首页|船舶燃气轮机冷却风机压头对排气引射系统流场特性的影响

船舶燃气轮机冷却风机压头对排气引射系统流场特性的影响

扫码查看
为了解决船舶燃气轮机在恶劣工况下冷却空气进气量较少的问题,以船舶燃气轮机完整排气引射系统为研究对象,采用标准k-ε模型模拟计算,分析了风机压头为0 Pa基准工况下的流场特性和温度分布特性,在此基础上探索了开启冷却风机后不同风机压头对排气引射系统流场特性的影响.研究表明:基准工况时无量纲出口温度为0.515 0,而当风机压头为200 Pa时无量纲温度为0.509 9,与基准工况对比,箱装体冷却进气质量流量随压力阶跃的增加而增加,冷却进气量增加使混合管道内的温度更加均匀、局部高温区更小、出口温度更低;在研究条件下,随着风机压头的提升,排气引射系统的总引射量和总引射系数也相应提高,在1 500 Pa工况下达到最大值,相较于基准工况,总引射系数提高了 17.2%;喷管进口的总压和静压均会随着压头增加而增大,排气引射系统出口温度持续降低,在阶跃压力从200 Pa增加到1 500 Pa的过程中,无量纲温度从0.509 9下降到0.477 1.
Effect of Cooling Fan Pressure Head on Flow Field Characteristics of Exhaust Ejector System of Marine Gas Turbine
In order to solve the problem of low cooling air intake of marine gas turbine under severe con-dition,the standard k-ω model was used to simulate the integrated exhaust ejector system of marine gas turbine and analyze the flow field characteristics and temperature distribution characteristics at the 0 Pa head under the baseline condition,on the basis of which,the effect of different fan pressure heads on the flow field characteristics of the exhaust ejector system after turning on the cooling fan was explored.The results show that the dimensionless outlet temperature is 0.515 0 under the baseline condition,while it is 0.509 9 at the 200 Pa head.Compared with the baseline condition,the case module cooling inlet mass flow rate increases with the increase of pressure step,which makes the temperature in the mixed pipe more uniform,the local high temperature zone smaller and the outlet temperature lower.Under the current study conditions,with the increase of the fan pressure head,the total mass entrainment and the total mass entrainment ratio of the exhaust ejector system also increase,reaching the maximum value at 1 500 Pa.Compared with the baseline condition,the total mass entrainment ratio increases by 17.2%;the total and static pressures of the nozzle inlet increase with the increase of the pressure head,and the outlet tempera-ture of the exhaust ejector system continues to decrease,and the dimensionless temperature decreases from 0.509 9 to 0.477 1 when the pressure step increases from 200 Pa to 1 500 Pa.

marine gas turbineexhaust ejector systemflow field characteristicsnumerical simulation

杨福正、刘宇骁、柴运强、吴轩

展开 >

中国船舶集团有限公司系统工程研究院,北京 100094

船舶燃气轮机 排气引射系统 流场特性 数值模拟

2024

热能动力工程
中国 哈尔滨 第七0三研究所

热能动力工程

CSTPCD北大核心
影响因子:0.345
ISSN:1001-2060
年,卷(期):2024.39(6)
  • 2