Structural and Parametric Investigations of Oxy-Fuel Combustion Cycles with the Aim of Increasing Efficiency of Electricity Production

Vladimir Kindra, S. Osipov, A. Vegera
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引用次数: 4

Abstract

This study aims to present the results of thermodynamic analysis and optimization of the E-MATIANT cycle. The design parameters of the cycle are set up on the basis of the component technologies of today's state-of-the-art gas turbines with a turbine inlet temperature between 1100°C and 1700°C. The optimal pressure ratio ranges for the considered turbine inlet temperatures are identified and a comparison with existing evaluations is made. For the optimal initial parameters E-MATIANT net efficiency varies from 42.0 to 49.8% without considering turbine cooling. An influence of additional reheat in combustor chamber on cycle efficiency was identified. Two turbine cooling schemes are proposed. The maximum net efficiency of E-MATIANT cycle, which is equal to 44.0%, is obtained for turbine inlet temperature equal to 1400°C and turbine inlet pressure equal to 40 bar taking into account turbine cooling. An influence of water injection in coolant flow on cycle efficiency was estimated. The performance penalty due to the oxygen production and carbon dioxide capture is examined.
以提高发电效率为目的的全氧燃烧循环的结构和参数研究
本研究旨在介绍E-MATIANT循环的热力学分析和优化结果。循环的设计参数是根据当今最先进的燃气轮机的组件技术建立的,涡轮进口温度在1100°C到1700°C之间。确定了考虑的涡轮进口温度的最佳压力比范围,并与现有的评估进行了比较。在不考虑涡轮冷却的情况下,对于最优初始参数E-MATIANT的净效率在42.0 ~ 49.8%之间变化。确定了燃烧室附加再热对循环效率的影响。提出了两种涡轮冷却方案。考虑涡轮冷却,当涡轮进口温度为1400℃,涡轮进口压力为40 bar时,E-MATIANT循环的最大净效率为44.0%。分析了冷却液流动中注水对循环效率的影响。研究了由于氧气产生和二氧化碳捕获造成的性能损失。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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