【24h】

Review of Ingress in Gas Turbines

机译:燃气轮机入口的回顾

获取原文
获取原文并翻译 | 示例
获取外文期刊封面目录资料

摘要

This review summarizes research concerned with the ingress of hot mainstream gas through the rim seals of gas turbines. It includes experimental, theoretical, and computational studies conducted by many institutions, and the ingress is classified as externally induced (EI), rotationally induced (RI), and combined ingress (CI). Although EI ingress (which is caused by the circumferential distribution of pressure created by the vanes and blades in the turbine annulus) occurs in all turbines, RI and CI ingress can be important at off-design conditions and for the inner seal of a double-seal geometry. For all three types of ingress, the equations from a simple orifice model are shown to be useful for relating the sealing effectiveness (and therefore the amount of hot gas ingested into the wheel-space of a turbine) to the sealing flow rate. In this paper, experimental data obtained from different research groups have been transformed into a consistent format and reviewed using the orifice model equations. Most of the published results for sealing effectiveness have been made using concentration measurements of a tracer gas (usually CO_2) on the surface of the stator, and-for a large number of tests with single and double seals-the measured distributions of effectiveness with sealing flow rate are shown to be consistent with those predicted by the model. Although the flow through the rim seal can be treated as inviscid, the flow inside the wheel-space is controlled by the boundary layers on the rotor and stator. Using boundary-layer theory and the similarity between the transfer of mass and energy, a theoretical model has been developed to relate the adi-abatic effectiveness on the rotor to the sealing effectiveness of the rim seal. Concentration measurements on the stator and infrared (IR) measurements on the rotor have confirmed that, even when ingress occurs, the sealing flow will help to protect the rotor from the effect of hot-gas ingestion. Despite the improved understanding of the "ingress problem," there are still many unanswered questions to be addressed.
机译:这篇综述总结了有关热的主流气体通过燃气轮机轮辋密封圈进入的研究。它包括许多机构进行的实验,理论和计算研究,并且入侵分为外部诱导(EI),旋转诱导(RI)和组合入侵(CI)。尽管EI进入(这是由涡轮机环中的叶片和叶片产生的压力的周向分布引起的)在所有涡轮机中均发生,但RI和CI进入在非设计条件下以及对于双密封的内部密封而言可能很重要。密封件的几何形状。对于所有三种类型的入口,都显示了来自简单孔板模型的方程式,对于将密封效果(以及因此吸入涡轮机叶轮空间中的热气量)与密封流速相关联非常有用。在本文中,从不同研究小组获得的实验数据已转换为一致的格式,并使用孔板模型方程式进行了审查。大部分已发表的密封效果结果是通过对定子表面上的示踪气体(通常为CO_2)进行浓度测量得出的,并且-对于单密封和双密封的大量测试-密封效果的实测分布流速显示与模型预测的一致。尽管通过轮辋密封的流量可以看作是不可见的,但叶轮空间内部的流量是由转子和定子上的边界层控制的。利用边界层理论和质量与能量传递之间的相似性,建立了一个理论模型,将转子上的绝热效果与轮辋密封的密封效果联系起来。定子上的浓度测量和转子上的红外(IR)测量已确认,即使发生侵入,密封流也将有助于保护转子免受热气吸入的影响。尽管人们对“进食问题”有了更深入的了解,但仍有许多未解决的问题需要解决。

著录项

  • 来源
    《Journal of Engineering for Gas Turbines and Power》 |2016年第12期|120801.1-120801.16|共16页
  • 作者单位

    Department of Mechanical Engineering, University of Bath, Bath BA2 7AY, UK;

    Department of Mechanical Engineering, University of Bath, Bath BA2 7AY, UK;

    Department of Mechanical Engineering, University of Bath, Bath BA2 7AY, UK;

    Department of Mechanical Engineering, University of Bath, Bath BA2 7AY, UK;

  • 收录信息
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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