CN117141085A - 一种耐候无反射多层复合多功能透明防弹材料及工艺 - Google Patents
一种耐候无反射多层复合多功能透明防弹材料及工艺 Download PDFInfo
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Abstract
本发明公开了一种耐候无反射多层复合多功能透明防弹材料及工艺,包括基础材料预加步骤、复合加工步骤、抽真空步骤、高温高压步骤、降温静停步骤;所述基础材料预加步骤是加入镀膜层、若干层粘结增强膜材料和若干层玻璃材料;本发明是以透明无反射或低反射的防火特种玻璃材料,经过复合加工、抽真空、高温高压及降温静停步骤,使得多层透明材料可以高强度粘合成一种无反射或低反射防火多层复合透明防弹材料的整体材料;适合军用、民用的各种车辆和舰船的驾驶室、透视窗;以及各种特殊防弹功能要求的军、民用建筑物,可以减少被攻击伤害,更有效保护使用者的生命安全。
Description
技术领域
本发明涉及防弹材料及制备工艺技术领域,具体为一种耐候无反射多层复合多功能透明防弹材料及工艺。
背景技术
目前市场上军用/民用的防弹玻璃材料,只是单一的防弹功能,不能适应现代战争军事技术的发展,特别是目前狙击手、无人机已经开始大量用于战场,急需一种无反射(低反射)功能的多层复合透明防弹材料(含中空);
普通的防弹玻璃产品,虽然具有一定的防止枪弹射击的功能,但由于通常这样的防弹玻璃反射率比较高,很容易被狙击手或无人机发现目标,非常容易受到攻击和严重伤害。
发明内容
本发明的目的在于提供一种耐候无反射多层复合多功能透明防弹材料及工艺,以解决上述背景技术中提出现有市场中普通的防弹玻璃产品仅具备有防弹的功能,但是防弹玻璃反射率高,容易被狙击手或无人机发现的问题。
为实现上述目的,本发明提供如下技术方案:一种耐候无反射多层复合多功能透明防弹材料及工艺,包括基础材料预加步骤、复合加工步骤、抽真空步骤、高温高压步骤、降温静停步骤;
所述基础材料预加步骤是加入镀膜层、若干层粘结增强膜材料和若干层玻璃材料;
所述复合加工步骤将基础材料复合加工成多层复合材料;
所述抽真空步骤是将复合加工步骤后的多层复合材料放入至抽真空软性容器内部进行抽真空操作;
所述高温高压步骤是将多层复合材料抽真空组件放入至高压釜的内部,进行升温增压处理,其温度首先是室温经过1~2h升温至80~90度,再经过3h升温至130~150度;其中压力通过0.5~1h升至8~9atm,再经过3~4h升至12~13atm;
所述降温静停步骤是将高压釜的内部保温1~1.5h,再保压降温4~5h,然后进行常温静停处理,降压至常压,最后从抽真空软性容器内部将多层复合材料取出,既为制作完成的防弹材料成品。
优选的,所述复合加工步骤具体为将多组相同规格的玻璃材料通过粘结增强膜材料粘合在一起形成玻璃复合体,然后将玻璃复合体的顶部通过粘结增强膜材料粘结上镀膜层。
优选的,所述抽真空步骤中真空软性容器内的真空度为0.08~0.1MP。
优选的,所述多层复合材料包括镀膜层、若干层粘结增强膜材料和若干层玻璃材料。
优选的,所述镀膜层为无反射或低反射的镀膜特种玻璃。
优选的,所述粘结增强膜材料可为SGP膜或PU膜。
优选的,所述玻璃材料可为普通玻璃或特种玻璃。
与现有技术相比,本发明的有益效果是:以透明无反射或低反射的防火特种玻璃材料,经过复合加工、抽真空、高温高压及降温静停步骤,使得多层透明材料可以高强度粘合成一种无反射或低反射防火多层复合透明防弹材料的整体材料;
本新型材料兼具透明、无反射或低反射、防火、防弹功能、并且在零下60度至零上60度的环境下不分层,不开裂;
适合军用、民用的各种车辆和舰船的驾驶室、透视窗;以及各种特殊防弹功能要求的军、民用建筑物,可以减少被攻击的伤害,更有效保护人,特别是战场上军人的生命安全。
附图说明
图1为本发明的结构示意图。
图中:1、镀膜层;2、粘结增强膜材料;3、玻璃材料。
具体实施方式
