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某超声速风洞测控系统

高川 刘烽 周波 周润 喻波

兵工自动化Issue(2):63-66,70,5.
兵工自动化Issue(2):63-66,70,5.DOI:10.7690/bgzdh.2013.02.018

某超声速风洞测控系统

Measure and Control System of the Supersonic Wind Tunnel

高川 1刘烽 1周波 1周润 1喻波1

作者信息

  • 1. 中国空气动力研究与发展中心高速所,四川 绵阳 622661
  • 折叠

摘要

Abstract

Aiming at the characteristics of large-scale intermittent type supersonic wind tunnel, designs measure and control system for the certain type supersonic wind tunnel. Introduces the general design of the system, key technical applying as general cascade pressure control, redundancy control of attack angle equipment, OPC, etc. and relate technical targets of subsystems, analyzes control mode of the wind tunnel running, gives results of the first term flow field calibration test and standard model test. The results show that the system can realize the design requirement of control dispersing node, concentrate command and dispatch, accurate measurement of signal collecting. It also has high automation level and expending ability and is easy to be domestic development.

关键词

超声速风洞/现场总线/测量系统/控制系统

Key words

supersonic wind tunnel/filed bus/measure system/control system

分类

军事科技

引用本文复制引用

高川,刘烽,周波,周润,喻波..某超声速风洞测控系统[J].兵工自动化,2013,(2):63-66,70,5.

兵工自动化

OACSTPCD

1006-1576

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