高超声速风洞引射器阀门系统的微机控制  

THE MICROCOMPUTER CONTROL OF INJECTOR VALVE SYSTEM OF HYPERSONIC WIND TUNNEL

作　　者：张福香[1] 王际敏[1] 

机构地区：[1]中国空气动力研究与发展中心

出　　处：《气动实验与测量控制》1994年第1期60-65,共6页

摘　　要：本文介绍了高超声速风洞引射器阀门系统采用计算机控制的设计思想和原理框图。在软件和硬件设计过程中采取了一系列措施，成功地在风洞中实现了微机实时控制．The design concept and principle of injector valve system of hypersonic wind tunnel controlled by the computer are introduced in this paper. In order to apply the technique of microcomputer controlling to the wind tunnel successfully, a series of measures have been taken in the process of designing software and hardware. Now, the real-time control of the injector valve system of the wind tunnel has been realized.

关 键 词：高超声速风洞 阀门 计算机控制 

分 类 号：V211.74[航空宇航科学与技术—航空宇航推进理论与工程]