底盘是由碳纤维与铝蜂窝状复合材料的合金。
The chassis is constructed with a combination of carbon-fiber and aluminum honeycomb materials.
研制了一种铝蜂窝芯材拼接胶膜。
A film adhesive for bonding aluminum honeycomb core materials was develope.
铝蜂窝板，不锈钢蜂窝板，石材蜂窝板，铝塑板，铝单板。
Aluminium honeycomb panel, Sandwich board, Stainless steel honeycomb panel, Stone honeycomb panel, Aluminium-plastics composite panel, ridge plates.
铝蜂窝夹芯板由于其强度好，重量轻，正广泛用于许多制件上。
Aluminium honeycomb sandwich panel has high strength, light weight, so it is widely used in many products.
蜂窝活性炭过滤风采用通孔结构的铝蜂窝、塑料蜂窝、纸蜂窝为载体。
Beehive active carbon filter is effective through the carrier of aluminum beehive and plastic beehive and paper beehive.
在试验的基础上，讨论分析了空间辐照对碳纤维面板铝蜂窝夹层结构力学性能的影响机理。
On the basis of a lot of experimental data, the laws of particle radiation and ultraviolet ray effecting the mechanical properties are found and the effecting mechanism is analyzed.
铝蜂窝板表面采用经氟炭喷涂处理的铝合金板材，中间是符合国际航空材料标准的铝蜂窝芯。
The surface on honeycomb board of aluminum is made of aluminum alloy spraying fluorine charcoal. The center is the core of honeycomb board meeting with the international standard of aviation material.
由于大理石铝蜂窝板是由大理石对剖而成，所以可以在一定程度上解决大理石花色拼接的问题。
Marble aluminum honeycomb panel as a result is formed by the marble on the autopsy, so it can be to some extent; solve the problem of Mosaic marble designs.
试验结果表明铝蜂窝圆芯、金属橡胶圆环及涡流磁阻尼都可以用作月球着陆器的阻尼材料或阻尼方式使用。
The experimental results show that all the aluminum honeycomb core, metal rubber annulus and magnetic damping of eddy current can be used as damping materials or modes of the lunar lander.
采用结构代表胞元模型数值模拟了在不同相对密度范围的单型铝蜂窝结构在单向压缩过 程中的变形、失稳和破坏现象。
The model of representative unit cell (RUC) is used to numerically simulate the deformation, instability and collapse of single-mode aluminum honeycombs under uniaxial compression.
不同性质缺陷的最佳检测时间不同，对于铝蜂窝铝蒙皮结构复合材料蒙皮的各种脱粘缺陷，检测速度都高于每分钟两屏。
The optimal testing time for different defects is different, and the testing speed is higher than two screens per minute for all bonding defects of honey…
用红外热波技术对铝蜂窝夹层胶接结构进行检测，结果表明，该技术可对试件夹层胶接质量和蜂窝结构作快速有效直观的检测。
It was shown by experimental results that the technique was effective for rapid and intuitive testing of the bonding quality and structure of an aluminum honeycomb composite test piece.
利用本文的方法，实现了对铝蜂窝夹层结构动力学特性的辨识，这对铝蜂窝夹层结构的设计，实验和分析具有一定的实用价值。
To identify the dynamic characteristic of honeycomb sandwich structure via method mentioned in this thesis can be valuable in practice for further design.
分析蜂窝结构在纵横方向上的差异性和面板原材料钎焊后的力学性能对钎焊铝蜂窝板纵向和横向侧压变形过程及破坏形式的影响。
Analyze the effect of the longitudinal and transverse structure difference of honeycomb on the longitudinal and transverse deformation process and destroy type of BAHP.
选择国家知识产权数据库、世界知识产权数据库等多个数据库进行检索，采集1960年到2010年与铝蜂窝有关的专利文献，建立专利数据库。
"The national intellectual property and WIPO" patent database is chosen, aluminium honeycomb technology patent between 1960 and 2010 are collected and the associated patent database is established.
本文针对卫星主要结构材料铝质蜂窝板的非线性动力特性现象进行了振动试验及分析。
In the paper the phenomena in test for nonlinear dynamic behavior of aluminum honeycomb sandwich plate in satellite structure are analysed.
分析结果有益于蜂窝铝的优化设计，有助于找到合适的蜂窝芯格尺寸以满足较大的强度要求。
The results of the analysis are helpful to optimize aluminum honeycomb design and find a suitable honeycomb cell size to meet the requirements of larger intensity.
得到了在受同样大小载荷时，蜂窝铝芯最大应力随蜂窝芯格对边距、深度变化而变化的曲线。
Under the same load, the curve that the maximum stress of aluminum honeycomb core varies with the subtense distance and depth of honeycomb core has been gained.
本文通过摆锤冲击实验，研究了蜂窝铝的动态压缩性能及低速冲击吸能特性。
The study of dynamic compression performance and energy absorption characteristics of aluminium honeycomb structure subjected to low-velocity impact was carried out based on pendulum impact test.
扫描电镜观察显示高铝组细胞表面皱缩，胞膜局部破损呈蜂窝状，突起短，数量少。
The number of swelling, degenerative and necrotic cells was significantly increased in high Al group.
最后再针对其他试验工况，将修正后的有限元模型与实验结果比对，以验证标准蜂窝结构来模拟泡沫铝夹芯的可行性。
In this paper, by modeling a actual foam sandwich panel, the aluminum foam sandwich simplifiedas standard honeycomb is preliminarily proved feasible.
最后再针对其他试验工况，将修正后的有限元模型与实验结果比对，以验证标准蜂窝结构来模拟泡沫铝夹芯的可行性。
In this paper, by modeling a actual foam sandwich panel, the aluminum foam sandwich simplifiedas standard honeycomb is preliminarily proved feasible.
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