首页> 外文会议>Society of Petroleum Engineers Russian Oil and Gas Exploration and Production Technical Conference and Exhibition >Increased turbo compressor reliability by analysis of fluid structure interaction
【24h】

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

获取原文

摘要

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对于天然气和石油工业来说至关重要。失败可能导致严重的生产损失,这些损失与所涉及的设备的成本没有比例。此外,由于不利的天气条件,该设备可以在很长一段时间内进行维护。压缩机对压力,容量,功率和操作范围的要求正在增加。答案是创新的压缩机概念,先进的材料和制造技巧。然而,例如由于流体结构相互作用,可能会导致机器的严重损坏,因此意外的现象。在本文中,通过呈现案例研究讨论了这种现象。在NAM L9平台上,操作离心式压缩机,用于将气体运输到岸上。压缩机在最终导致失败的某些条件下表现出严重的振动。对振动测量的分析表明,在叶片通过频率可能会出现极大的振动。通过建模,可以对可能发生在压缩机中的声谐振来进行分析。结果发现,失败的可能原因是第3和第4阶段的护罩腔中的共振模式。声谐振模式可以通过机器中存在的脉动源激发。特别是,怀疑低固态叶片的来源有助于激发共振。叶轮边缘的涡旋脱落也被怀疑有助于贡献。腔中的共振可以在叶轮护罩的后缘附近发挥大动力力。由于护罩的结构振动模式,发生了疲劳失效。本文描述了由声学和结构振动模式分析的根本原因分析。随后审查了对类似压缩机设计的后果。未来的前景是关于CO2和高压再注的致密气体压缩系统。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号