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DEVELOPMENT OF THE SUPERCRITICAL CARBON DIOXIDE POWER CYCLE EXPERIMENTAL LOOP IN KIER

机译:基尔超临界二氧化碳动力循环实验环的研制

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Three supercritical carbon dioxide (CO_2) power cycle experimental loops have been developed in Korea Institute of Energy Research (KIER) from 2013. As the first step, a 10 kWe-class simple un-recuperated Brayton power cycle experimental loop was designed and manufactured to test its feasibility. A 12.6 kWe hermetic turbine-alternator-compressor (TAC) unit which is composed of a centrifugal compressor, a radial turbine and the gas foil bearings was manufactured. The turbine inlet design temperature and pressure were 180 °C and 130 bar, respectively. Preliminary operation was successful at 30,000 RPM which all states of the cycle existed in the supercritical region. Second, a multi-purpose 1 kW-class test loop which operates as a transcritical cycle at a temperature of 200 °C was developed to concentrate on the characteristics of the cycle, control and stability issues of the cycle. A high-speed turbo-generator was developed which is composed of a radial turbine with a partial admission nozzle and the commercial oil-lubricated angular contact ball bearings. Finally, a 60 kWe-class Brayton cycle is being developed which is composed of two turbines and one compressor to utilize flue-gas waste heat. As the first phase of development, a turbo-generator which is composed of an axial turbine, a mechanical seal and the oil-lubricated tilting-pad bearings was designed and manufactured.
机译:韩国能源研究所(KIER)从2013年开始开发了三个超临界二氧化碳(CO_2)功率循环实验回路。第一步,设计并制造了一个10 kWe级的简单非蓄能式布雷顿功率循环实验回路,用于测试其可行性。制造了一个12.6 kWe的密闭式涡轮发电机-压缩机(TAC)单元,该单元由离心压缩机,径向涡轮机和气箔轴承组成。涡轮机入口设计温度和压力分别为180°C和130 bar。初步运行在30,000 RPM下成功进行,该循环的所有状态都存在于超临界区域。其次,开发了一个多功能的1 kW级测试回路,该回路在200°C的温度下作为跨临界循环运行,以专注于循环的特性,循环的控制和稳定性问题。开发了一种高速涡轮发电机,该发电机由带有部分进气喷嘴的径向涡轮机和商用油润滑角接触球轴承组成。最后,正在开发一个60 kWe级的布雷顿循环,该循环由两台涡轮机和一台压缩机组成,以利用烟气余热。作为开发的第一阶段,设计并制造了由轴流式涡轮机,机械密封件和油润滑式可倾瓦轴承组成的涡轮发电机。

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