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<正>1、复合板的分类(1)按复合板基底材料分类①石材铝蜂窝复合板。复合板基底材料由铝蜂窝生产出来的石材复合板。石材铝蜂窝复合板以其重量轻、强度高、性能卓越,节约资源,这些年越来越多地被大量应用在建筑物装饰上,也受到越来越多的设计公司重视。所谓铝蜂窝是以蜂窝结构为芯层的蜂窝夹层板,其灵感来源于天然六边形蜂窝。一张20mm的铝蜂窝板除了上下两层是0.8~1.2mm的铝板板外,中间18mm是如蜂窝状的极薄的铝箔(铝箔的厚度大概 相似文献
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本文对建筑幕墙用铝蜂窝复合板芯材参数设计问题进行掌探讨。介绍了铝蜂窝芯的最小厚度估算式、表观密度表达式,推导出了铝蜂窝格边长与壁厚的关系式,并举倒应用一些算式及曲线图初。步设计铝蜂窝芯材诸参数;最后对芯材参数的进一步设计及与之相关的面板厚度设计问题做强。本文对将要发布的《建筑幕墙用铝蜂窝复合板》行业标准的执行,对幕墙用铝蜂窝板的设计具有一定参考价值。 相似文献
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铝蜂窝复合板在建筑外墙施工中使用广泛,本文通过对复合板施工技术要求的阐述,提出复合板施工工艺的主要内容,为相关施工提供思路. 相似文献
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目前,金属幕墙使用的板主要有三类,即纯铝板、铝复合板和蜂窝芯板.其中,铝复合板由于具有重量轻、色差小、平面性好、加工成型方便、以及价格相对较为便宜等诸多优点,因而大受欢迎,成为金属幕墙中使用最为广泛的一种.作为较为新颖的建筑装饰材料,很多人还不太了解铝复合板的加工和安装方法,下面就作简单的介绍.现在市面上铝复合板的品种较多,质量品质各异,但加工方法基本相同,这里就以日本三菱化学公司的雅保丽固(Aloolic)铝复合板为例. 相似文献
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铝装饰板是新型、高档内外墙装饰材料,包括单层彩色铝板、铝塑复合板、铝蜂窝板和铝保温复合板等几种。从高档建筑物的幕墙装饰来看,国内目前以玻璃幕墙、装饰石材幕墙和铝装饰板幕墙为主。其中铝装饰板后来居上,是目前发展最快的幕墙装饰材料。1 企业的基本情况 我国铝装饰板的市场70%以上为铝塑板所占,单层铝板约占20%,蜂窝板和保温板不到10%。由此可看出,铝塑板是铝装饰板行业的主力 相似文献
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一、简介 铝蜂窝夹层石材(以下简称复合板)是一种大约4~8mm厚的天然石材薄板(大理石、花岗石、合成石)用环氧树脂胶接于轻质铝蜂窝/玻璃纤维复合夹层结构基板上而成的一种复合材料板材。其特点在于面层为天然石或合成石薄板,用以表现石材的装饰效果,而基板采用玻璃钢板与铝蜂窝的复合结构,用以 相似文献
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浙江温州麦克辛石业有限公司攻克了超薄型石材复合板的核心技术,建成了目前国际领先的大型超薄石材蜂窝复合板生产流水线与超薄型石材大板后续整理生产线,主要生产超薄型石材大板、石材蜂窝复合板和超薄石材透光板3大系列产品,年生产能力达20万m2。这些产品通过众多重大工程的应用,得到良好的赞誉。超薄型石材大板以铝蜂窝和塑料蜂窝为基料,以1.0~3.5mm厚的天然石材与6~50mm厚的蜂窝材料复合而成,每平方米仅10~11kg,是传统干挂石材(75kg)的1/7。产品抗压强度为传统干挂石材的3~5倍,具有平整度高、抗震性强、防火、隔音和隔热效果好等特… 相似文献
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石材铝蜂窝复合板质量轻、强度高、刚度好,与其他吊顶装饰材料相比具有良好的保温、隔热性能和抗冲击性能,从而广泛地应用于室内装饰工程。天津美术馆工程采用具有创新的挂搭式施工方法,并详细介绍了关键施工技术和施工质量检查标准。结果表明:该施工方法方便快捷、安全可靠。 相似文献
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研究了在4点弯曲工况下,铝泡沫核心/热塑性复合材料面层构成的夹芯板的核心厚度对变形机制的影响。通过全过程应力分析和观察,得出不同核厚下一系列的失效机制。各个样本厚度对应不同失效区域均可观察到高应变集中。相对薄的样本表面出现折皱和破裂现象,一些核也会碎裂,相对厚的样本的失效取决于核的凹陷。增加表面厚度可以避免核的凹陷,否则,可以观察到关键的核被剪碎。 相似文献
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For the classic thin-walled energy absorber, the energy dissipation during a collision is concentrated over relatively narrow zones. This means that a great deal of materials of the columns do not participate in the plastic deformation or not enter into the large plastic deformation stage. To expand the plastic deformation zones and improve the energy absorption efficiency, a new type of kagome honeycomb sandwich bitubal circular column is presented in this paper. This innovative impact energy absorber is made of two circular aluminum tubes filled with core shaped as a large-cell kagome lattice. The interaction effect, deformation mode and energy absorption characteristics of the composite structure are investigated numerically. Observing the collapsing process, it is found that the kagome lattices buckle first, which triggers the outer and inner skin tubes to fold locally. This behavior increases the plastic deformation areas. Moreover, the presence of the outer and inner tubes strengthens the buckling capacity of kagome cell. Furthermore, the folded tube walls intrude into the gap of the honeycomb cell, which further retards the collapse of the honeycomb cell. So the interaction effects between the honeycomb and column walls greatly improve the energy absorption efficiency. In addition, the effects of geometrical parameters of the kagome honeycomb on the structural crashworthiness are studied. It is found that the cell wall thickness and cell distribution (cell number in the circumferential direction) have distinct effects on the specific energy absorption. Besides, we also studied the foam-filled column with the same foam density as the kagome honeycomb and compared it with the kagome sandwich structure. It is found that the kagome sandwich column has higher mean crash force and better energy absorption characteristics. 相似文献
