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Multilevel finite element modeling and coupling vibration analysis of the drum in blade-disk-drum assembly

机译:叶片-磁盘-滚筒组件中滚筒的多级有限元建模和耦合振动分析

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Blade-disk-drum (BDD) assemblies are commonly used in rotors of aeroengine. This paper investigates the vibration characteristics of the drum in the BDD assembly. In the analysis, multilevel modeling method based on ANSYS software is proposed. Free vibrations of single drum, disk-drum assembly, and the BDD assembly are calculated and carefully examined to discover the special modal shapes and coupling effects. Then according to the working environment, equivalent aerodynamic loads are imposed on blades and the drum respectively, to explore the vibration behaviors of the drum in the BDD assembly. Results reveal that, vibration of the drum, which may result in rub-impact or/and fatigue failure, can be induced by coupling vibration result from the aerodynamic loads on blades and drum, as well as the drum-dominant mode triggered by the aerodynamic loads on drum.
机译:叶片盘鼓组件(BDD)通常用于航空发动机的转子。本文研究了BDD组件中感光鼓的振动特性。在分析中,提出了基于ANSYS软件的多层次建模方法。计算并仔细检查了单鼓,磁盘-鼓组件和BDD组件的自由振动,以发现特殊的模态形状和耦合效果。然后根据工作环境,分别在叶片和滚筒上施加等效的空气动力学载荷,以探索BDD组件中滚筒的振动行为。结果表明,鼓的振动(可能导致摩擦影响或疲劳破坏)可以由叶片和鼓上的气动载荷耦合振动结果以及由气动触发的鼓主导模式引起。装在鼓上。

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