主管单位:中华人民共和国工业和信息化部
主办单位:西北工业大学  中国航空学会
地       址:西北工业大学友谊校区航空楼
蜂窝夹层结构弯曲性能测试方法的离散度分析
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航空工业第一飞机设计研究院 结构设计研究所

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V214.6

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Dispersion analysis of the testing method for the flexural performance of honeycomb sandwich structure
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The Structure Institute,AVIC The First Aircraft Institute

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    摘要:

    在对蜂窝夹层结构弯曲性能的测试中,由于测试方法的不同,存在数据离散度较大,造成可信度降低的情形,不利于对结构真实性能的评估。应用弯曲方法测定、弯曲性能均值法分析和侧压法对蜂窝夹层结构进行弯曲性能研究,对比数据的离散性差异,评定三种测试方法的有效性;通过对试验件的测试和分析,获得蜂窝夹层板的弯曲性能数据。结果表明:按ASTM 方法测定的弯曲性能数据,离散系数大于0.1,无法体现测试结果的真实性;按弯曲性能均值法将蜂窝芯剪切模量代入关系式求解夹层结构的弯曲性能,离散系数小于0.09,结果可信;按GB/T 1454—2005 侧压法测定夹层结构的侧压模量,其结果低于弯曲方法测定值,考虑面板自身的刚度影响,侧压方法的结果真实性更高,离散系数小于0.07,可信度进一步提高。

    Abstract:

    In the test of the flexural performance of the honeycomb sandwich structure, due to the different test methods, there is a situation that the data dispersion is large, which causes the reliability to be reduced, which is not conducive to the evaluation of the true performance of the structure. The flexural performance of the honeycomb sandwich structure was studied by flexural method measurement; flexural performance average method analysis and lateral pressure method, and the discrete difference of data was compared to evaluate the effectiveness of the three test methods. Through the test and analysis of the test pieces, the flexural performance data of the honeycomb sandwich panel is obtained. The results show that: the dispersion coefficient of the flexural performance data measured according to the ASTM method is greater than 0.1, which conceals the authenticity of the test results; according to the mean value of the flexural performance The method substituting the honeycomb core shear modulus into the relational formula to solve the flexural performance of the sandwich structure, the dispersion coefficient is less than 0.09, the result is credible; according to GB/T 1454-2005 lateral compression method, the lateral compression modulus of the sandwich structure is lower than that of flexural test, considering the influence of the stiffness of the panel itself, the result of the lateral pressure method is more authentic and the dispersion coefficient is less than 0.07, which is credible The degree is further improved.

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引用本文

李云鹏,郭祥.蜂窝夹层结构弯曲性能测试方法的离散度分析[J].航空工程进展,2022,13(5):116-122

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历史
  • 收稿日期:2021-12-21
  • 最后修改日期:2022-03-13
  • 录用日期:2022-03-19
  • 在线发布日期: 2022-08-19
  • 出版日期: