西门子能源SGT-300-2S干式低排放燃烧系统燃料灵活性的扩展

Phill Hubbard, Jadeed Beita, Kexin Liu, S. Sadasivuni, G. Bulat
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摘要

为了评估西门子能源SGT-300-2S干式低排放(DLE)燃烧系统在各种发动机负载和环境条件下的燃油灵活性,在高压燃烧台上进行了测试。燃料热值的变化,在标准条件下,Wobbe指数(WI)分别为23 MJ/Sm3, 25 MJ/Sm3, 27.5 MJ/Sm3, 30 MJ/Sm3和45 MJ/Sm3(英国天然气),在混合厂通过将天然气与二氧化碳作为稀释剂混合获得。排放、燃料压力、燃烧动力学以及通过测量燃烧器和燃烧器金属温度进行的闪回监测是评估燃料柔韧性对燃烧器性能影响的主要参数。试验结果表明,由于MCV(中等热值)燃料的绝热火焰温度较低,燃料热值降低,NOx排放减少。CO排放性能不受影响。然而,燃料热值的降低导致需要增加燃料供应压力,从而提高燃料的体积流量,以达到燃气轮机的热输入要求。发现不同燃料成分的燃烧动力学特性是相似的。通过测量过渡管道出口处的燃烧热气体温度分布,研究了燃油热值变化对涡轮喷管导叶和叶片的影响。结果表明,在最高温度和模式因子方面,涡轮入口温度分布没有显著变化。成功的开发项目扩大了SGT-300-2S标准生产DLE燃烧器的能力,使其能够在WI范围为25 MJ/Sm3至49 MJ/Sm3的燃料范围内运行。在SGT-300-2S燃烧系统上获得的试验结果为工业燃气轮机燃烧器燃料灵活性设计提供了重要经验。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Extension of Fuel Flexibility for Siemens Energy SGT-300-2S Dry Low Emission Combustion System
This paper reports the results of high-pressure combustion rig testing carried out to assess the fuel flexibility of the standard Siemens Energy SGT-300-2S dry low emission (DLE) combustion system operated at engine conditions across a wide range of engine loads and ambient conditions. Variations of the fuel heating value, with Wobbe Index (WI) of 23 MJ/Sm3, 25 MJ/Sm3, 27.5 MJ/Sm3, 30 MJ/Sm3 and 45 MJ/Sm3 (UK natural gas) at standard conditions1, were achieved in a mixing plant by blending natural gas with CO2 as diluent. Emissions, fuel pressure, combustion dynamics, and flashback monitoring via measurement of burner and combustor can metal temperatures were the main parameters used to assess the effect of fuel flexibility on combustor performance. Test results show that NOx emissions decrease as the fuel heating value is reduced due to lower adiabatic flame temperatures for the MCV (Medium Calorific Value) fuels. CO emissions performance was found to be unaffected. However, decreasing fuel heating value leads to a requirement to increase the fuel supply pressure as a consequence of higher volumetric fuel flow rate to achieve the heat input requirements of the gas turbine. Combustion dynamics characteristics were found to be similar for the different fuel compositions. The impact of fuel heating value change on turbine nozzle guide vanes and blades was also investigated by measuring the combustion hot gas temperature profile at the exit of transition duct. The results show that there is no significant change in turbine entry temperature profile in terms of maximum temperature and pattern factors. The successful development program has expanded the capability of the SGT-300-2S standard production DLE combustor to operate with a range of fuels covering a WI range of 25 MJ/Sm3 to 49 MJ/Sm3. The test results obtained on the SGT-300-2S combustion system provide significant experience for industrial gas turbine burner design for fuel flexibility.
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