Dynamic characteristics analysis of supercritical CO2 closed Brayton power generation system for hypersonic vehicles

IF 6.9 2区 工程技术 Q2 ENERGY & FUELS Applied Thermal Engineering Pub Date : 2025-02-22 DOI:10.1016/j.applthermaleng.2025.126016
Lei Lang , Fangyan Jiang , Kunlin Cheng , Zhijie Liu , Song Wang , Chaolei Dang , Jiang Qin , Hongyan Huang , Xin Zhang
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Abstract

Supercritical CO2 closed Brayton cycle (SCO2CBC) has great application potential in the field of airborne power generation (APG) for hypersonic vehicles due to its high power-to-weight ratio and high thermal efficiency. Owing to the complex thermophysical properties of SCO2 in CBC and considering the unique limited cold source environment on hypersonic vehicles, the dynamic cycle law of the SCO2CBC APG system remains unknown. In this context, this paper constructs the dynamic model of the SCO2CBC APG system for hypersonic vehicles and validates the key components and systems. On this basis, the main dynamic process and control effect in the cycle process are simulated and analyzed. Finally, the dynamic operating characteristics and the coupling influence law among the main components are determined through sensitivity analysis. The results demonstrate that the dynamic response of the system to the decrease in the power of the wall cooling channel is noticeably slower than that to the increase in the power. Furthermore, the system is more sensitive to the flow of cooling fuel than to temperature of cooling fuel. The designed SCO2 dynamic regulation module can effectively adjust the fluctuation range of compressor inlet pressure in the load reduction process, and ensure the efficient and stable operation of the cycle, but the control range of the pressure threshold should not be too low. Among all the system components, the recuperator is the most sensitive to the change in the power of the wall cooling channel, while the compressor is the most sensitive to the dynamic response of cooling fuel flow and temperature disturbance. The above conclusions can provide necessary theoretical support for the performance evaluation, dynamic regulation, and variable condition design of the APG system of hypersonic vehicles.
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高超声速飞行器超临界CO2闭式布雷顿发电系统动态特性分析
超临界CO2闭式布雷顿循环(SCO2CBC)由于其高功率重量比和高热效率,在高超声速飞行器机载发电领域具有很大的应用潜力。由于CBC中SCO2复杂的热物理性质和高超声速飞行器上独特的有限冷源环境,SCO2CBC APG系统的动态循环规律尚不清楚。在此背景下,本文构建了高超声速飞行器SCO2CBC APG系统的动态模型,并对关键部件和系统进行了验证。在此基础上,对循环过程中的主要动态过程和控制效果进行了仿真分析。最后,通过灵敏度分析确定了系统的动态工作特性和主要部件之间的耦合影响规律。结果表明,系统对壁面冷却通道功率减小的动态响应明显慢于对壁面冷却通道功率增大的动态响应。此外,该系统对冷却燃料的流量比冷却燃料的温度更敏感。所设计的SCO2动态调节模块可有效调节减载过程中压缩机进口压力波动范围,保证循环高效稳定运行,但压力阈值控制范围不能过低。在所有系统部件中,回热器对壁面冷却通道功率变化最为敏感,而压缩机对冷却燃料流量和温度扰动的动态响应最为敏感。上述结论可为高超声速飞行器APG系统的性能评估、动态调节和变工况设计提供必要的理论支持。
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来源期刊
Applied Thermal Engineering
Applied Thermal Engineering 工程技术-工程:机械
CiteScore
11.30
自引率
15.60%
发文量
1474
审稿时长
57 days
期刊介绍: Applied Thermal Engineering disseminates novel research related to the design, development and demonstration of components, devices, equipment, technologies and systems involving thermal processes for the production, storage, utilization and conservation of energy, with a focus on engineering application. The journal publishes high-quality and high-impact Original Research Articles, Review Articles, Short Communications and Letters to the Editor on cutting-edge innovations in research, and recent advances or issues of interest to the thermal engineering community.
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