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EXERGY ANALYSIS OF PART FLOW EVAPORATIVE GAS TURBINE CYCLES― PART 2: RESULTS AND DISCUSSION

机译:部分流动蒸发燃气涡轮循环分析 - 第2部分:结果与讨论

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This paper is the second part of a two-part paper. The first part contains an introduction to the evaporative gas turbine (EvGT) cycle and the methods used in the study. The second part contains the results, discussion, and conclusions. In this study, exergy analysis of EvGT cycles with part flow humidification based on the industrial GTX100 and the aerode-rivative Trent has been performed. In part flow EvGT cycles, only a fraction of the compressed air is passed through the humidification system. The paper presents and analyzes the exergetic efficiencies of the components of both gas turbine cycles. The highest cycle exergetic efficiencies were found for the full flow case for the GTX100 cycles and for the 20% part flow case for the Trent cycles. The largest exergy destruction occurs in the combustor, and the exergetic efficiency of this component has a large influence on the overall cycle performance. The exergy destruction of the heat recovery system is low.
机译:本文是两篇纸的第二部分。第一部分包含蒸发燃气轮机(EVGT)循环的介绍以及研究中使用的方法。第二部分包含结果,讨论和结论。在该研究中,已经进行了基于工业GTX100的部分流量加湿的EVGT循环的电力分析,已经进行了基于工业GTX100和空气致动钻。在部分流动EVGT循环中,仅通过加湿系统的压缩空气的一部分。本文提出并分析了燃气涡轮机循环组件的横向效率。找到了最高的循环渗透效率,用于GTX100循环的全流量案例,以及用于特伦特循环的20%零件流量情况。在燃烧器中发生最大的漏洞破坏,该组件的前进效率对整体循环性能具有很大影响。热回收系统的暴露破坏是低的。

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