| 1. | Peeling analysis of unperforated honeycomb structure
无孔蜂窝夹层结构脱粘剥离应力分析 |
| 2. | Brazed all honeycomb sandwich
铜焊全金属蜂窝夹层结构 |
| 3. | Thermal conductivity of honeycomb sandwich panels with carbon fibre mesh plates at low temperature
网状碳纤维面板蜂窝夹层结构低温热导率测试研究 |
| 4. | Application of homogenization fem to the equivalent elastic constants of honeycomb structures
蜂窝夹层结构等效弹性常数的多步三维均匀化数值计算分析 |
| 5. | To use the macro - mechanics theory and the composite - mechanics theory analysed the honeycomb structure , and get the equivalent parameter of the honeycomb structure
进而从宏观力学、复合材料力学的角度,对蜂窝夹层结构进行了理论分析,得出了蜂窝结构等效参数的推导方法。 |
| 6. | To identify the dynamic characteristic of honeycomb sandwich structure via method mentioned in this thesis can be valuable in practice for further design ,
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。 |
| 7. | Finally , the nonlinear identification method to stochastic data in frequency domain is used to analyze and identify the nonlinear characteristic of some multifunctional electrical case with honeycomb sandwich structure
最后,将随机数据的频域非线性分析与辨识方法应用于某铝蜂窝夹层结构多功能电子机箱的非线性特性研究中。 |
| 8. | The paper briefly describes the characteristic and damnification of carbon / epoxy facings - aluminum honeycomb sandwich construction which was used for one satellite that was manufactured by us , and also detailed introduce the repairing technics for damnification
摘要本文介绍了我单位研制的某型号卫星碳环氧面板铝蜂窝夹层结构件结构特点及损伤情况，且对损伤修补内容作了较详细叙述。 |
| 9. | Through the studies of its forming process and performance of nomex sandwich constructions composite , it not only provides the perfotmance data and test basis for the normal usage of sandwich constructions but also provides the experiences that was to be accumulated in aircraft
总之，通过对nomex蜂窝夹层结构成型工艺及材料性能的研究，为蜂窝夹层结构在航空领域中的正常应用提供了性能数据和实验依据，同时也为蜂窝夹层结构在飞机上的应用积累了经验。 |
| 10. | After mechanical and process properties testing , the results indicated that : ( 1 ) the film resin can make the properties good in climbing drum peer strength of sandwich constructions composite , the little effects of the film resin on other mechanical properties have been given ; ( 2 ) the sandwich composite has the better mechanical properties at central symmetry layer than asymmetric layer ; ( 3 ) through the study of the different pressure of the sandwich composite , the result is obtained that the edgewise properties increases , the flexural properties decreases with the pressure increase from 0 . 2mpa to 0 . 5mpa ; ( 4 ) at the sameness extend layer , the mechanical properties of the laminate is bigger than that of the honeycomb sandwich panel ; ( 5 ) through the studies on honeycomb sandwich plate delamination under three - point bending tests . it is found that the flexural strength decreases with the area of delamination increases
研究表明： ( 1 )胶膜能明显的提高蜂窝夹层结构的剥离性能，对其它性能的影响不大； ( 2 )对称铺层较非对称铺层的力学性能高； ( 3 )固化压力由0 . 3mpa提高至0 . 5mpa时，蜂窝夹层结构的侧压强度提高，而弯曲强度和剪切刚度分别降低； ( 4 )蜂窝夹层结构中的面板较同样材料铺层的复合材料叠层板的力学性能低； ( 5 )蜂窝夹层结构的界面上有缺陷时，弯曲强度下降，且随着缺陷面积增大，弯曲强度下降幅度增大。 |
