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PRACTICAL BLADE VIBRATION ANALYSIS USING THE RESULTS OF FREE-FREE MODAL TEST

机译:使用无自由模态试验的结果实用刀片振动分析

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Experimental results show that natural frequencies are often significantly affected by small differences in the construction of joints in nominally identical test pieces. But it can be difficult to find joint parameters to which the numerical predictions are sensitive. Testing in free-free condition needs no fixture; this advantage has made it cost efficient and easier to install than clamped test, especially for test pieces with complex shapes such as turbine blades. In addition clamped test often produces relatively inaccurate data. The modal analysis of a single turbine blade is investigated in this paper. The blade has been tested in free-free and clamped conditions. Finite element analysis is firstly accomplished for free-free condition and the FE model has been updated using experimental data obtained from the free-free test. The accuracy of the FE model has been verified by comparing results with the experimental data of clamped test. Good correlation between results obtained from modal test and FEA in clamped condition shows that free-free test of the blade can be used to update the FE model. Subsequently, the reconciled FE model can be fixed to find natural frequencies of the blade in clamped condition.
机译:实验结果表明,在名义上相同的测试件中的关节构建的小差异差异很大,自然频率往往受到显着影响。但是,很难找到数值预测敏感的联合参数。在自由状态下测试不需要夹具;这一优势使得其成本高,更容易安装而不是夹紧测试,特别是对于具有复杂形状的测试件,例如涡轮叶片。此外,夹紧测试通常会产生相对不准确的数据。本文研究了单涡轮机叶片的模态分析。刀片已在无自由夹紧条件下进行测试。首先实现有限元分析,无需自由测试的无自由状况,并且使用从自由测试中获得的实验数据更新Fe模型。通过将结果与钳位试验的实验数据进行比较来验证Fe模型的准确性。从夹紧条件的模态测试和FEA获得的结果之间的良好相关性表明,刀片的无自由试验可用于更新FE模型。随后,可以将和解的Fe模型固定以在夹紧状态下找到刀片的自然频率。

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