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Free vibrations of the cantilever blades and shrouded bladed discs of the gas turbine

机译:燃气轮机的悬臂叶片和带罩叶片盘的自由振动

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摘要

The failure of the rotor blades in a gas turbine was reported. The global rotating mode shapes of flexible shrouded bladed disc assemblies are calculated by using a finite element approach. Rotational effects, such as centrifugal stiffening are accounted for, and all the possible couplings between the flexible parts are allowed. The spin softening effects are neglected. The dynamic analyze of the shrouded bladed disc shows that the bladed disc was designed with the sufficient safety region of the resonance. In case of one blade getting loose, this blade is vibrating in resonance.
机译:据报道,燃气轮机中的转子叶片出现故障。挠性带叶片叶片盘组件的整体旋转模式形状是通过使用有限元方法计算的。考虑到旋转效应,例如离心加强,并且允许在挠性部件之间进行所有可能的联接。忽略自旋软化效果。笼罩式叶片盘的动态分析表明,叶片盘的设计具有足够的共振安全区域。如果一个刀片松动,则该刀片会共振。

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