| Citation: | ZHAO Weiwei, LOU Decang, ZHONG Shilin. Performance evaluation method of thermal management system based on exergy analysis and compensatory loss[J]. Journal of Aerospace Power, 2023, 38（12）：2829-2836 doi: 10.13224/j.cnki.jasp.20220121
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A method based on exergy analysis and compensatory loss was put forward to evaluate the performance of aero-engine thermal management system. Different thermal management system schemes were compared and analyzed from the perspectives of thermodynamic performance and total takeoff weight added value. According to the established analysis method, the performance of two schemes of engine compartment thermal management system (direct air bleed and bleed after pump) was comprehensively evaluated. The results showed that the scheme of the heat management system of the air intake after the pump can realize comprehensive utilization of the power extraction and cooling, and reduce the aerodynamic resistance loss caused by the whole air intake, which was better than the scheme of the direct air intake, as the maximum exergy efficiency was increased by 12.3%, and the total mass of take-off was reduced by 233.7 kg. Therefore, the comprehensive performance of the heat management scheme after pumping was better than that of direct air intake scheme. This method can provide a reference for the performance evaluation of other similar system schemes.
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