下面将结合本发明实施例中的附图,对本发明实施例中的技术方案进行清楚、完整地描述,显然,所描述的实施例仅仅是本发明一部分实施例,而不是全部的实施例。基于本发明中的实施例,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,都属于本发明保护的范围。
请参阅图1,本发明提供的实施例:一种耐候无反射多层复合多功能透明防弹材料及工艺,包括基础材料预加步骤、复合加工步骤、抽真空步骤、高温高压步骤、降温静停步骤;
基础材料预加步骤是加入镀膜层、若干层粘结增强膜材料和若干层玻璃材料;
所述复合加工步骤将基础材料复合加工成多层复合材料;
复合加工步骤具体为将多组相同规格的玻璃材料3通过粘结增强膜材料2粘合在一起形成玻璃复合体,然后将玻璃复合体的顶部通过粘结增强膜材料粘结上镀膜层1,镀膜层1为无反射或低反射的镀膜特种玻璃,粘结增强膜材料2,可为SGP膜或PU膜,玻璃材料3可为普通玻璃或特种玻璃;
抽真空步骤是将复合加工步骤后的多层复合材料放入至抽真空软性容器内部进行抽真空操作,抽真空步骤中真空软性容器内的真空度为0.08~0.1MP;
高温高压步骤是将多层复合材料抽真空组件放入至高压釜的内部,进行升温增压处理,其温度首先是室温经过1~2h升温至80~90度,再经过3h升温至130~150度;其中压力通过0.5~1h升至8~9atm,再经过3~4h升至12~13atm;
降温静停步骤是将高压釜的内部保温1~1.5h,再保压降温4~5h,然后进行常温静停处理,降压至常压,最后从抽真空软性容器内部将多层复合材料取出,既为制作完成的防弹材料成品。
对于本领域技术人员而言,显然本发明不限于上述示范性实施例的细节,而且在不背离本发明的精神或基本特征的情况下,能够以其他的具体形式实现本发明。因此,无论从哪一点来看,均应将实施例看作是示范性的,而且是非限制性的,本发明的范围由所附权利要求而不是上述说明限定,因此旨在将落在权利要求的等同要件的含义和范围内的所有变化囊括在本发明内。不应将权利要求中的任何附图标记视为限制所涉及的权利要求。
Claims (7)
1.一种耐候无反射多层复合多功能透明防弹材料制备工艺,包括基础材料预加步骤、复合加工步骤、抽真空步骤、高温高压步骤、降温静停步骤,其特征在于:
所述基础材料预加步骤是加入镀膜层、若干层粘结增强膜材料和若干层玻璃材料;
所述复合加工步骤将基础材料复合加工成多层复合材料;
所述抽真空步骤是将复合加工步骤后的多层复合材料放入至抽真空软性容器内部进行抽真空操作;
所述高温高压步骤是将多层复合材料抽真空组件放入至高压釜的内部,进行升温增压处理,其温度首先是室温经过1~2h升温至80~90度,再经过3h升温至130~150度;其中压力通过0.5~1h升至8~9atm,再经过3~4h升至12~13atm;
所述降温静停步骤是将高压釜的内部保温1~1.5h,再保压降温4~5h,然后进行常温静停处理,降压至常压,最后从抽真空软性容器内部将多层复合材料取出,既为制作完成的防弹材料成品。
2.根据权利要求1所述的一种耐候无反射多层复合多功能透明防弹材料制备工艺,其特征在于:所述复合加工步骤具体为将多组相同规格的玻璃材料通过粘结增强膜材料粘合在一起形成玻璃复合体,然后将玻璃复合体的顶部通过粘结增强膜材料粘结上镀膜层。
3.根据权利要求1所述的一种耐候无反射多层复合多功能透明防弹材料制备工艺,其特征在于:所述抽真空步骤中真空软性容器内的真空度为0.08~0.1MP。
4.根据权利要求1所述的一种耐候无反射多层复合多功能透明防弹材料,其特征在于:所述多层复合材料包括镀膜层(1)、若干层粘结增强膜材料(2)和若干层玻璃材料(3)。
5.根据权利要求4所述的一种耐候无反射多层复合多功能透明防弹材料,其特征在于:所述镀膜层(1)为无反射或低反射的镀膜特种玻璃。
6.根据权利要求4所述的一种耐候无反射多层复合多功能透明防弹材料,其特征在于:所述粘结增强膜材料(2)可为SGP膜或PU膜。
7.根据权利要求4所述的一种耐候无反射多层复合多功能透明防弹材料,其特征在于:所述玻璃材料(3)可为普通玻璃或特种玻璃。
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