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LOW-EMISSION OPERATION OF AERODERIVATIVE GAS-TURBINE COMBUSTOR OVER A WIDE RANGE OF AMBIENT CONDITIONS

机译:在广泛的环境条件下,Aeroderivativative气涡轮机燃烧器的低排放运行

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摘要

The capabilities of controlling a low-emission combustor (LEC) over a wide range of ambient conditions are analyzed. The LES is intended for a GTU-16P gas turbine that is a derivative of the PS-90A aircraft engine by the UEC Aviadvigatel company. The LEC is of premix swirl stabilized type based on GTE-110 prototype. Its burner consists of pilot and main burners. The main burner has two fuel supply channels that allow controlling the quality of the air-fuel mixture. The low-emission operation range of the LEC can be extended to 70% load at negative ambient temperatures by bleeding air to the compressor inlet.
机译:分析了在宽范围的环境条件下控制低发射燃烧器(LEC)的能力。 LES用于GTU-16P燃气轮机,由UEC AVIADVIGATEL公司提供PS-90A飞机发动机的衍生物。 LEC是基于GTE-110原型的预混旋流稳定类型。它的燃烧器包括飞行员和主要燃烧器。主燃烧器有两个燃料供应通道,可允许控制空气燃料混合物的质量。 LEC的低排放操作范围可以通过在压缩机入口中出现空气来延伸到负环境温度的70%负载。

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