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Aluminum sandwich construction has been recognized as a promising concept for structural design of lightweight transportation systems such as aircraft, high-speed trains and fast ships. The aim of the present study is to investigate the strength characteristics of aluminum sandwich panels with aluminum honeycomb core theoretically and experimentally. A series of strength tests are carried out on aluminum honeycomb-cored sandwich panel specimen in three point bending, axial compression and lateral crushing loads. Simplified theories are applied to analyze bending deformation, buckling/ultimate strength and crushing strength of honeycomb sandwich panels subject to the corresponding load component. The structural failure characteristics of aluminum sandwich panels are discussed. The test data developed are documented. 相似文献
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《Thin》2014
The full potential of carbon-fiber and aluminum-honeycomb sandwich panels and structures has been limited by the huge property mismatch between the high-stiffness carbon fiber and low-stiffness aluminum honeycomb. In this study, an orthogrid structure was added into the sandwich structure to raise the stiffness of soft honeycomb and therefore reduce the interfacial mismatch. The core then became an aluminum orthogrid structure filled with aluminum-honeycomb blocks. Three point bending tests were conducted to compare carbon fiber sandwiches with different types of core: (1) aluminum-honeycomb core; (2) aluminum-plate orthogrid core; and (3) aluminum-plate orthogrid core filled by aluminum-honeycomb blocks. The honeycomb filled orthogrid core sandwich was a bit heavier than the honeycomb or grid sandwich, but the critical load, specific strength and energy absorption ability were all improved. The results indicated that the honeycomb filled orthogrid core sandwich with carbon fiber face sheet could provide improved structural properties for thin walled engineering structures. 相似文献
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《Thin》2014
Crashworthiness parameters of aluminum hexagonal honeycomb structures under impact loads are investigated by using finite element methods and conducting experiments. To validate the finite element models, numerical results are compared with experimental measurements and theoretical results reported in literature. In numerical simulations of honeycomb structures, out-of-plane loads are considered while the aluminum foil thickness, cell side size, cell expanding angle, impact velocity and mass are varying, and dynamic behavior and crashworthiness parameters are examined. It is observed that there are good agreements between numerical, experimental and theoretical results. Numerical simulations predict that crashworthiness parameters depend on cell specification and foil thickness of the honeycomb structure and are independent of impact mass and velocity. 相似文献