆性特性,抗多发弹性能较差。为了提高其抗多发弹性能,纤维增韧是其中重要的方案之一。
发明内容:
本发明的目的就是针对现有技术之不足,而提供一纤维增加碳化硅陶瓷防弹板的制作方法,能有效提高陶瓷加背板复合防弹板抗多发弹性能。
本发明的技术方案如下:
纤维增加碳化硅陶瓷防弹板的制作方法,包括如下步骤:
a、制粉:将碳化硅粉末、碳源、碳化硅纤维、添加剂等混合后造粒,得到纤维增强碳化硅陶瓷粉料;
b、压制:将制得的纤维增强碳化硅陶瓷粉料模压,得到纤维增强碳化硅陶瓷生坯;
c、烧结:将上述生坯放入真空烧结炉内渗硅反应烧结,烧结温度为1500~1800℃,烧结时间为5小时~25小时,得到纤维增强碳化硅陶瓷;
d、复合:将纤维增强碳化硅陶瓷与纤维复合材料背板复合在一起,得到纤维增强碳化硅陶瓷加背板复合防弹板。采用这种方式就可以使纤维充满整个防弹板的内部,使得防弹板在被打击时不仅可以通过纤维卸力,杂乱的碳化硅纤维排序更可以止裂,从而极大得强化了由此方法制得的纤维增加碳化硅陶瓷防弹板的强度以及防弹性能,经过测试由此方法制得的纤维增加碳化硅陶瓷防弹板的防弹性能达到了NIJ标准的Ⅳ级标准,不仅可以防手枪子弹,更可以防.30及以下口径的步枪穿甲弹,极大的提升了使用者的生存率。
作为优选,主要原料为碳化硅粉末、碳源、碳化硅纤维的混合物。
作为优选,背板材料为芳纶或者超高分子量聚乙烯纤维。
作为优选,增强纤维为碳化硅纤维,纤维的直径为0. 1um~20um,长度为20um~500um。
作为优选,纤维加入量为原料质量的0.1%~10%。
本发明的有益效果在于:
本发明采用这种方式可以提高陶瓷的韧性和抗多发弹性能。经过测试,由此方法制得的防弹板的防弹性能满足NIJ0101.06 标准IV级要求,并且能防御3发子弹的射击。
附图说明:
图1为实施例1~3的纤维内嵌式强化防弹板坯板的结构示意图;
图2为实施例4~6的纤维内嵌式强化防弹板坯板的结构示意图;
图中:防弹坯板本体1。
具体实施方式:
实施例1:纤维增加碳化硅陶瓷防弹板的制作方法,包括如下步骤:
a、混合压胚:将陶瓷粉和纤维混合后压胚,得到胚体;
b、压铸:将胚体放入真空烧结炉内加热,加热温度为1750℃,加热时间为6小时;
c、冷却:加热完毕,待冷却后,脱模后就得到纤维内嵌式强化防弹板坯板;
d、复合:将纤维内嵌式强化防弹板坯板和强化板念粘合在一起,再进行表面处理后得到纤维内嵌式强化防弹板。
陶瓷粉为碳化硅粉末。
纤维为玻璃纤维。
纤维的直径为0.1mm,所述纤维的长度为2mm。
压胚内纤维的加入量为陶瓷粉质量的0.5%。
混合压胚步骤中采用温等静压设备,压制压力为150Mpa。
一种如图1所示的一种纤维内嵌式强化防弹板,包括防弹坯板本体1,防弹坯板本体1呈平板状,防弹坯板本体1内填充有大量纤维。
本纤维内嵌式强化防弹板坯板经过NIJ标准测试,可防御.30口径穿甲弹(美国军用M2 AP),弹重10.8g,弹速870m/s,达到Ⅳ级防弹标准。
实施例2:纤维增加碳化硅陶瓷防弹板的制作方法,包括如下步骤:
a、混合压胚:将陶瓷粉和纤维混合后压胚,得到胚体;
b、压铸:将胚体放入真空烧结炉内加热,加热温度为2050℃,加热时间为3小时;
c、冷却:加热完毕,待冷却后,脱模后就得到纤维内嵌式强化防弹板坯板;
d、复合:将纤维内嵌式强化防弹板坯板和强化板念粘合在一起,再进行表面处理后得到纤维内嵌式强化防弹板。
陶瓷粉为碳化硼粉末。
纤维为碳纤维。
纤维的直径为0.01mm,纤维的长度为6mm。
压胚内纤维的加入量为陶瓷粉质量的4%。
混合压胚步骤中采用温等静压设备,压制压力为100Mpa。
一种如图1所示的一种纤维内嵌式强化防弹板,包括防弹坯板本体1,防弹坯板本体1呈平板状,防弹坯板本体1内填充有大量纤维。
本纤维内嵌式强化防弹板坯板经过NIJ标准测试,可防御.30口径穿甲弹(美国军用M2 AP),弹重10.8g,弹速855m/s,达到Ⅳ级防弹标准。
实施例3:纤维增加碳化硅陶瓷防弹板的制作方法,包括如下步骤:
a、混合压胚:将陶瓷粉和纤维混合后压胚,得到胚体;
