基于旋转的总温/总压双向同时采集试验测控系统
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- 英文论文题名：Measurement and Control System for Total Temperature and Total Pressure Bidirectional Simultaneous Collecting By Rotation
- 论文作者：刘金林 ; 肖添明 ; 葛新 ; 杨志民
- 英文论文作者：LIU Jin-lin ; XIAO Tian-ming ; GE Xin ; YANG Zhi-min ; AVIC Shenyang Engine Design and Research Institute
- 年：2016
- 作者机构：中航工业沈阳发动机设计研究所;
- 论文关键词：燃烧室 ; 双向采集 ; 测控系统
- 英文论文关键词：combustor ; bidirection data collecting ; measurement and control system
- 会议召开时间：2016-07-15
- 会议录名称：2016航空试验测试技术学术交流会论文集
- 语种：中文
- 分类号：V263.3
- 学会代码：ZGHU
- 学会名称：中国航空学会
- 页数：3
- 文件大小：515k
- 原文格式：O
摘要
设计了基于旋转的总温/总压双向同时采集主燃烧室试验测控系统。利用此系统可以同时进行主燃烧室的出口温度场品质和压力损失试验,经试验验证,此系统可以稳定高效地完成出口温度场品质和压力损失试验;其正转和反转双向采集状态满足试验重复性要求。
The measurement and control system for total temperature and total pressure bidirectional simultaneous collecting by rotation is designed.By this system,temperature field performance collection of main combustion chamber and pressure loss test can be done simultaneously.Experiments show that this system can complete temperature field performance test and pressure loss test stably and efficiendy,and its bidirectional data collection can meet the requirement of test repeatability.
The measurement and control system for total temperature and total pressure bidirectional simultaneous collecting by rotation is designed.By this system,temperature field performance collection of main combustion chamber and pressure loss test can be done simultaneously.Experiments show that this system can complete temperature field performance test and pressure loss test stably and efficiendy,and its bidirectional data collection can meet the requirement of test repeatability.
引文
[1]邓明.航空燃气涡轮发动机原理与构造[M].北京:国防工业出版社,2008.
[2]侯晓春,季鹤鸣,刘庆国,等.高性能航空燃气轮机燃烧技术[M].北京:国防工业出版社,2002.
[3]刘金林,杨广,杨志民.基于LabWindows/CVI和组态王的主燃烧室试验测控系统[J].测控技术,2014,33(增刊):62-64.
[4]杨志民,孙永飞,赵煜,等.航空发动机燃烧室出口温度场双向测量方法[J].航空发动机,2010,36(1):42-43.
[5]马宏宇,赵传亮,程明,等.取样密度对燃烧室试验测量结果的影响[J].航空发动机,2014,40(3):19-23.
[2]侯晓春,季鹤鸣,刘庆国,等.高性能航空燃气轮机燃烧技术[M].北京:国防工业出版社,2002.
[3]刘金林,杨广,杨志民.基于LabWindows/CVI和组态王的主燃烧室试验测控系统[J].测控技术,2014,33(增刊):62-64.
[4]杨志民,孙永飞,赵煜,等.航空发动机燃烧室出口温度场双向测量方法[J].航空发动机,2010,36(1):42-43.
[5]马宏宇,赵传亮,程明,等.取样密度对燃烧室试验测量结果的影响[J].航空发动机,2014,40(3):19-23.