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New Dry Low Nox Combustor for Mitsubishi M501/701G

机译:三菱M501 / 701G的新型干式低氮燃烧器

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摘要

MHI G class gas turbine was designed to operate with a Turbine Inlet Temperature (TIT) of 1500 ℃. This elevated temperature results in high thermal efficiency but also can induce relatively high emissions. MHI has developed a new Dry Low Nox (DLN) combustor that improves this class turbine compliance with stringent environmental regulations imposed around world.In addition to targeting an environmentally friendly combustor with lower emissions, the redesigned DLN combustor also improves the stability margin.Verification tests of the new DLN combustor were conducted in a M501G1 gas turbine at MHI's T-Point Combined Cycle Power Plant from May, 2005 to March, 2007. In addition to verifying lower emission levels, these tests confirmed a wide stable operation margin as well as the reliability and durability of the components. The new design is optimized to be retrofitted into existing G class engines. The combustor is now in mass production as a MHI's standard combustor.This paper describes the design process applied for the new combustor, including the Computational fluid Dynamics (CFD) and other analytical tools used.
机译:MHI G级燃气轮机设计为在1500℃的涡轮进气温度(TIT)下运行。升高的温度导致较高的热效率,但也会引起较高的排放。三菱重工开发了新型干式低氮燃烧器(DLN),以符合世界各地严格的环境法规,提高了此类涡轮机的适应性。重新设计的DLN燃烧器除了针对具有较低排放量的环保型燃烧器外,还提高了稳定性裕度。 2005年5月至2007年3月,新的DLN燃烧器在MHI的T点联合循环发电厂的M501G1燃气轮机中进行了测试。除了验证较低的排放水平外,这些测试还确认了广泛的稳定运行余量以及组件的可靠性和耐用性。新设计经过优化,可改装到现有的G级发动机中。该燃烧器现已作为MHI的标准燃烧器投入量产。本文介绍了该新型燃烧器的设计过程,包括计算流体动力学(CFD)和使用的其他分析工具。

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