Dynamic characteristics of the sCO<sub>2</sub> recompression Brayton cycle for aerodynamic heat recovery of long-duration high-speed aircraft

<p indent="0mm">Aerodynamic heat protection and the efficient recovery and utilization of thermal energy represent significant challenges for long-duration, high-speed flight vehicles. This study introduces a novel approach utilizing a supercritical carbon dioxide (sCO<sub>2</sub>) Brayton cycle to recover and harness aerodynamic heat, thereby achieving dual objectives of thermal protection and power generation. A dynamic thermal-to-work conversion model of the sCO<sub>2</sub> Brayton cycle for aerodynamic heat recovery has been developed. The system’s dynamic operational characteristics and the interactions among key components are evaluated using metrics such as temperature, pressure, thermal efficiency, and net power output. Research findings indicate that the sCO<sub>2</sub> Brayton cycle system holds considerable promise for engineering applications in high-speed aircraft aerodynamic heat recovery. Under varying aerodynamic heat flux conditions, the cycle exhibits nonlinear dynamic behavior and overshoot phenomena. Increasing the temperature difference in the regenerator’s heat exchange process can effectively mitigate the system’s thermal inertia.

Authors

Publication Details

Journal
Scientia Sinica Technologica
Published
2025-03-17
DOI
https://doi.org/10.1360/sst-2024-0308
Primary Topic
Thermodynamic and Exergetic Analyses of Power and Cooling Systems
Type
article
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article

Dynamic characteristics of the sCO&lt;sub&gt;2&lt;/sub&gt; recompression Brayton cycle for aerodynamic heat recovery of long-duration high-speed aircraft

Fei Gao, Wenqing Lai, Chengbin Zhang
Scientia Sinica Technologica
Thermodynamic and Exergetic Analyses of Power and Cooling Systems
article

Dynamic characteristics of the sCO&lt;sub&gt;2&lt;/sub&gt; recompression Brayton cycle for aerodynamic heat recovery of long-duration high-speed aircraft

Fei Gao, Wenqing Lai, Chengbin Zhang
article en

Abstract

<p indent="0mm">Aerodynamic heat protection and the efficient recovery and utilization of thermal energy represent significant challenges for long-duration, high-speed flight vehicles. This study introduces a novel approach utilizing a supercritical carbon dioxide (sCO<sub>2</sub>) Brayton cycle to recover and harness aerodynamic heat, thereby achieving dual objectives of thermal protection and power generation. A dynamic thermal-to-work conversion model of the sCO<sub>2</sub> Brayton cycle for aerodynamic heat recovery has been developed. The system’s dynamic operational characteristics and the interactions among key components are evaluated using metrics such as temperature, pressure, thermal efficiency, and net power output. Research findings indicate that the sCO<sub>2</sub> Brayton cycle system holds considerable promise for engineering applications in high-speed aircraft aerodynamic heat recovery. Under varying aerodynamic heat flux conditions, the cycle exhibits nonlinear dynamic behavior and overshoot phenomena. Increasing the temperature difference in the regenerator’s heat exchange process can effectively mitigate the system’s thermal inertia.

Scientia Sinica TechnologicaVol. 55(10)
Openalex Percentile: Top 95%
Thermodynamic and Exergetic Analyses of Power and Cooling Systems
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