摘要
ＷＪ９是我国第一台按适航条例研制的涡桨发动机。本文阐述了该机的研制概况，总体结构和技术性能；介绍了压气机、燃气发生器、涡轮、减速器等部件先进的结构设计和制造技术。
WJ9 is the first domestic turboprop engine developed according to CCAR33. This paper introduces its development, total structure and performances, and discusses the structure design and manufacture technology of its components such as compressor,turbine and reducing gears.
出处
《航空制造工程》
1997年第9期14-15,18,共3页
Aviation Engineering & Maintenance
