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.
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.
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.
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.
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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