CN111086286A - 一种轻质耐高温防雷击复合板材及成型方法 - Google Patents

一种轻质耐高温防雷击复合板材及成型方法 Download PDF

Info

Publication number
CN111086286A
CN111086286A CN201911348038.7A CN201911348038A CN111086286A CN 111086286 A CN111086286 A CN 111086286A CN 201911348038 A CN201911348038 A CN 201911348038A CN 111086286 A CN111086286 A CN 111086286A
Authority
CN
China
Prior art keywords
lightning
temperature
composite board
light high
resistant
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
CN201911348038.7A
Other languages
English (en)
Inventor
高丽红
钟振全
党婧
贺辉
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.)
Xian Aircraft Design and Research Institute of AVIC
Original Assignee
Xian Aircraft Design and Research Institute of AVIC
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 Xian Aircraft Design and Research Institute of AVIC filed Critical Xian Aircraft Design and Research Institute of AVIC
Priority to CN201911348038.7A priority Critical patent/CN111086286A/zh
Publication of CN111086286A publication Critical patent/CN111086286A/zh
Pending legal-status Critical Current

Links

Images

Classifications

    • 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
    • B32B5/00Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
    • B32B5/02Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by structural features of a fibrous or filamentary layer
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28Shaping operations therefor
    • B29C70/30Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
    • B29C70/34Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core and shaping or impregnating by compression, i.e. combined with compressing after the lay-up operation
    • 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
    • B32B33/00Layered products characterised by particular properties or particular surface features, e.g. particular surface coatings; Layered products designed for particular purposes not covered by another single class
    • 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
    • B32B37/00Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
    • B32B37/06Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the heating method
    • 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
    • B32B37/00Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
    • B32B37/10Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the pressing technique, e.g. using action of vacuum or fluid pressure
    • 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
    • B32B5/00Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
    • B32B5/22Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed
    • B32B5/24Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer
    • B32B5/26Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer another layer next to it also being fibrous or filamentary
    • 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
    • B32B7/00Layered 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
    • B32B7/04Interconnection of layers
    • B32B7/08Interconnection of layers by mechanical means
    • 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
    • B32B2250/00Layers arrangement
    • B32B2250/055 or more layers
    • 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
    • B32B2250/00Layers arrangement
    • B32B2250/40Symmetrical or sandwich layers, e.g. ABA, ABCBA, ABCCBA
    • 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
    • B32B2262/103Metal 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
    • B32B2262/106Carbon fibres, e.g. graphite 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
    • B32B2307/70Other properties
    • 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
    • B32B2307/70Other properties
    • B32B2307/752Corrosion inhibitor

Abstract

本发明公开了一种轻质耐高温防雷击复合板材及成型方法,包括两层上面板和两层下面板按照[(+45,-45)/(0,90)]S的铺层比例进行均衡对称顺序铺设,所述的最外层的上面板及最外层的下面板上均设置有一层防雷击铜网胶膜,所述的防雷击铜网胶膜由铜网与胶膜复合而成,本发明成型会后的复合板材重量轻,雷击防护性好,耐蚀性与工艺性优良,满足了航空产品的需求。

Description

一种轻质耐高温防雷击复合板材及成型方法
技术领域
本发明属于材料技术领域,尤其涉及一种轻质耐高温防雷击复合板材及成型方法。
背景技术
轻质耐高温防雷击板材对实现材料的多重功能和减轻结构重量具有明显的效果。目前,国内建筑行业广泛使用了金属防护网、火焰喷涂铝组成的防雷击板材,其重量和厚度不适用其对减重、结构尺寸的需求。国内航空领域广泛使用了碳纤维复合材料与金属网、胶膜复合成的板材或在制件表面采用火焰喷涂铝等雷电防护方式,其缺点是:一、重量大,成本高。金属铝网和胶膜的密度较大,火焰喷涂铝防护层厚度较大,导致结构重量增加较多;加之混炼工艺复杂;加温硫化需专用设备等问题,导致成本高。二、工艺复杂,易变形。需手工分别覆铺金属网和胶膜,铺设绝缘玻璃布层、火焰喷涂铝、涂封孔剂、涂地漆面漆,工序复杂,生产周期长,而且无自粘性、施工困难,且存在金属网容易起皱、变形、甚至断开等问题。三、耐蚀性与防雷击性差。因需表面处理,结合力不好,还要涂胶,易腐蚀,雷击防护效果较差。
发明内容
本发明的目的:提出一种重量轻、雷击防护性好、耐腐性与工艺性优良的轻质耐高温防雷击复合板材及成型方法,以满足航空产品的需求。
本发明的技术方案:
一种轻质耐高温防雷击复合板材,包括两层上面板和两层下面板按照[(+45,-45)/(0,90)]S的铺层比例进行均衡对称顺序铺设,所述的最外层的上面板及最外层的下面板上均设置有一层防雷击铜网胶膜,所述的防雷击铜网胶膜由铜网与胶膜复合而成。
所述的上面板和下面板均为苯并噁嗪碳纤维复合材料板。
所述单层上面板和单层下面板厚度均为0.300±0.01mm。
所述的防雷击铜网胶膜厚度为0.152±0.01mm。
所述苯并噁嗪碳纤维复合材料板的密度为1.52g/cm3
所述的防雷击铜网胶膜密度为0.97g/cm3
所述的防雷击铜网胶膜电阻率为1.75×10-8Ω·m。
轻质耐高温防雷击复合板材的成型方法:在最外层的上面板及最外层的下面板上铺置一层厚度为0.152mm±0.01mm的防雷击铜网胶膜,放入模具中,在 0.62MPa±0.05MPa压力作用下,升温至185℃±5℃,并保温180min~240min,最后在60℃下卸压,制成所述的轻质耐高温防雷击复合板材。
本发明的有益效果:本发明提出的一种轻质耐高温防雷击复合板材及成型方法,成型会后的复合板材重量轻,雷击防护性好,耐蚀性与工艺性优良,满足了航空产品的需求。
附图说明
图1是本发明铺层方式示意图;
图2是防雷击铜网胶膜铺放示意图;
图3是成型后的轻质耐高温防雷击复合板材示意图;
图4为模拟雷击试验装置;
图5为模拟雷击试验装置试验电极示意图;
其中,1、上面板,2、下面板,3、防雷击铜网胶膜。
具体实施方式
下面结合附图对本发明作进一步的介绍,本发明所述的一种轻质耐高温防雷击复合板材,包括两层上面板1和两层下面板2按照[(+45,-45)/(0,90)]S的铺层比例进行均衡对称顺序铺设,所述的最外层的上面板1及最外层的下面板2上均设置有一层防雷击铜网胶膜3,所述的防雷击铜网胶膜3由铜网与胶膜复合而成。
所述的上面板1和下面板2均为苯并噁嗪碳纤维复合材料板,苯并噁嗪碳纤维复合材料在力学性能优异的基础上,兼具良好的防火性能,成为新型结构功能一体化材料。
作为一种新型的热固性树脂基复合材料,相比传统的热固性环氧树脂类复合材料,更低的固化收缩和放热性(固化收缩<1%),可进一步提高试板的尺寸稳定性;同时具有更高的耐湿热性能,优良的FST(烟、火、毒)性能,可用于飞机耐高温、防火部位,如短舱、发动机整流罩等,并可室温储存(>6个月) 和输运(盒装或袋装),有利于进一步降低成本。
所述单层的上面板1和单层下面板2厚度均为0.300±0.01mm。
所述的防雷击铜网胶膜3厚度为0.152±0.01mm,密度为0.97g/cm3,电阻率为1.75×10-8Ω·m。
所述苯并噁嗪碳纤维复合材料板的密度为1.52g/cm3
轻质耐高温防雷击复合板材的成型方法:在最外层的上面板1及最外层的下面板2上铺置一层厚度为0.152mm±0.01mm的防雷击铜网胶膜3,放入模具中,在0.62MPa±0.05MPa压力作用下,升温至185℃±5℃,并保温180min~240min,最后在60℃下卸压,制成所述的轻质耐高温防雷击复合板材。
本发明材料结构将各向异性材料(上面板1及下面板2)和各向同性材料(防雷击铜网胶膜3)相结合,复合成一种多层材料结构,充分发挥两种材料各自的优势并弥补各自材料的缺点,实现具备轻量化、力学性能优异、耐腐蚀性好的一种多层材料结构。具体是将这种多层材料结构划分为两大部分,第一部分是由各向异性的LOCTITE BZ9704 5HS285-40AERO树脂基复合材料,具体是苯并噁嗪碳纤维复合材料板,密度为1.52g/cm3,按照[(+45,-45)/(0,90)]S均衡对称顺序铺4层构成,以最大限度的保留LOCTITE BZ9704 5HS285-40AERO材料结构的强度和刚度特性,获得最佳的力学性能,第二部分是由一种具有防雷击功能、密度为0.97g/cm3,电阻率为1.75×10-8Ω·m的LOCTITE EA 9837.1 030-040 AERO各向同性、铜网表面膜构成。第一部分LOCTITE BZ9704 5HS285-40 AERO 层板与第二部分LOCTITE EA 9837.1 030-040 AERO通过热压共固化成5层的整体结构板材。
按照图4的模拟雷击试验装置的布置形式,验证成型后的复合板材的防雷击性能,
a)轻质耐高温防雷击复合板材(试验件)四周上下两面,用金属压条夹紧固定,金属压条连接发生器回线;
b)试验电极放置于试验件中心上方。
通过对轻质耐高温防雷击复合板材(试验件)进行模拟雷击试验,大电流直接效应试验,对试验件形成雷击损伤进行测试,由冲击电流发生器(设备型号: LCG200S设备参数200kA)产生电流A和电流D,电流分量A为首次回击电流,其幅值200kA 10%,上升时间不超过50,作用积分2×106A2s±20%,试验时选用阻尼振荡波形。电流分量D为后续回击电流,其幅值为100kA±10%,上升时间不超过25μs,作用积分0.25×106A2s±20%,试验时选用阻尼振荡波形。
试验电极:
试验电极喷射型电极,如图5所示,电极距离放电位置不小于50mm,在试验电极与放电位置之间搭接一根直径不超过0.1mm的细铜丝。
进过模拟雷击试验后,苯并噁嗪碳纤维复合材料板的性能如下表所示。
Figure RE-GDA0002403878600000051
实施例1与同样厚度的金属网相比,雷击防护效果提高了约20%。

