摘要
主要介绍ROTAX航空发动机914UL/F基本参数、结构特点、性能和应用的领域,并对结构设计参数和强化指标进行了分析,从而将有助于这款活塞式航空发动机在国内轻型飞机上的应用。
This paper mainly introduces the basic parameters, characteristics of structure, performance and application fields of aircraft engine ROTAX 914UL/F. The structure design parameters and intensifying indexes are analyzed. It will be helpful to the application of this aircraft piston engine in the domestic light aircraft.
出处
《小型内燃机与摩托车》
CAS
2014年第5期88-91,共4页
Small Internal Combustion Engine and Motorcycle
基金
天津市重大科技专项(13ZCZDGX04400)
