Mg-6Gd-3Y-0.5Zr镁合金阻尼性能及机理研究
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北京宇航系统工程研究所,北京 100076

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TB30

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Research on Damping Performance and Mechanism of Mg-6Gd-3Y-0.5Zr Magnesium Alloy
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Beijing Institute of Astronautical Systems Engineering, Beijing 100076

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    摘要:

    Mg-6Gd-3Y-0.5Zr镁合金已开始应用于航天结构产品,其材料阻尼性能直接关系到结构的动态特性及响应,采用DMA测试仪对其阻尼性能进行了测试并分析了其阻尼机理。结果表明:Mg-6Gd-3Y-0.5Zr合金阻尼性能随应变振幅增大而增大,其常温下符合G-L位错阻尼理论;合金阻尼性能随温度升高而增加,在测试的1~80 Hz范围内,频率越低则阻尼随温升的变化越敏感,温度对其阻尼性能的影响符合Schoeck理论。

    Abstract:

    The Mg-6Gd-3Y-0.5Zr magnesium alloy had been used in aerospace structural products,its internal damping performance was directly related to the dynamic characteristics and response of structures,the internal damping performance of Mg-6Gd-3Y-0.5Zr magnesium alloy was studied using DMA tester and the mechanism was analyzed.The results show that the damping of Mg-6Gd-3Y-0.5Zr alloy gradually increases with the increase of strain amplitude and the mechanism at temperature conforms to the G-L dislocation damping theory.The damping performance of alloy gradually increases with the increase of temperature.Within the tested frequency range of 1~80 Hz,the lower the frequency is, the more sensitive the damping is to the change of temperature,and the influence of temperature on damping performance conforms to the Schoeck theory.

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孟德浩,邢力超,王非凡,马飞,袁文全. Mg-6Gd-3Y-0.5Zr镁合金阻尼性能及机理研究[J].宇航材料工艺,2025,55(1):93-97.

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历史
  • 收稿日期:2023-01-20
  • 最后修改日期:2025-02-23
  • 录用日期:2023-06-30
  • 在线发布日期: 2025-03-04
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