Claims (8)

1.一种轻质耐高温防雷击复合板材,其特征在于:包括两层上面板(1)和两层下面板(2)按照[(+45,-45)/(0,90)]S的铺层比例进行均衡对称顺序铺设,所述的最外层的上面板(1)及最外层的下面板(2)上均设置有一层防雷击铜网胶膜(3),所述的防雷击铜网胶膜(3)由铜网与胶膜复合而成。
2.根据权利要求1所述的一种轻质耐高温防雷击复合板材,其特征在于:所述的上面板(1)和下面板(2)均为苯并噁嗪碳纤维复合材料板。
3.根据权利要求2所述的一种轻质耐高温防雷击复合板材,其特征在于:所述苯并噁嗪碳纤维复合材料板的密度为1.52g/cm3
4.根据权利要求1所述的一种轻质耐高温防雷击复合板材,其特征在于:所述单层上面板和单层下面板厚度均为0.300±0.01mm。
5.根据权利要求1所述的一种轻质耐高温防雷击复合板材,其特征在于:所述的防雷击铜网胶膜(3)厚度为0.152±0.01mm。
6.根据权利要求1所述的一种轻质耐高温防雷击复合板材,其特征在于:所述的防雷击铜网胶膜(3)密度为0.97g/cm3
7.根据权利要求1所述的一种轻质耐高温防雷击复合板材,其特征在于:所述的防雷击铜网胶膜(3)电阻率为1.75×10-8Ω·m。
8.如权利要求1所述的轻质耐高温防雷击复合板材的成型方法,其特征在于:在最外层的上面板(1)及最外层的下面板(2)上铺置一层厚度为0.152mm±0.01mm的防雷击铜网胶膜(3),放入模具中,在0.62MPa±0.05MPa压力作用下,升温至185℃±5℃,并保温180min~240min,最后在60℃下卸压,制成所述的轻质耐高温防雷击复合板材。
CN201911348038.7A 2019-12-24 2019-12-24 一种轻质耐高温防雷击复合板材及成型方法 Pending CN111086286A (zh)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201911348038.7A CN111086286A (zh) 2019-12-24 2019-12-24 一种轻质耐高温防雷击复合板材及成型方法

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201911348038.7A CN111086286A (zh) 2019-12-24 2019-12-24 一种轻质耐高温防雷击复合板材及成型方法

Publications (1)

Publication Number Publication Date
CN111086286A true CN111086286A (zh) 2020-05-01

Family

ID=70396724

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201911348038.7A Pending CN111086286A (zh) 2019-12-24 2019-12-24 一种轻质耐高温防雷击复合板材及成型方法

Country Status (1)

Country Link
CN (1) CN111086286A (zh)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112706427A (zh) * 2020-12-08 2021-04-27 同济大学 雷击防护、电磁屏蔽及承载一体化航空材料及其制备方法
CN113061789A (zh) * 2021-02-02 2021-07-02 重庆材料研究院有限公司 轻质超宽防雷击用含铜铝网及其制备方法
CN113944050A (zh) * 2021-12-21 2022-01-18 宁波诺丁汉新材料研究院有限公司 一种轻质导电复合材料及其制成的防雷击风机叶片

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102454035A (zh) * 2010-10-29 2012-05-16 威海光威复合材料有限公司 0度及90度角双轴向碳纤维经编布
CN102454034A (zh) * 2010-10-29 2012-05-16 威海光威复合材料有限公司 ±45度角双轴向碳纤维经编布
CN202357543U (zh) * 2011-08-15 2012-08-01 中国航空工业集团公司西安飞机设计研究所 一种轻质多层结构板材
CN203032022U (zh) * 2012-11-30 2013-07-03 南京航空航天大学 一种轻质耐高温碳纤维金属混杂层板
CN107719394A (zh) * 2016-08-10 2018-02-23 株洲联诚集团有限责任公司 纤维增强泡沫夹芯结构复合材料机车驾驶舱及其制备方法
CN107825810A (zh) * 2017-09-04 2018-03-23 中航复材(北京)科技有限公司 一种轻质雷击防护表面层及其制备和使用方法
CN208085162U (zh) * 2017-12-01 2018-11-13 中国直升机设计研究所 一种具有闪电防护和电磁屏蔽功能的直升机蒙皮

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102454035A (zh) * 2010-10-29 2012-05-16 威海光威复合材料有限公司 0度及90度角双轴向碳纤维经编布
CN102454034A (zh) * 2010-10-29 2012-05-16 威海光威复合材料有限公司 ±45度角双轴向碳纤维经编布
CN202357543U (zh) * 2011-08-15 2012-08-01 中国航空工业集团公司西安飞机设计研究所 一种轻质多层结构板材
CN203032022U (zh) * 2012-11-30 2013-07-03 南京航空航天大学 一种轻质耐高温碳纤维金属混杂层板
CN107719394A (zh) * 2016-08-10 2018-02-23 株洲联诚集团有限责任公司 纤维增强泡沫夹芯结构复合材料机车驾驶舱及其制备方法
CN107825810A (zh) * 2017-09-04 2018-03-23 中航复材(北京)科技有限公司 一种轻质雷击防护表面层及其制备和使用方法
CN208085162U (zh) * 2017-12-01 2018-11-13 中国直升机设计研究所 一种具有闪电防护和电磁屏蔽功能的直升机蒙皮

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112706427A (zh) * 2020-12-08 2021-04-27 同济大学 雷击防护、电磁屏蔽及承载一体化航空材料及其制备方法
CN113061789A (zh) * 2021-02-02 2021-07-02 重庆材料研究院有限公司 轻质超宽防雷击用含铜铝网及其制备方法
CN113061789B (zh) * 2021-02-02 2022-03-08 重庆材料研究院有限公司 轻质超宽防雷击用含铜铝网及其制备方法
CN113944050A (zh) * 2021-12-21 2022-01-18 宁波诺丁汉新材料研究院有限公司 一种轻质导电复合材料及其制成的防雷击风机叶片
CN113944050B (zh) * 2021-12-21 2022-04-12 宁波诺丁汉新材料研究院有限公司 一种轻质导电复合材料及其制成的防雷击风机叶片

Similar Documents

Publication Publication Date Title
CN111086286A (zh) 一种轻质耐高温防雷击复合板材及成型方法
CN109291575B (zh) 一种表面防护型导电复合材料及其制备方法
CN104647823B (zh) 一种抗冲击吸能材料及其制备方法
CN102014590B (zh) 多层印制电路板的生产方法及该多层印制电路板
CN103722807A (zh) 一种高导热高耐压的铝基覆铜板及其制备方法
CN108274829A (zh) 一种具有雷达隐身功能的轻量化的屏蔽方舱壁板及其制备方法
CN107498952B (zh) 间位芳纶纤维/玻璃纤维纸基覆铜箔层压板及其制造方法
US3179531A (en) Method of coating a laminated plastic structure
CN109747257A (zh) 陶瓷涂装复合板及其制备方法
CN105774095A (zh) 具有电磁屏蔽功能的复合材料面板
CN102009514B (zh) 多层板的制作方法
CN202029463U (zh) 一种低热阻高绝缘金属基覆铜板
CN110295408B (zh) 一种芳纶1313网状纤维及其制备方法、芳纶环氧树脂胶及其制备方法
CN205946346U (zh) 一种高散热性能的多层电池保护电路板
CN111688232B (zh) 一种碳纳米管/碳纤维复合材料及其制备方法和应用
CN110757917B (zh) 一种桉木单板贴面木基复合板材及其制备方法
CN102529222B (zh) 一种低热阻高绝缘金属基覆铜板及其制备方法
CN113696567A (zh) 耐高温宽频吸波/承载复合材料及其制备方法
CN108162431B (zh) 一种连续玻璃纤维织物增强聚苯硫醚复合材料及制备方法
CN112706427A (zh) 雷击防护、电磁屏蔽及承载一体化航空材料及其制备方法
RU2317210C1 (ru) Способ изготовления многослойной панели
CN201272306Y (zh) 旅客列车内装复合装饰材料板
CN209336213U (zh) 一种多层结构铝基复合板
CN110588087B (zh) 填充mre夹层的纤维金属混杂复合材料及其制备方法
CN212005143U (zh) 高强度超厚型补强板

Legal Events

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

Application publication date: 20200501

RJ01 Rejection of invention patent application after publication