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Study on aluminum alloy helicopter deck under static loads

机译:静电负荷下铝合金直升机甲板的研究

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Test and study of aluminum alloy helicopter deck under static load were carried out. The deck is made of aluminum alloy sandwich panel. In the experiment, the deflection and stress of deck are measured under different static load conditions. Load conditions are determined by the conditions that helicopter berths at the deck. When helicopter berths at the deck, the deck endures vertical compressive loads on the deck surface and diagonal tension loads on the tie-down rod which is used to fasten the helicopter. According to the test results under different load conditions, the characteristic behavior and ultimate load carrying capacity were analyzed. Based on experimental results, FEM simulation was made. The results of FEM analysis was agreed with the test results very well. It is shown that the helicopter deck which is composed of aluminum alloy sandwich panel has good mechanical performance.
机译:静电负荷下铝合金直升机甲板的试验研究。甲板由铝合金三明治板制成。在实验中,在不同的静载条件下测量甲板的挠曲和应力。负载条件由直升机泊位在甲板上的条件确定。当甲板上的直升机泊位时,甲板在甲板表面上恢复垂直压缩载荷,并在焊盘上载荷载荷,用于固定直升机。根据在不同负载条件下的测试结果,分析了特征行为和最终负载承载能力。基于实验结果,制造有限元模拟。有限元分析的结果与测试结果相加,非常好。结果表明,由铝合金夹心板组成的直升机甲板具有良好的机械性能。

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