CN105346164A - 一种高强航空复合金属板 - Google Patents

一种高强航空复合金属板 Download PDF

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Publication number
CN105346164A
CN105346164A CN201510868010.1A CN201510868010A CN105346164A CN 105346164 A CN105346164 A CN 105346164A CN 201510868010 A CN201510868010 A CN 201510868010A CN 105346164 A CN105346164 A CN 105346164A
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China
Prior art keywords
metal
thickness
carbon cloth
plate
core board
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CN201510868010.1A
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English (en)
Inventor
李上
鲁鹏
刘波林
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China Aero Polytechnology Establishment
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China Aero Polytechnology Establishment
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Priority to CN201510868010.1A priority Critical patent/CN105346164A/zh
Publication of CN105346164A publication Critical patent/CN105346164A/zh
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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
    • B32B15/00—Layered products comprising a layer of metal
    • B32B15/04—Layered products comprising a layer of metal comprising metal 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
    • B32B15/00—Layered products comprising a layer of metal
    • B32B15/14—Layered products comprising a layer of metal next to a fibrous or filamentary layer
    • 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
    • B32B15/00—Layered products comprising a layer of metal
    • B32B15/18—Layered products comprising a layer of metal comprising iron or steel
    • 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
    • B32B33/00—Layered 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
    • 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
    • B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
    • B32B2262/10—Inorganic fibres
    • B32B2262/106—Carbon fibres, e.g. graphite 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
    • B32B2307/50—Properties of the layers or laminate having particular mechanical properties
    • 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
    • B32B2605/00—Vehicles
    • B32B2605/18—Aircraft

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Ceramic Engineering (AREA)
  • Laminated Bodies (AREA)

Abstract

本发明涉及一种高强航空复合金属板，包括金属面板(1)、金属芯板(3)、金属背板(2)和碳纤维布(4)；所述金属面板(1)、金属芯板(3)、金属背板(2)之间铺设有碳纤维布(4)；所述金属面板(1)的材质为碳钢；所述金属芯板(3)的材质为镁合金；所述金属背板(2)的材质为铝合金；所述金属面板(1)的厚度为1～1.5mm，所述金属芯板(3)厚度为1.5～2mm，所述金属背板(2)的厚度为1.5～2mm；所述碳纤维布(4)的厚度为1～1.5mm。本发明是一种制作简单、造价便宜，强度高的一种高强航空复合金属板。

Description

一种高强航空复合金属板
技术领域
本发明涉及一种航空复合金属板，具体地说，是一种高强航空复合金属板。
背景技术
金属板具有高强度、高刚度，加工性好的特点，在航空制造业应用最广泛的材料。但是目前，航空用金属板存在金属板重量与金属板强度之间的矛盾，若想获得强度高的胶合板，往往会导致航空金属板重量增加。在满足容积与重量要求情况下，如何提高航空用金属板的强度成为了亟待解决的问题。
碳纤维布是一种单向碳纤维加固产品，通常采用12K碳纤维丝织造。碳纤维布强度高，密度小，厚度薄，基本不增加加固构件自重及截面尺寸，并且具有高耐久性，由于不会生锈，非常适合高酸、碱、盐及大气腐蚀环境中使用。
利用热可塑性树脂或热固化性树脂，可将碳纤维布与金属板加工成为一体化结构的复合金属板。该复合金属板能维持表面的金属材料特征而整体重量变轻，并且具有相同或更高之刚性强度。
发明内容
本发明所要解决的技术问题是提供一种高强航空复合金属板。
一种高强航空复合金属板，包括金属面板、金属芯板、金属背板和碳纤维布；
所述金属面板、金属芯板、金属背板之间铺设有碳纤维布；
所述金属面板的材质为碳钢；
所述金属芯板的材质为镁合金；
所述金属背板的材质为铝合金；
所述金属面板的厚度为1～1.5mm，所述金属芯板厚度为1.5～2mm，所述金属背板的厚度为1.5～2mm；
所述碳纤维布的厚度为1～1.5mm。
所述碳纤维布为缎纹或网纹。
本发明的有益效果是：保留航空用金属板原有的制作简单、造价便宜的优势，在金属板中加入碳纤维布，在充分满足使用要求情况下，获得强度更高、性能更好的航空复合金属板。
附图说明
图1是本发明结构示意图。
具体实施方式
通过下面给出的本发明的具体实施例可以进一步清楚的理解本发明，但下述实施例并不是对本发明的限定。
实施例1：
参见图1，金属面板1的材质为碳钢；金属芯板3的材质为镁合金；金属背板的材质为铝合金；金属面板1、金属芯板3、金属背板2之间铺设有碳纤维布4；碳纤维布4缎纹；金属面板1的厚度为1mm，金属芯板3厚度为1.5mm，金属背板2的厚度为1.5mm；碳纤维布4的厚度为1mm。
实施例2：
参见图1，金属面板1的材质为碳钢；金属芯板3的材质为镁合金；金属背板的材质为铝合金；金属面板1、金属芯板3、金属背板2之间铺设有碳纤维布4；碳纤维布4网纹；金属面板1的厚度为1.5mm，金属芯板3厚度为2mm，金属背板2的厚度为2mm；碳纤维布4的厚度为1.5mm。

Claims (2)

1.一种高强航空复合金属板，包括金属面板(1)、金属芯板(3)、金属背板(2)和碳纤维布(4)，其特征在于：所述金属面板(1)、金属芯板(3)、金属背板(2)之间铺设有碳纤维布(4)；所述金属面板(1)的材质为碳钢；所述金属芯板(3)的材质为镁合金；所述金属背板(2)的材质为铝合金；所述金属面板(1)的厚度为1～1.5mm，所述金属芯板(3)厚度为1.5～2mm，所述金属背板(2)的厚度为1.5～2mm；所述碳纤维布(4)的厚度为1～1.5mm。
2.根据权利要求1所述的高强航空复合金属板，其特征在于：所述碳纤维布(4)为缎纹或网纹。
CN201510868010.1A 2015-12-01 2015-12-01 一种高强航空复合金属板 Pending CN105346164A (zh)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201510868010.1A CN105346164A (zh) 2015-12-01 2015-12-01 一种高强航空复合金属板

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
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Publications (1)

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109130384A (zh) * 2018-08-23 2019-01-04 同济大学 用于汽车底盘的碳纤维增强镁铝层状复合板及其制备方法
CN109226959A (zh) * 2018-10-26 2019-01-18 同济大学 一种纤维增强金属基复合板材及其预处理方法

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109130384A (zh) * 2018-08-23 2019-01-04 同济大学 用于汽车底盘的碳纤维增强镁铝层状复合板及其制备方法
CN109226959A (zh) * 2018-10-26 2019-01-18 同济大学 一种纤维增强金属基复合板材及其预处理方法
CN109226959B (zh) * 2018-10-26 2020-08-25 同济大学 一种纤维增强金属基复合板材及其预处理方法

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Application publication date: 20160224