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某型航空发动机试车测控系统

杨鲁峰 曾嵘 王敏华 陶文典

测控技术2012,Vol.31Issue(8):137-139,3.
测控技术2012,Vol.31Issue(8):137-139,3.

某型航空发动机试车测控系统

Measurement and Control System for ,an Aero-Engine Test Rig Running

杨鲁峰 1曾嵘 2王敏华 2陶文典2

作者信息

  • 1. 贯州黎阳航空动力有限公司,贵州平坝561102
  • 2. 贵州觊阳航空发动机有限公司,贵州平坝561102
  • 折叠

摘要

Abstract

A measurement and control system for an aero-engine test rig running is established based on virtual instrument technology, using PXI bus data acquisition system and PLC. A touch screen is used to instead of the traditional physical control panel, and the control interfaces can be automatically switched with the condition of the engine. The communication between the PLC, serial equipments and industrial control computers is realized with the TCP/IP Ethernet communication protocol, Many functions such as calibration of measurement parameters, data acquisition, monitor, analysis and processing, reports of test, and test process prompt, are realized by detailed analysis of the aero-engine running requirement. It is demonstrated that this system is flexible, stable and reliable, easy to operation and maintenance. It fully meets the requirement of the aero-engine test rig running.

关键词

航空发动机/试车/测控系统/PXI/PLC

Key words

aero-engine/ running/ measurement and control system/ PXI/ PLC

分类

航空航天

引用本文复制引用

杨鲁峰,曾嵘,王敏华,陶文典..某型航空发动机试车测控系统[J].测控技术,2012,31(8):137-139,3.

测控技术

OA北大核心CSCDCSTPCD

1000-8829

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