航空发动机加力状态最小油耗优化控制

推进技术 ›› 2005, Vol. 26 ›› Issue (6): 552-555.

航空发动机加力状态最小油耗优化控制

孙丰诚,孙健国

南京航空航天大学能源与动力学院江苏南京210016;南京航空航天大学能源与动力学院江苏南京210016

发布日期:2021-08-15
基金资助:
航空科学基金资助项目(00C52030);博士点基金资助项目(2000028701)

Optimization control of minimum fuel consumption at aero-engine afterburning condition

Nanjing Univ.of Aeronautics and Astronautics,Nanjing 210016,China;Nanjing Univ.of Aeronautics and Astronautics,Nanjing 210016,China

Published:2021-08-15

摘要/Abstract

摘要： 分析了发动机加力状态燃油消耗的特点,利用主燃烧室燃烧效率远大于加力燃烧室燃烧效率的特点,将性能寻优控制中的最小油耗模式扩展至加力状态。用线性规划(L inear Programm ing)算法进行发动机性能寻优。进行了加力状态最小油耗模式的数字仿真实验,仿真结果表明在加力状态应用最小油耗模式,可以使单位耗油率减少5%~7%,其效益远高于非加力状态的最小油耗模式,具有明显的实际应用价值。

关键词: 涡扇发动机;线性规划;加力状态;性能优化

Abstract: The characteristic of fuel consumption at aero-engine afterburning condition was analyzed.Based on the fact that the efficiency of main combustor is higher than that of the afterburner,this article puts minimum fuel consumption mode into use at aero-engine afterburning condition.Linear Programming was used to optimize the aero-engine performance.Digital simulations show that the specific fuel consumption was decreased by 5%~7%.The benefit of minimum fuel consumption mode at afterburning condition is much more than that of non-afterburning condition.It has great application potential in engineering.

Key words: Turbofan engine;Linear programming;Afterburning condition;Performance optimization

孙丰诚,孙健国. 航空发动机加力状态最小油耗优化控制[J]. 推进技术, 2005, 26(6): 552-555.