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轴驱动升力风扇发动机稳态性能仿真模型研究
Steady performance mathematical model of a turbofan engine with the shaft-driven lift-fan
【摘要】 以常规混排涡扇发动机性能模型为基础,结合升力系统工作原理,并以推力比为控制目标,建立了轴驱动升力风扇发动机稳态性能仿真数学模型。根据此模型编制了轴驱动升力风扇发动机整机稳态性能计算软件,并以轴驱动升力风扇发动机的三种工作状态为例进行了计算分析。结果表明,该模型软件逻辑正确,计算精度满足后续研究需要,为轴驱动升力风扇发动机性能分析及控制规律研究提供了必要的技术基础。
【Abstract】 Based on a conventional turbofan steady performance mathematical model, and combined withthe working principle of the lifting system, steady performance mathematical model of a turbofan enginewith the shaft-driven lift-fan was built with thrust ratio as a control target. According to this model, steadyperformance simulation software was compiled and calculation analysis was carried out on three typicalworking conditions. The calculation findings suggest that the procedure of the software is logically accurate,and the precision of the calculation will satisfy the further research. It provides the foundation for the perfor-mance analysis and control law design of shaft-driven lift-fan turbofan.
【Key words】 aero-engine; lift-fan; VTOL; mathematical model; F-35B; F135-PW-600;
- 【文献出处】 燃气涡轮试验与研究 ,Gas Turbine Experiment and Research , 编辑部邮箱 ,2018年03期
- 【分类号】V235.13
- 【下载频次】147