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.
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.
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.
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.
基于磁场与摩擦学蜂窝芯材料固持原理，提出复杂型面纸基蜂窝零件固持平台的模块化设计思想。
Based on magnetic field and frictional-clamping principle, a new modularization design concept is presented for the fixation system of paper honeycomb parts with complex shapes.
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.
地板是由蜂窝夹芯粘接于玻璃纤维增强塑料(GFRP)薄板之间制成的。
The floor panels are made of a honeycomb core which is bonded between Glass-fiber Reinforced Plastic (GFRP) sheets.
建立了蜂窝夹芯结构的脱胶修补计算模型，分析了胶膜参数对剩余强度的影响，初步研究了其修补技术；
The repaired honeycomb structures are calculated, and the influence of glue's parameters is discussed by the finite element model and program stated above, the technique of its repair is studied.
分析了微波加热机理，介绍了一种用微波加热固化技术粘接修理蜂窝夹芯结构的新工艺。
The mechanism of microwave heating was analyzed, and a new technics of repairing composite sandwich structure with microwave heating was introduced.
本文利用木质面板与和纸质蜂窝材料复合，该夹芯材料不但保留了原蜂窝材料的优点，而且还大大提高了力学强度。
The sandwich construction which was consisted of wooden faceplate with a paper honeycomb retained the original advantages of the honeycomb material and greatly increased the mechanical intensity.
对复合材料蜂窝夹芯结构受损伤之后的几种典型修理方法及修理材料、修理工艺等内容进行了试验研究。
A few methods, materials and techniques of repair on composite honeycomb sandwich structures after damages are investigated experimentally in this paper.
采用横向涂胶、纵向切割、纸芯连续的蜂窝纸板生产工艺可提高生产效率，并实现全自动生产。
A new kind of beehive carton production craft was introduced: horizontal gum, lengthways incision, the continuous paper core. It can improve productivity and realize automatic production.
采用瞬间液相扩散复合原理生产钢质蜂窝夹芯减振板的关键问题之一是中间夹层助复剂的选择和配制。
One of the problems experienced in transient liquid diffusion bonding for carbon steel sandwich panels is the interlayer bonding assistant coat.
提出了蜂窝纸芯正六边形边长值对压缩性能的影响。
The influence of side length value of regular hexagon on compression characteristics of honeycomb paperboard core was discussed.
凯腾公司拥有最先进的全自动蜂窝纸芯、纸板生产线及最新的生产工艺。
Kai Teng company has the most advanced automatic Honeycomb Paper Core, cardboard production line and the latest production technology.
提出一种三层32结点温度壳单元，对蜂窝夹芯复合材料壳体的瞬态温度场进行了有限元分析。
A kind of three layered 32-node temperature shell element is presented for the transient temperature field FEM analysis of the honeycomb sandwich composite shell.
通过分析结果可知蜂窝纸板的应力集中出现在纸芯的上端，最大变形出现在离上端1/5处，且蜂窝纸芯的高度对蜂窝纸板压缩力学性能影响较小，与实验结果相符合。
The stress and strain of honeycomb paperboard is also analyzed. The result proves that the concentrative stress is the honeycomb paperboard off the top, and the furthest distortion is at the 1/5.
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.
根据用户需要制作各种克重、蜂窝孔径密度、规格和材质的蜂窝纸芯和蜂窝纸板！
We can provide customers with honeycombed boards with various areas densities, honeycomb-sizes, and paper materials.
蜂窝夹芯复合梁进行损伤检测的实验研究，通过使用相结合的损伤检测方法。
Experimental investigations are performed on the damage detection for honeycomb sandwich composite beams by using a combined damage detection method.
给出了复合材料蜂窝夹芯结构修理前后的刚度和强度变化规律。
The authors also present the rule of changes of stiffness and strength of composite honeycomb sandwich before and after repair.
面板采用对称铺层、等高度蜂窝夹芯，利用能量法对临界载荷进行了计算并给出了一些计算曲线。
The faces are symmetrical and the height of cores is constant. In this paper, critical loads are evaluated using energy method. Some calculative figures are given.
面板采用对称铺层、等高度蜂窝夹芯，利用能量法对临界载荷进行了计算并给出了一些计算曲线。
The faces are symmetrical and the height of cores is constant. In this paper, critical loads are evaluated using energy method. Some calculative figures are given.
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