b、压铸:将胚体放入真空烧结炉内加热,加热温度为1900℃,加热时间为6小时;
c、冷却:加热完毕,待冷却后,脱模后就得到纤维内嵌式强化防弹板坯板;
d、复合:将纤维内嵌式强化防弹板坯板和强化板念粘合在一起,再进行表面处理后得到纤维内嵌式强化防弹板。
陶瓷粉为碳化硅粉末碳化硼粉末两者的混合粉末。
纤维为硫化玻璃纤维。
纤维的直径为0.5mm,纤维的长度为10mm。
压胚内纤维的加入量为陶瓷粉质量的10%。
混合压胚步骤中采用温等静压设备,压制压力为300Mpa。
一种如图1所示的一种纤维内嵌式强化防弹板,包括防弹坯板本体1,防弹坯板本体1呈平板状,防弹坯板本体1内填充有大量纤维。
本纤维内嵌式强化防弹板坯板经过NIJ标准测试,可防御.30口径穿甲弹(美国军用M2 AP),弹重10.8g,弹速880m/s,达到Ⅳ级防弹标准。
实施例4:纤维增加碳化硅陶瓷防弹板的制作方法,包括如下步骤:
a、混合压胚:将陶瓷粉和纤维混合后压胚,得到胚体;
b、压铸:将胚体放入真空烧结炉内加热,加热温度为2000℃,加热时间为5小时;
c、冷却:加热完毕,待冷却后,脱模后就得到纤维内嵌式强化防弹板坯板;
d、复合:将纤维内嵌式强化防弹板坯板和强化板念粘合在一起,再进行表面处理后得到纤维内嵌式强化防弹板。
陶瓷粉为碳化硅粉末。
纤维为玻璃纤维。
纤维的直径为0.3mm,纤维的长度为8mm。
压胚内纤维的加入量为陶瓷粉质量的20%。
混合压胚步骤中采用温等静压设备,压制压力为100Mpa。
一种如图2所示的一种纤维内嵌式强化防弹板,包括防弹坯板本体1,防弹坯板本体1呈弧形板状,防弹坯板本体1内填充有大量纤维。
防弹坯板本体呈弧形板状,且弧度为25°。
本纤维内嵌式强化防弹板坯板经过NIJ标准测试,可防御.30口径穿甲弹(美国军用M2 AP),弹重10.8g,最高承受弹速889m/s,达到Ⅳ级防弹标准。
实施例5:纤维增加碳化硅陶瓷防弹板的制作方法,包括如下步骤:
a、混合压胚:将陶瓷粉和纤维混合后压胚,得到胚体;
b、压铸:将胚体放入真空烧结炉内加热,加热温度为1800℃,加热时间为4小时;
c、冷却:加热完毕,待冷却后,脱模后就得到纤维内嵌式强化防弹板坯板;
d、复合:将纤维内嵌式强化防弹板坯板和强化板念粘合在一起,再进行表面处理后得到纤维内嵌式强化防弹板。
陶瓷粉为碳化硼粉末。
纤维为碳纤维。
纤维的直径为0.02mm,所述纤维的长度为0.5mm。
压胚内纤维的加入量为陶瓷粉质量的12%。
混合压胚步骤中采用温等静压设备,压制压力为150Mpa。
一种如图2所示的一种纤维内嵌式强化防弹板,包括防弹坯板本体1,防弹坯板本体1呈弧形板状,防弹坯板本体1内填充有大量纤维。
防弹坯板本体呈弧形板状,且弧度为40°。
本纤维内嵌式强化防弹板坯板经过NIJ标准测试,可防御.30口径穿甲弹(美国军用M2 AP),弹重10.8g,最高承受弹速915m/s,达到Ⅳ级防弹标准。
实施例6:纤维增加碳化硅陶瓷防弹板的制作方法,包括如下步骤:
a、混合压胚:将陶瓷粉和纤维混合后压胚,得到胚体;
b、压铸:将胚体放入真空烧结炉内加热,加热温度为2050℃,加热时间为4小时;
c、冷却:加热完毕,待冷却后,脱模后就得到纤维内嵌式强化防弹板坯板;
d、复合:将纤维内嵌式强化防弹板坯板和强化板念粘合在一起,再进行表面处理后得到纤维内嵌式强化防弹板。
陶瓷粉为碳化硅粉末与碳化硼粉末两者的混合粉末。
纤维为硫化玻璃纤维。
纤维的直径为0.5mm,所述纤维的长度为8mm。
压胚内纤维的加入量为陶瓷粉质量的10%。
混合压胚步骤中采用温等静压设备,压制压力为250Mpa。
一种如图2所示的一种纤维内嵌式强化防弹板,包括防弹坯板本体1,防弹坯板本体1呈弧形板状,防弹坯板本体1内填充有大量纤维。
防弹坯板本体呈弧形板状,且弧度为32°
本纤维内嵌式强化防弹板坯板经过NIJ标准测试,可防御.30口径穿甲弹(美国军用M2AP),弹重10.8g,最高承受弹速1102m/s,达到Ⅳ级防弹标准。
以上所述仅为本发明的较佳实施例,本领域普通技术人员在没有做出创造性劳动前提下所获得的所有其他实施例,都应当属于本发明保护的范围。

