EXPERIMENTAL INVESTIGATION OF ROTOR PASSAGE LOSS IN S-CO2 RADIAL TURBINE

被引:0
|
作者
Lee, Seungkyu [1 ]
Lee, Jeong Ik [1 ]
Kim, Gihyeon [1 ]
Baek, Jeong Yeol [1 ]
机构
[1] Korea Adv Inst Sci & Technol, Daejeon, South Korea
来源
PROCEEDINGS OF ASME TURBO EXPO 2024: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, GT2024, VOL 11 | 2024年
关键词
S-CO2; Turbomachinery; Inflow Radial Turbine; Rotor Passage Loss; Experimental Performance Map; Nuclear Power Cycle;
D O I
暂无
中图分类号
TE [石油、天然气工业]; TK [能源与动力工程];
学科分类号
0807 ; 0820 ;
摘要
This paper presents an experimental investigation of rotor passage loss in an S-CO2 radial turbine. It addresses the need to adapt existing design methodologies for S-CO2 turbomachinery due to its distinct physical behavior compared to ideal gas turbomachinery. This study involves selecting and calibrating existing rotor passage loss models, crucial for determining the pressure ratio and efficiency of a radial turbine. An S-CO2 Turbine-Alternator-Compressor (TAC) in KAIST is utilized for empirical measurements, leading to the calibration of existing Balje's rotor passage loss model. The paper highlights the uniqueness of S-CO2 turbomachinery and contributes to the understanding and improvement of their design and operation.
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页数:9
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