摘要
介绍了一种基于 VXI总线的航空发动机进气压力畸变测控系统。在高速采集的同时 ,实现了数据的不间断存储、多种实时显示、综合畸变指数 W的实时计算。
An aero engine inlet pressure distortion measurement and control system based on VXI bus is introduced in this paper.The data continuous store,the real time multi display and the real time calculation of composite distortion factor W have been realized at the same time of high speed acquisition.The functions of this system have been validated through experiment.
出处
《航空计测技术》
2002年第6期16-20,共5页
Aviation Metrology & Measurement Technology
基金
本课题 2 0 0 2年 3月获军队科技进步一等奖
