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湿热环境对铝蜂窝夹层复合材料性能的影响

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鉴于某型号整流罩存在环境温湿度较大,在该条件存放较长时间,可能会对产品的性能造成不利影响.为了验证湿热环境对铝蜂窝夹层结构复合材料性能的影响,将试样放置80 ℃、相对湿度85%的环境中,考察试样的存放时间与吸湿率的关系以及湿热环境对双压剪性能、平拉性能、侧压性能的影响规律.试验结果表明,存放时间达到8 d时吸水率达到平衡,双压剪强度基本不变,平拉强度下降了 11.08%;侧压强度、侧压模量分别下降了 11.04%,13.94%.通过对破坏形貌分析发现,吸水率达到平衡后,铝蜂窝表面的Al/Mg比值由42.11%提高至48.79%,蜂窝外观未出现明显变化.此时,平拉试样的破坏形貌由铝蜂窝破坏向铝蜂窝及铝蜂窝/面板界面混合破坏模式转变.
Effect of Humid and Hot Environment on Properties of Aluminum Honeycomb Sandwich Composites
Due to the high ambient temperature and humidity associated with a specific type of fairing,the product performance may be adversely affected if the fairing is stored for an extended period.In order to verify the influence of hot and humid environment on the properties of aluminum honeycomb sandwich structure composites,the samples were subjected to conditions of 80℃ and 85%relative humidity,and the relationship between storage time and moisture absorption was investigated,along with the effects of the hot and humid environment on the properties of flatwise tension strength,double compression shear and edgewise compressive strength.The test results show that the water absorption reaches equilibrium when the storage time reaches 8 days,the double compression shear strength remains relativel unchanged,and the flatwise tension strength decreases by 11.08%.Additionally,the edgewise compressive strength and edgewise compressive modulus decreas by 11.04%and 13.94%respectively.An analysis of the damage morphology reveals that after the water absorption reached equilibrium,the Al/Mg ratio on the surface of aluminum honeycomb increases from 42.11%to 48.79%,and the honeycomb appearance did not change significantly.At this time,the failure morphology of the flatwise tensile specimen transitions from aluminum honeycomb failure to aluminum honeycomb and aluminum honeycomb/panel interface mixed failure mode.

Aluminum honeycombSandwich structureMoisture absorptionMechanical properties

郑国栋、郭子民、李桂洋、李伟明、肖瑛、NAN Xun

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航天长征睿特科技有限公司,天津 300475

航天材料及工艺研究所,北京 100076

Aerospace Research Institute of Materials & Processing Technology,Beijing 100076

蜂窝 夹层结构 吸湿 力学性能

2024

宇航材料工艺
航天材料及工艺研究所

宇航材料工艺

CSTPCD北大核心
影响因子:0.378
ISSN:1007-2330
年,卷(期):2024.54(6)