变海拔下两级空压机气动性能严重下降,无法满足高功率密度燃料电池的动态需求,为拓宽两级空压机工作极限,采用数值模拟方法研究典型工况下的气动性能。结果表明:随着进气压力的降低,两级空压机压比降低32.73%,等熵效率降低34.60%;随着进气温度的升高,两级空压机压比升高23.27%,等熵效率降低12.76%;随着空压机转速的增大,两级空压机压比升高145%,等熵效率先升高后下降,在设计转速附近达到最大值,为66.83%。
Abstract
The aerodynamic performance of a two-stage air compressor under variable altitude is severely degraded and cannot meet the dynamic demands of high-power-density fuel cells. In order to broaden the working limit of the two-stage air compressor, numerical simulation was used to study the aerodynamic performance under typical working conditions. The results show that: with the decrease of inlet pressure, the pressure ratio of the two-stage air compressor decreases by 32.73%, and the isentropic efficiency decreases by 34.60%; with the increase of inlet temperature, the pressure ratio of the two-stage air compressor increases by 23.27%, and the isentropic efficiency decreases by 12.76%; with the increase of rotational speed, the pressure ratio of the two-stage compressor increases by 145%, and the isentropic efficiency increases first and then decreases, reaching a maximum value of 66.83% near the design speed.
关键词
离心空压机 /
燃料电池 /
叶轮 /
数值模拟 /
气动性能 /
变海拔
Key words
centrifugal compressors /
fuel cells /
impellers /
numerical simulation /
aerodynamic performance /
variable altitude
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基金
国家自然科学基金(52305257); 天津市科技计划(22JCQNJC00110); 河北省自然科学基金(E2023202168)