重型燃气轮机燃烧室全温全压排故试验  

High-Temperature and Pressure Debugging Test of a Heavy-Duty Gas Turbine Combustor

作　　者：罗智锋[1] 刘重阳[1] 黄治国 王秀兰[1] 李华东[1] 

机构地区：[1]中国燃气涡轮研究院,四川江油621703 [2]中航发动机有限责任公司,北京100028

出　　处：《燃气涡轮试验与研究》2014年第6期33-36,共4页Gas Turbine Experiment and Research

摘　　要：详细介绍了某重型燃气轮机天然气燃料燃烧室全温全压试车台建设,及全温全压排故试验。建立的全温全压试车台满足使用要求,积累的试验台建设经验为后续更高指标的试验器建设奠定了技术基础;燃烧室全温全压试验重现了电厂故障,验证了燃烧室壁面烧蚀的原因,为燃烧室现场排故及后续优化设计提供了技术支持,同时也获得了宝贵的全温全压燃烧室排故试验经验。The high-temperature and pressure test rig construction for heavy-duty gas turbine combustor with natural gas, and the debugging tests were presented. Abundant construction experience was accumulat？ed in the process and it made a technology base for the higher index tester building. The combustor working faults in the electricity generating station were reappeared in the high-temperature and pressure tests and the reasons of combustor liner wall ablation were certificated, which is helpful for the combustor debugging and optimum design. At the same time, the valuable experience of high-temperature and pressure combus？tor debugging test are also got.

关 键 词：重型燃气轮机 燃烧室 天然气 试验台 全温全压 排故 

分 类 号：TK477[动力工程及工程热物理—动力机械及工程]