摘要
详细分析了部件老化对发动机性能影响的机理.利用所能得到的统计数据,基于部件匹配技术,通过将考虑部件老化影响的部件特性嵌入到发动机稳态性能计算模型中,建立了考虑部件老化的发动机性能计算模型,采用Newton-Raphson迭代收敛技术求解非线性方程组,获得考虑部件老化影响的发动机性能.以某型涡扇发动机为例,定量地计算分析了部件老化对发动机性能的影响,计算结果和发动机实际试车数据对比具有较好的一致性,表明本文发展的方法是合理的.
The effect of component deterioration on engine performance is considerable. This influence can not be easily computed with normal engine steady performance computer program. A new mathematical method and computer program were developed to accurately compute the effect of component deterioration on engine performance. First, the mechanisms of the effect of component deterioration on engine performance were analyzed; then, statistical method was used to calculate this influence. Taking a turbofan engine as an example, the effect of component deterioration on engine performance,such as specific fuel consumption and temperature at turbine inlet was computed with this method, and compared with experimental data. The results indicate that the mathematical model in this paper can be used to compute the effect of component deterioration on engine performance.
出处
《航空动力学报》
EI
CAS
CSCD
北大核心
2007年第5期792-796,共5页
Journal of Aerospace Power
关键词
航空、航天推进系统
涡扇发动机
部件老化
性能损失
aerospace propulsion system
turbofan engine
component deterioration
performance loss