以Zn-22Al（ZA22）基泡沫材料为芯材，LY12铝板为面板制备了泡沫夹芯复合板。研究了泡沫夹芯复合板的三点弯曲行为，观察了复合板的破坏模式，分析了复合板弯曲性能的影响因素，运用层合梁刚度优化理论探讨了其机理。研究结果表明，ZA22泡沫夹芯复合板的三点弯曲载荷位移曲线可按线性段、非线性段和失稳段表示其特征；其弯曲极限载荷随孔隙率的增大而减小，并且泡沫夹芯复合板表现出明显的层合效果。三点弯曲载荷作用下，泡沫夹芯复合板的主要失效模式为芯材的剪切破坏。%The sandwich panel were fabricated using Zn-22A1 matrix foam as the core material and the LY12 aluminum panel as the shell. The bending behavior of the sandwich panel was studied by threepoint bending test. The failure mode of the sandwich panel was observed and the influencing factors were analyzed. Applying the stiffness optimization theory of sandwich panels, the deformation mechanism of the sandwich panels was discussed. The results showed that the bending curves of the sandwich panel can be divided into three regions, including the linear deformation region, the non- linear deformation region and the unsteady region. The ultimate load of the sandwich panel decreases when the porosity of the foam is rising. The sandwich panel shows a favorable cooperative effect on mechanical property. The primary failure mode of the sandwich panel is the core shearing.
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