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Increased turbo compressor reliability by analysis of fluid structure interaction

机译:通过分析流体结构相互作用来增加涡轮压缩机可靠性

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The integrity of compressors and pumps is of paramount importance for the gas and oil industry. Failures may result in serious production losses that are in no proportion with the cost of the equipment involved. Besides, the equipment may be inaccessible for maintenance for a long period of time due to unfavourable weather conditions. The requirements of compressors with respect to pressures, capacity, power and operating range, are increasing. The answer to this is innovative compressor concepts, advanced materials and manufacturing techniques. Unexpected phenomena, however, for instance due to fluid structure interactions, will occur that can lead to serious damage of the machine. In this paper such a phenomenon is discussed by presenting a case study. On the NAM L9 platform, a centrifugal compressor was operated for the transport of gas to shore. The compressor showed serious vibrations at certain conditions that finally led to failure. An analysis of the vibration measurements showed that extremely large vibrations could occur at the blade passing frequency. By means of modeling, an analysis could be made of the acoustic resonances that could possibly occur in the compressor. It was found that a likely cause of the failure was a resonance mode in the shroud cavity of the 3rd and 4th stage. The acoustic resonance modes could be excited by pulsation sources present in the machine. Especially, the sources at the low solidity vanes were suspected to contribute to the excitation of the resonance. Vortex shedding at the impeller edge was also suspected to contribute. The resonance in the cavity may exert large dynamic forces near the trailing edge of the impeller shroud. Due to a structural vibration modes of the shroud, a fatigue failure occurred. The paper describes the root cause analysis consisting of an analysis of the acoustic and structural vibration modes. The consequences for the design of similar compressors are subsequently reviewed. A future outlook is presented concerning dense gas compression systems for CO2 and high pressure reinjection.
机译:压缩机和泵的完整性是为石油和天然气行业至关重要。故障可能会导致严重的生产损失,其与所涉及的设备的成本没有比例。此外,该设备可能无法访问对维护的很长一段时间,由于不利的天气条件。压缩机相对于压力,容量,功率和操作范围的要求,正在增加。这个问题的答案是创新的压缩机理念,先进的材料和制造技术。意外的现象,但是,例如由于流体结构相互作用,会发生,可导致机器的严重损坏。在本文中这种现象是由呈现为例进行讨论。在NAM L9平台,离心压缩机被用于气体输送到岸上操作。压缩机在一定条件最终导致失败存在严重的振动。振动测量的分析表明,非常大的振动可能在叶片通过频率发生。通过建模的装置,分析可以由那些可能发生在压缩机的声共振。结果发现,失败的可能原因是在第3和第4级的护罩空腔共振模式。声谐振模式可以由存在于机脉动源激发。特别是,在低稠度叶片来源被怀疑有助于共振的激励。在叶轮边缘涡街也涉嫌作出贡献。在腔体谐振可施加叶轮护罩的后缘附近的大的动态力。由于护罩的结构振动模式,发生疲劳破坏。本文描述了由声学和结构振动模式的分析的根本原因分析。类似的压缩机设计的后果随后审查。提出未来的前景有关的CO2和高压回注稠密气体压缩系统。

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