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Predicting vibration characteristics of rotating composite blades containing CNT-reinforced composite laminae and damaged fiber-reinforced composite laminae

机译:旋转复合叶片的振动特性,含有CNT加强复合薄层和损坏的纤维增强复合薄层

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摘要

Existing of cracks within blade structures can cause stiffness degradation and hence changes their vibration characteristics. This study investigates the vibration behaviors of rotating pre-twisted hybrid composite blades containing functionally graded carbon nanotube-reinforced composite (FG-CNTRC) laminae and damaged fiber-reinforced composite (FRC) laminae. The degraded stiffness of the cracked lamina is modeled through the self-consistent model (SCM). The blade is modeled as a shell structure that is formed by twisting a plate around its mean line. With the help of the differential geometry theory, a novel shell model has been derived to describe the kinetics of the blade. The effect of the Coriolis and centrifugal force are both presented in the formulation, which results in a damped-like free vibration system governed by a system of second-order ordinary differential equations (ODEs). Utilizing the state space technique, the system is reformulated to a system of first-order ODEs. The IMLS-Ritz method is then used for discretizing the ODEs. After carefully validating the effectiveness of the presented model through a series of comparison studies, parametric studies including CNT distribution configuration, rotating speed, geometrical parameters on the vibration responses of cross-plied composite blades are systematically examined. The vibration characteristics of angle-plied composite blades are also investigated.
机译:叶片结构内的裂缝存在可能导致刚度降解,因此改变它们的振动特性。本研究研究了旋转预扭曲的混合复合叶片的振动行为,其含有功能梯度碳纳米管增强复合物(FG-CNTRC)薄层和受损纤维增强复合材料(FRC)薄层的液体。裂化薄层的降解刚度通过自我致一致的模型(SCM)进行建模。刀片被建模为壳结构,该壳结构通过围绕其平均线扭转板而形成。在差分几何论的帮助下,已经得出了一种新颖的壳模型来描述刀片的动力学。 Coriolis和离心力的效果均呈现在制剂中,这导致由二阶常微分方程(ODES)的系统管辖的湿润的自由振动系统。利用状态空间技术,该系统将重新重新格式化到一阶码内系统。然后使用IML-RITZ方法来离散化杂散。通过一系列比较研究仔细验证所呈现的模型的有效性,系统地检查包括CNT分布配置,转速,旋转速度,交叉复合刀片的振动响应的几何参数的参数研究。还研究了角度覆盖复合刀片的振动特性。

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