摘要
综述了CFM56系列大涵道比发动机在风扇叶片、防冰、吞水、燃烧室、尾喷管方面所采用的结构技术。
The structure technologies of fan blades, anti-ice,water ingestion, combustor and exhaust nozzle for the CFM56 series high-bypass ratio turbofan engine were reviewed.
出处
《航空发动机》
2010年第4期57-60,36,共5页
Aeroengine