全数字海拔模拟试验台进排气压力自动控制系统

2010 Third International Conference on Intelligent Networks and Intelligent Systems Pub Date : 2010-11-01 DOI:10.1109/ICINIS.2010.165

Song Zhang, Ying-qing Guo, Min–jie Hou, Long Li, Jie Guo, Zhihong Dan

{"title":"全数字海拔模拟试验台进排气压力自动控制系统","authors":"Song Zhang, Ying-qing Guo, Min–jie Hou, Long Li, Jie Guo, Zhihong Dan","doi":"10.1109/ICINIS.2010.165","DOIUrl":null,"url":null,"abstract":"The identification work of the aero-engine altitude test is influenced directly by the quality and accuracy of the pressure control of the intake and exhaust. In this paper, these aspects, including: the hardware structure, the software function, the digital PID engineering improvement method of the digital pressure regulation plat, and the GE90-70 based semi-physical simulation test bed construction are introduced in detail. Many advanced control techniques developed for intake and exhaust control system have been applied to the multi-type engine altitude simulation tests successfully, improved the simulation accuracy of the altitude and Mach number greatly, as well as the quality of the simulation.","PeriodicalId":319379,"journal":{"name":"2010 Third International Conference on Intelligent Networks and Intelligent Systems","volume":"28 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2010-11-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"All-Digital Altitude Simulation Test Stand Intake and Exhaust Pressure Automatic Control System\",\"authors\":\"Song Zhang, Ying-qing Guo, Min–jie Hou, Long Li, Jie Guo, Zhihong Dan\",\"doi\":\"10.1109/ICINIS.2010.165\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"The identification work of the aero-engine altitude test is influenced directly by the quality and accuracy of the pressure control of the intake and exhaust. In this paper, these aspects, including: the hardware structure, the software function, the digital PID engineering improvement method of the digital pressure regulation plat, and the GE90-70 based semi-physical simulation test bed construction are introduced in detail. Many advanced control techniques developed for intake and exhaust control system have been applied to the multi-type engine altitude simulation tests successfully, improved the simulation accuracy of the altitude and Mach number greatly, as well as the quality of the simulation.\",\"PeriodicalId\":319379,\"journal\":{\"name\":\"2010 Third International Conference on Intelligent Networks and Intelligent Systems\",\"volume\":\"28 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2010-11-01\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"2010 Third International Conference on Intelligent Networks and Intelligent Systems\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/ICINIS.2010.165\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"2010 Third International Conference on Intelligent Networks and Intelligent Systems","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/ICINIS.2010.165","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}

引用次数: 0

摘要

航空发动机进排气压力控制的质量和精度直接影响着高空试验的识别工作。本文详细介绍了数字调压台的硬件结构、软件功能、数字PID工程改进方法以及基于GE90-70的半实物仿真试验台的搭建。许多先进的进气和排气控制系统控制技术已成功地应用于多型号发动机高度仿真试验，大大提高了高度和马赫数的仿真精度和仿真质量。

本文章由计算机程序翻译，如有差异，请以英文原文为准。

查看原文本刊更多论文

All-Digital Altitude Simulation Test Stand Intake and Exhaust Pressure Automatic Control System

The identification work of the aero-engine altitude test is influenced directly by the quality and accuracy of the pressure control of the intake and exhaust. In this paper, these aspects, including: the hardware structure, the software function, the digital PID engineering improvement method of the digital pressure regulation plat, and the GE90-70 based semi-physical simulation test bed construction are introduced in detail. Many advanced control techniques developed for intake and exhaust control system have been applied to the multi-type engine altitude simulation tests successfully, improved the simulation accuracy of the altitude and Mach number greatly, as well as the quality of the simulation.

求助全文

通过发布文献求助，成功后即可免费获取论文全文。去求助

来源期刊

2010 Third International Conference on Intelligent Networks and Intelligent Systems

自引率

0.00%

发文量