摘要
为适应不同用途先进航空发动机燃烧室的研制,美、英、法、德、俄等国建设了大量的燃烧室试验器。概述了国外航空发动机研发机构主要的燃烧室试验器类型,详细介绍了各类试验器的总体参数、系统组成、结构布局、加温方式、测试系统和特种测量等,分析了国内燃烧室试验器的现状及其与国外的差距,并提出相关建议。对我国新一代高性能航空发动机燃烧室试验器的规划和建设,具有一定的参考和借鉴意义。
Lots of combustor test facilities were built for different purposes by U.S, Great Britain, France,Germany and Russia to meet the requirements of advanced combustor development. The main types of tes?ter of foreign research organizations were introduced, and the key information such as overall parameters,layout, heating type, instrumentation and emission measurement of these test facilities were presented in de?tail. At last, the present situation in our country and the gap between abroad and domestic were summa?rized. Additionally, some suggestions were also given. It could be referential in the process of planning anddesigning the next generation combustor test facilities of our country.
作者
孟刚
赵聪聪
孙用军
董干
孙鑫
张瑜
MENG Gang;ZHAO Cong-cong;SUN Yong-jun;DONG Gan;SUN Xin;ZHANG Yu(Center for Instrumentation & Rig Testing,Shanghai AVIC Commercial Aircraft Engine Manufacturing Co.,Ltd,Shanghai 201108,China)
出处
《燃气涡轮试验与研究》
北大核心
2016年第3期55-62,共8页
Gas Turbine Experiment and Research
关键词
航空发动机
燃烧室试验器
性能测试
设备建设
美国
英国
俄罗斯
aero-engine
combustor tester
performance test
test facility construction
U.S
Great Britain
Russia