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某型涡扇发动机部件老化对性能影响的分析与计算
引用本文:王占学,刘增文,叶新农.某型涡扇发动机部件老化对性能影响的分析与计算[J].航空动力学报,2007,22(5):792-796.
作者姓名:王占学  刘增文  叶新农
作者单位:1. 西北工业大学,动力与能源学院,西安,710072
2. 海军航空兵驻西安航空发动机(有限)公司军事代表室,西安,710089
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.

关 键 词:航空、航天推进系统  涡扇发动机  部件老化  性能损失
文章编号:1000-8055(2007)05-0792-05
收稿时间:2006/4/10 0:00:00
修稿时间:2006年4月10日

Effect of component deterioration on turbofan engine performance
WANG Zhan-xue,LIU Zeng-wen and YE Xin-nong.Effect of component deterioration on turbofan engine performance[J].Journal of Aerospace Power,2007,22(5):792-796.
Authors:WANG Zhan-xue  LIU Zeng-wen and YE Xin-nong
Institution:School of Power and Energy, Northwestern Polytechnical University, Xi'an 710072, China;School of Power and Energy, Northwestern Polytechnical University, Xi'an 710072, China;Representative office of Navy Aviation Army in Xi'an Aeroengin(group) Ltd, Xi'an 710089, China
Abstract: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.
Keywords:aerospace propulsion system  turbofan engine  component deterioration  performance loss
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