摘要
本文在聚氧提高航机部件性能，总体性能的研究基础上，进一步探索航空发动机聚氯减重的规律，提供聚氧缩短压气机、燃烧室、涡沦轴向尺寸、减少发动机直径、减轻上述核心机部件和发动机总重量的理论依据，可供航机预研参考。
This paper goes a step fuitbcr to Study the effect on reducing aeroengine weight by oxygen Concentration in the air passing through the Compressor The oxygen concentration is notonly a new way to improve the performance of aeroengine based on early work, and also shorten the axial length of compressor, combustor and turbine moreorer decrease diameter of engine. So the total weight of the core can be reduced. The principle of reducing engine weight are discussed in this paper
出处
《沈阳航空工业学院学报》
1997年第4期7-12,共6页
Journal of Shenyang Institute of Aeronautical Engineering
基金
航空科学基金