Claims (5)

1.纤维增加碳化硅陶瓷防弹板的制作方法,其特征在于:包括如下步骤:
a、制粉:将碳化硅粉末、碳源、碳化硅纤维、添加剂等混合后造粒,得到纤维增强碳化硅陶瓷粉料;
b、压制:将制得的纤维增强碳化硅陶瓷粉料模压,得到纤维增强碳化硅陶瓷生坯;
c、烧结:将上述生坯放入真空烧结炉内渗硅反应烧结,烧结温度为1500~1800℃,烧结时间为5小时~25小时,得到纤维增强碳化硅陶瓷;
d、复合:将纤维增强碳化硅陶瓷与纤维复合材料背板复合在一起,得到纤维增强碳化硅陶瓷加背板复合防弹板。
2.根据权利要求1 所述的纤维增加碳化硅陶瓷防弹板的制作方法,其特征在于:所述陶瓷粉为碳化硅粉末、碳源、碳化硅纤维的混合粉末。
3.根据权利要求1所述的纤维增加碳化硅陶瓷防弹板的制作方法,其特征在于:所述纤维复合材料背板为芳纶或者超高分子量聚乙烯材料纤维。
4.根据权利要求1所述的纤维增加碳化硅陶瓷防弹板的制作方法,其特征在于:所述碳化硅纤维的直径为0. 1um~20um,长度为20um~500um。
5.根据权利要求1所述的纤维增加碳化硅陶瓷防弹板的制作方法,其特征在于:所述生坯中碳化硅纤维的加入量为原料质量的0.1%~10%。
CN201610761357.0A 2016-08-31 2016-08-31 纤维增加碳化硅陶瓷防弹板的制作方法 Pending CN106380199A (zh)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201610761357.0A CN106380199A (zh) 2016-08-31 2016-08-31 纤维增加碳化硅陶瓷防弹板的制作方法

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201610761357.0A CN106380199A (zh) 2016-08-31 2016-08-31 纤维增加碳化硅陶瓷防弹板的制作方法

Publications (1)

Publication Number Publication Date
CN106380199A true CN106380199A (zh) 2017-02-08

Family

ID=57939570

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201610761357.0A Pending CN106380199A (zh) 2016-08-31 2016-08-31 纤维增加碳化硅陶瓷防弹板的制作方法

Country Status (1)

Country Link
CN (1) CN106380199A (zh)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107556012A (zh) * 2017-08-28 2018-01-09 郑州市立新实业有限公司 一种嵌扣式防弹陶瓷片及其制备方法
CN114993113A (zh) * 2022-06-22 2022-09-02 浙江富研新型材料有限公司 防弹用多晶钻石烧结体及其应用
WO2023221297A1 (zh) * 2022-05-19 2023-11-23 浙江立泰复合材料股份有限公司 一种抗多发弹陶瓷的制备方法及防弹插板

