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New Dry Low Nox Combustor for Mitsubishi M501/701G

机译:适用于MITSUBISHI M501 / 701G的新型干燥低NOx燃烧器

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MHI G class gas turbine was designed to operate with a Turbine Inlet Temperature (TIT) of 1500 °C. 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类燃气轮机设计用于1500℃的涡轮入口温度(山雀)。这种升高的温度导致高热效率,但也可以诱导相对高的排放。 MHI开发了一种新的干燥低Nox(DLN)燃烧器,可提高这种级联涡轮机符合世界各地的严格环境规则。除了针对具有较低排放的环保燃烧器外,重新设计的DLN燃烧器还提高了稳定性率。可验证测试在新的DLN燃烧器中,在2005年5月至2007年5月至2007年5月的MHI的T点组合循环发电厂的MHI燃气轮机中进行。除了验证较低的排放水平之外,这些测试还证实了宽敞的运行余量以及组件的可靠性和耐用性。新设计经过优化,以改装为现有的G类引擎。燃烧器现在处于批量生产,作为MHI的标准燃烧器。本文介绍了用于新燃烧器的设计过程,包括计算流体动力学(CFD)和所使用的其他分析工具。

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