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DOI:
燃气轮机技术:2018,31(2):29-36
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小型燃气轮机CCHP系统变工况性能入口加热调控研究
(1.中国联合重型燃气轮机技术有限公司,北京 102209;2.中国科学院工程热物理研究所,北京 100190)
Effect of the Inlet Air Heating on Part Load Performance of a Combined Cooling,Heating and Power (CCHP) System Driven by the Small Scale Gas Turbine
(1.China United Gas Turbine Technology Corporation, Beijing 102209, China;2.Insititute of Engineering Thermophysics, Chinese Academy of Science, Beijing 100190, China)
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中文摘要: 提出了一种利用冷热电联产系统(CCHP)低温烟气与环境空气混和加热控制压气机人口温度,提升燃气轮机冷热电系统变工况性能的方法,并以1.9 MW小型燃气轮机0PRA16为例,建立了CCHP系统模型,分析了调控方法的效果、机理。结果表明,人口混和加热可以有效改善冷热电联产系统变工况下系统性能,并扩展系统节能运行范围。与传统燃料流量调控方法相比,新型调控手段下夏季制冷与冬季供热模式下系统节能率分别提升5.7%和21.6%。
Abstract:The combined cooling, heating and power ( CCHP) system driven by a small scale gas turbine is a booming new technology for efficient and clean production of energy. However, because of the fluctuations in the energy demand, the CCHP system frequently runs under off design points, especially under part load conditions, which results in performance deterioration. This paper presents a novel power regulation method of compressor inlet air heating for the part load operation of the CCHPsystem. The novel method is performed b' recirculating a fraction of the low temperature exhaust gas to the inlet of the gas turbine and thereby adjusting the inlet air temperature. Amathematical model of the CCHP system was set up, of which the small scale gas turbine OPRA16 simulation was implemented using the GateCycle software and calibrated by the real gas turbine data. The part load performance of the CCHP system by the novel power reduction method was compared with the conventional fuel flow method systematical implemented on most engines. Analysis results showthat the Fuel Energy Saving Ratio ( FESR) was enhanced by 5.1% point in summer and 21.6% point in winter. The conclusion can be drawn that the CCHP system in both summer and winter under the novel method achieves more energy saving than the conventional power reduction method.
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[2]KIM K M, PARK J S, DONG H L, et al. Analysis of conjugated heat transfer, stress and failure in a gas turbine blade with circular cooling passages[J]. Engineering Failure Analysis, 2011, 18(4):1212-1222.

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