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101555144A (zh) * 2009-05-21 2009-10-14 浙江大学 碳化硅短纤维增韧强化碳化硅陶瓷及其制备方法
CN202382650U (zh) * 2011-11-01 2012-08-15 北京同益中特种纤维技术开发有限公司 陶瓷复合防弹板
JP5405844B2 (ja) * 2009-02-02 2014-02-05 株式会社日本セラテック 耐衝撃部材
CN103868413A (zh) * 2014-02-24 2014-06-18 北京同益中特种纤维技术开发有限公司 一种陶瓷复合防弹板
CN104045348A (zh) * 2014-06-19 2014-09-17 浙江立泰复合材料有限公司 反应烧结陶瓷防弹插板及反应烧结防弹陶瓷的制备方法
CN104671790A (zh) * 2015-01-28 2015-06-03 安徽省和翰光电科技有限公司 一种防弹板用碳化硅陶瓷及其制备方法

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP5405844B2 (ja) * 2009-02-02 2014-02-05 株式会社日本セラテック 耐衝撃部材
CN101555144A (zh) * 2009-05-21 2009-10-14 浙江大学 碳化硅短纤维增韧强化碳化硅陶瓷及其制备方法
CN202382650U (zh) * 2011-11-01 2012-08-15 北京同益中特种纤维技术开发有限公司 陶瓷复合防弹板
CN103868413A (zh) * 2014-02-24 2014-06-18 北京同益中特种纤维技术开发有限公司 一种陶瓷复合防弹板
CN104045348A (zh) * 2014-06-19 2014-09-17 浙江立泰复合材料有限公司 反应烧结陶瓷防弹插板及反应烧结防弹陶瓷的制备方法
CN104671790A (zh) * 2015-01-28 2015-06-03 安徽省和翰光电科技有限公司 一种防弹板用碳化硅陶瓷及其制备方法

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107556012A (zh) * 2017-08-28 2018-01-09 郑州市立新实业有限公司 一种嵌扣式防弹陶瓷片及其制备方法
WO2023221297A1 (zh) * 2022-05-19 2023-11-23 浙江立泰复合材料股份有限公司 一种抗多发弹陶瓷的制备方法及防弹插板
CN114993113A (zh) * 2022-06-22 2022-09-02 浙江富研新型材料有限公司 防弹用多晶钻石烧结体及其应用

Similar Documents

Publication Publication Date Title
US8628857B2 (en) Ballistic plate and method of fabrication thereof
CN101967059B (zh) 一种碳化硅防弹陶瓷的制备方法
CN106380199A (zh) 纤维增加碳化硅陶瓷防弹板的制作方法
CN103508734B (zh) 一种防弹碳化硼/碳化硅复合陶瓷制备方法
CN108516831A (zh) 一种防弹陶瓷整板的制备方法
US10794665B1 (en) Ballistics resistant hard plate armor
CN112592184B (zh) 一种超轻质碳化硼防弹陶瓷及其制备方法和应用
CN108467272A (zh) 一种碳化硼/碳化硅层状复合陶瓷材料的制备方法
US20060141237A1 (en) Metal-ceramic materials
CN114933479B (zh) 一种抗多发弹陶瓷的制备方法及防弹插板
CN110156486A (zh) 高韧性层状防弹陶瓷材料及流延法结合热压烧结法的制备方法
CN103073318A (zh) 一种碳化硼/碳纤维复合陶瓷及其制备方法
CN107990783A (zh) 一种球形体内置复合结构防弹装甲材料及其制备方法
CN111805983A (zh) 一种防弹单元及其制造工艺
Reddy et al. Ceramic composite armour for ballistic protection
CN108151588A (zh) 一种蜂窝阻隔结构防弹插板及其制备方法
CN110041076B (zh) 一种大厚度轻质叠层装甲陶瓷及其制备方法
US20120318131A1 (en) Polymer ceramic composite
CN108859357A (zh) 一种可防御12.7mm穿甲燃烧弹陶瓷基复合材料
CN108395251B (zh) 一种整体式碳化硅木质陶瓷防弹面板的制备方法
CN106631028A (zh) 一种金属复合镁碳化硅防弹陶瓷的制备工艺
CN108794015A (zh) 一种碳化硅、二硼化钛复合陶瓷材料的制作方法及其应用
CN114216372A (zh) 一种石墨烯复合防弹板及其制备方法
CN113932655A (zh) 一种碳化硼陶瓷装甲结构及其设计方法
CN107687792A (zh) 一种大厚度碳化硼‑铝合金复合板

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
RJ01 Rejection of invention patent application after publication
RJ01 Rejection of invention patent application after publication

Application publication date: 20170208