摘要
研究了基于在线可变压气机导叶角的涡轴发动机最小油耗优化控制.分析了压气机导叶角的变化对涡轴发动机的影响.提出了基于在线可变导叶角的涡轴发动机优化控制方法.最后,进行了涡轴发动机最小油耗优化控制的仿真实验.仿真结果表明通过调节压气机导叶角可以使单位功率耗油率降低3%~7%,具有实际应用价值.
The online optimization control of variable inlet guide vane was studied for minimum fuel consumption,and the effect of variable inlet guide vane on the turboshaft .engine was analyzed. Thus, an online optimization method based on variable inlet guide vane was proposed. At last,a simulation test was conducted for online optimization control of turboshaft engine, showing that the specific fuel consumption (SFC) will decreases by 3 %-7% with higher applicability.
出处
《航空动力学报》
EI
CAS
CSCD
北大核心
2007年第11期1930-1934,共5页
Journal of Aerospace Power
基金
国家自然科学基金(50576033)
航空支撑科技基金(04B52006)
关键词
航空
航天推进系统
可变导叶角
涡轴发动机
优化
aerospace propulsion system variable inlet guide vane turboshaft engine optimization