中国大型飞机发动机研制中的关键技术  

Key technologies of high bypass ratio engine in China

作　　者：张德志[1] 

机构地区：[1]沈阳发动机设计研究所,沈阳110015

出　　处：《中国民航大学学报》2008年第5期26-28,共3页Journal of Civil Aviation University of China

摘　　要：简要论述了中国研制大涵道航空发动机的部分关键技术,以期对中国具有自主知识产权的大涵道比发动机研制工作提供参考。As China＇s airplane project to start, the development of aero-engine with high bypass ratio is also on the agenda. Aero-engine technology is one of the key technologies which is must given the development priority, tight blockade and high degree of monopoly in few developed countries. Not to develop aero-engine with high bypass ratio, there will be no independence, integrity and a strong driving force for the aviation industry, and the independent innovation strategy will not be able to achieve. This paper discusses the key technologies of the high bypass ratio engine with a view to provide a reference to the development.

关 键 词：大型飞机 大涵道比发动机 关键技术 

分 类 号：V263[航空宇航科学与技术—航空宇航制造工程]