顶部铰接-底部固定悬链线型柔性立管空间耦合振动特性实验研究

Experimental investigation on the spatial coupling vibration of a top-hinged-bottom-fixed catenary flexible riser

  • 摘要: 海洋立管顶部常铰接于水面浮式设施下方,在波流激励下存在涡激振动响应,潜在疲劳失效风险。采用高速摄像非介入光学测试方法,对布置于循环水槽中的顶部铰接-底部固定、长径比为125的悬链线型柔性立管进行了涡激振动实验监测,发现立管平面内与平面外的振动阶数及频率均随约化速度的增加逐渐升高,平面外的最大均方根振幅在模态过渡时有明显起伏,而在平面内不明显,但主导频率在模态过渡时有明显的跃升。悬链线型柔性立管的涡激振动在空间三个方向上的模态转移均不同步,在模态过渡组次,立管轴向不同部位的主振频率及主导模态不同,存在空间上的模态竞争现象,整根立管呈现的均方根振幅曲线形状取决于模态权重的空间分布及主导模态控制的管段长度。根据均方根振幅曲线的波峰个数和振动频率的吻合程度,提出了强耦合+、强耦合、弱耦合和弱耦合四种振动耦合模式,对柔性立管空间上的耦合模式进行了分区。

     

    Abstract: Marine risers are usually hinged under a platform, experiencing the Vortex-Induced Vibration (VIV) due to the excitation of wave and current and hence the potential fatigue damage. In this paper, the non-intrusive optical test technique was employed to monitor the vibration displacement of a catenary flexible riser arranged in a water-circulating flume. The aspect ratio of the top-hinged and bottom-fixed riser model is 125. It was found that the in- and out-of-plane excited modal order and frequency grows with the reduced velocity. The maximum root-mean-squared amplitude in the out-of-plane direction underwent distinct undulation during the mode transition, while it was not obvious in the in-plane response. Nevertheless, the dominant frequency has a significant rise when the mode transition occurred. The mode transition was out of sync in the three directions. In mode transition cases, the dominant frequency and mode varied along the riser length, suggesting the spatial mode competition. The profile of root-mean-squared amplitude depended on the spatial distribution of mode weight and the dominated riser length by the dominant mode. Comprehensively taking into account the number of the peaks of root-mean-squared amplitude profile and the consistency of vibration frequency, four interaction patterns are proposed, including the strong coupling+, strong coupling, weak coupling and weak coupling. Accordingly, the space partition of the response interaction in the considered reduced velocity range is provided.

     

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