首页 | 本学科首页   官方微博 | 高级检索  
     

环管型燃烧室火焰筒壁温气热耦合数值模拟
引用本文:董红,闻雪友,李名家,贺星. 环管型燃烧室火焰筒壁温气热耦合数值模拟[J]. 航空动力学报, 2014, 29(5): 1071-1078
作者姓名:董红  闻雪友  李名家  贺星
作者单位:海军工程大学 动力工程学院, 武汉 430033;中国船舶重工集团公司 第七〇三研究所, 哈尔滨 150078;中国船舶重工集团公司 第七〇三研究所, 哈尔滨 150078;海军工程大学 动力工程学院, 武汉 430033
摘    要:针对某型燃气轮机运行时回流式环管型燃烧室的火焰筒常发生烧蚀和裂纹,需获取其火焰筒壁温分布特点,进行分析以提出改进措施.全面考虑固体导热和辐射传热、气体与固体间的对流换热以及火焰和燃气的辐射,对燃烧室进行三维气热耦合数值模拟计算,获取流场、温度场以及壁温分布信息,并结合实验验证了三维气热耦合数值模拟能够较有效预测火焰筒壁温分布.由模拟结果知该型火焰筒壁温未超过设计值1 223K,但在联焰管与筒体连接处以及多个主燃孔处的温度较高、温度梯度较大,需要对这些部位的冷却方案进行改进.

关 键 词:环管型燃烧室  火焰筒壁温  气热耦合  温度梯度  实验验证
收稿时间:2013-03-14

Coupled heat transfer numerical simulation of wall temperature of can-annular combustor flame tube
DONG Hong,WEN Xue-you,LI Ming-jia and HE Xing. Coupled heat transfer numerical simulation of wall temperature of can-annular combustor flame tube[J]. Journal of Aerospace Power, 2014, 29(5): 1071-1078
Authors:DONG Hong  WEN Xue-you  LI Ming-jia  HE Xing
Affiliation:College of Power Engineering, Naval University of Engineering, Wuhan 430033, China;The 703 Research Institute of China Shipbuilding Industry Corporation, Harbin 150078, China;The 703 Research Institute of China Shipbuilding Industry Corporation, Harbin 150078, China;College of Power Engineering, Naval University of Engineering, Wuhan 430033, China
Abstract:The wall temperature distribution of a can-annular reversed combustor flame tube was obtained and analyzed to ameliorate the flame tube design, since the flame tube was often ablated partly and cracked when a gas turbine running. The distributions of flow field, temperature field and wall temperature were obtained by the method of three-dimensional numerical simulation of coupled heat transfer, while heat conduction and radiation of solid, heat convection between gas and solid, radiation of flame and flue gas were took into account. The simulation result was checked by experiments, so the temperature distribution of flame tube can be predicted with the method of three-dimensional numerical simulation of coupled heat transfer. According to the simulation result, the wall temperature of combustor flame tube doesn't exceed the design value 1223K, but the temperature and temperature gradient are relatively high at several primary holes and the joint of the flame crossover tube and flame tube, and the cooling design of these parts needs to be improved.
Keywords:can-annular combustor  wall temperature of flame tube  coupled heat transfer  temperature gradient  checking by experiment
本文献已被 CNKI 等数据库收录!
点击此处可从《航空动力学报》浏览原始摘要信息
点击此处可从《航空动力学报》下载全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号