本文研究了蜂窝夹层结构雷达天线罩损伤的修补。
In this paper the repair of damaged honeycomb sandwich radome was studied.
对碳纤维蜂窝夹层结构的动力学问题进行了深入分析。
In this paper, the dynamic analysis of the carbon fiber honeycomb sandwich structure was deeply investigated.
蜂窝夹层结构已成为雷达罩结构设计中广泛应用的重要材料。
Honeycomb sandwich has become an important material in designing radomes instruction.
试验表明，该系统可用于复合材料结构和蜂窝夹层结构的无损检测。
It is concluded that the system can be used in nondestructive detection of composite material and honeycomb structure.
试验证明，该系统可成功用于复合材料结构和蜂窝夹层结构的无损检测。
Experiment proved that the system was successful for the nondestructive testing of composite and honeycomb interlayer structures.
利用热电偶测试热补仪修补复合材料蜂窝夹层结构的面内及厚度方向的温度分布；
The in-plane and through-thickness direction temperature distribution of composite honeycomb sandwich structure repaired by hot bonder was tested with thermocouples.
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.
本文对碳纤维复合材料蜂窝夹层结构侧压强度进行了理论计算，试验值在理论计算范围内。
Theoretical calculation of edge Compressio strength of CFRP Sanduich Construction with honey core is gotten in this paper. The test value is in the range of theoretical Caculation.
本文对玻璃钢蜂窝夹层结构板的弯曲试验结果（四边简支和四边固支）进行理论分析，理论值与试验值符合得很好。
Through the theoretical analysis of the flexural properties of FRP honeycomb sandwich construction, it proves that the values of theory and test agree well.
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.
本文主要研究工作内容如下：1、结合国内外研究成果，综述蜂窝夹层结构常用的动力学分析方法，对常用的几种模型的优缺点进行了分析。
The main contents are as follows:1) In overview of the latest worldwide research results, three equivalent models of honeycomb sandwich structures are given out.
在夹层的地板上，一片半透明的蜂窝结构形成绝缘层，同时让热量和阳光通过它过滤到正下方的传统日本榻榻米房间里。
A section of translucent honeycomb-formation insulation in the floor of a mezzanine level also allows heat and sunlight to filter through to a traditional Japanese tatami room situated directly below.
飞机复合材料零件结构分为蜂窝结构、夹心结构、空心结构、夹层结构等。
Structures of aircraft composite parts include honeycomb, inner contained part, inner empty part, and layered etc.
通过理论设计及CAD辅助计算得到了一种“陷阱”式的宽频带层板型结构吸波材料和一种宽频带蜂窝夹层型结构吸波材料。
By theoretical design and CAD, a kind of wide frequency-width Radar Absorbent Structure Plate named "trap" and a kind of wide frequency-width Radar Absorbent Honeycomb Sandwich Material are obtained.
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.
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.
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