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Development of a performance estimation tool for gas turbine engine centrifugal compressors.

机译:开发用于燃气轮机离心压缩机的性能评估工具。

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摘要

A preliminary design tool has been created to aid in the design and development of a centrifugal flow compressor impeller for a gas turbine engine. The design tool requires basic compressor design point geometry which could be obtained from simple calculations during the preliminary design phase of a gas turbine engine. Using this information, the design tool is able to estimate the compressor map. Elements from several models are incorporated in the design tool, most notably the impeller two-zone model for the construction of the compressor map at higher rotational speeds. To complete the map, the developed tool utilizes a low speed extrapolation technique to estimate low speed characteristics. The two-zone model utilizes few empirical correlations, however those used represent the most appropriate available. Furthermore, the design tool estimates the gas turbine performance based upon the design point data of the compressor, most notably the design pressure ratio and design mass flow rate. From this, component matching calculations are performed to estimate the gas turbine performance over a range of mass flow rates and rotational speeds.;The tool was validated against several test impellers obtained in the literature and also against a computational fluid dynamics study. The design tool is useful for synthesis of a compressor map which is required for the estimation of off-design engine performance at the preliminary design phase. One of the strengths of the design tool is that it allows for compressor characteristics estimation without the requirement for more complex streamline curvature or computational fluid dynamics studies. Overall, the developed tool showed good agreement between the developed compressor maps and actual compressor maps obtained in the literature. Furthermore, the design tool showed good agreement in the overall engine performance calculations when compared to more popular gas turbine engine performance estimation packages.
机译:已经创建了一种初步的设计工具,以帮助设计和开发用于燃气涡轮发动机的离心式流动压缩机叶轮。该设计工具需要基本的压缩机设计点几何形状,这可以从燃气涡轮发动机的初步设计阶段的简单计算中获得。使用此信息,设计工具能够估算压缩机图。设计工具中包含了来自多个模型的元素,最著名的是叶轮两区模型,用于在较高转速下构造压缩机图。为了完成地图,开发的工具利用低速外推技术来估计低速特性。两区域模型几乎没有经验相关性,但是所使用的那些相关性是最合适的。此外,设计工具基于压缩机的设计点数据(最主要是设计压力比和设计质量流率)估算燃气轮机性能。据此,进行了组件匹配计算,以估算在一定质量流量和转速范围内的燃气轮机性能。该工具已针对文献中获得的多个测试叶轮进行了验证,同时还针对计算流体动力学研究进行了验证。该设计工具可用于合成压缩机图,这是在初步设计阶段估算非设计发动机性能所必需的。该设计工具的优势之一在于,它可以估算压缩机的特性,而无需进行更复杂的流线曲率或计算流体动力学研究。总体而言,开发的工具显示出已开发的压缩机图与文献中获得的实际压缩机图之间具有良好的一致性。此外,与更流行的燃气轮机性能评估软件包相比,该设计工具在总体发动机性能计算中显示出良好的一致性。

著录项

  • 作者

    Britton, Ian A. W.;

  • 作者单位

    Carleton University (Canada).;

  • 授予单位 Carleton University (Canada).;
  • 学科 Engineering Mechanical.
  • 学位 M.A.Sc.
  • 年度 2008
  • 页码 160 p.
  • 总页数 160
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 机械、仪表工业;
  • 关键词

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