摘要
介绍了油雾润滑技术的基本原理。分析探讨了国外两种微型涡轮喷气发动机的油雾润滑系统。针对自行设计的推力为58.8N、长时间使用的涡轮喷气发动机的油雾润滑系统提出了初步方案,分析和计算表明,这种方案是可行的。
The principle of oil mist Irbrication was introduced in this paper. Oil mist lubrication system of two toreign turbojet engines were analyzed and discussed. A inirial scheme of a oil mist oubrication system was put forward, which was used in a turbojet engine designed by ourselves. The engine's thrust is 6 kilograms and can be used in longtime. It was indicated from analysis and calculation that the scheme is feasible.
出处
《润滑与密封》
CAS
CSCD
北大核心
2003年第4期87-89,共3页
Lubrication Engineering
基金
西北工业大学首届青年科技创新基金
