摘要
The axial turbine is a critical component of the supercritical carbon dioxide (sCO2) cycle system, where fast and accurate off-design performance prediction is essential for improving system optimization and design efficiency. This paper presents a one-dimensional calculation method for real gas turbines. The method introduces a detailed computational preprocessing approach to handle blade choking, enabling rapid determination of the turbine's choked state and accurate performance prediction under both off-design and choked conditions. Validation was conducted using two air turbines and two sCO2 turbines, including published literature data and experimental data. The results show that the method achieves high accuracy, with a maximum relative error of 0.3% for choking mass flow prediction and efficiency prediction errors consistently below 3%. Additionally, the proposed method significantly enhances computational efficiency, reducing the calculation time for 30 operating points on a characteristic curve to 5.6% of that required by traditional methods. This method provides a reliable and efficient tool for the design and optimization of real gas turbines.
| 源语言 | 英语 |
|---|---|
| 文章编号 | 125414 |
| 期刊 | Applied Thermal Engineering |
| 卷 | 264 |
| DOI | |
| 出版状态 | 已出版 - 1 4月 2025 |
指纹
探究 'Mean-line prediction for sCO2 axial turbine performance characteristics using a novel method for critical state quick judgement' 的科研主题。它们共同构成独一无二的指纹。引用此
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