摘要
研究了民用飞机涡扇发动机短舱内的通风冷却系统,介绍了通风冷却系统的设计方案,提出了通风冷却系统的设计要求和设计内容,给出了通风冷却系统的验证思路。
The nacelle wind cooling system for civil aircraft is studied,and the system scheme of wind cooling system is introduced.The design requirement and design contents of the wind cooling system are proposed.Finally,the verification method for the wind cooling system is put forward.
出处
《工程与试验》
2015年第3期92-94,共3页
Engineering and Test
关键词
通风冷却系统
系统方案
设计要求
验证思路
wind cooling system
system scheme
design requirement
verification method
