首页 | 本学科首页   官方微博 | 高级检索  
     

高负荷缝隙弯曲扩压叶栅展向负荷实验
引用本文:陈焕龙,陈浮,宋彦萍. 高负荷缝隙弯曲扩压叶栅展向负荷实验[J]. 航空动力学报, 2009, 24(2): 420-426
作者姓名:陈焕龙  陈浮  宋彦萍
作者单位:哈尔滨工业大学能源科学与工程学院,哈尔滨,150001;哈尔滨工业大学能源科学与工程学院,哈尔滨,150001;哈尔滨工业大学能源科学与工程学院,哈尔滨,150001
基金项目:国家重点基础研究发展规划(973计划),国家自然科学基金 
摘    要:实验研究了不同冲角下压气机采用带切向缝隙的大转角弯曲叶片对叶栅展向负荷的影响.研究结果表明,切向缝隙射流能够有效地增加整个叶展的扩压因子,提高气流的折转能力,缝隙反弯叶片出口静压比沿展向呈现C形分布特点,缝隙射流控制技术与弯曲叶片技术相结合是未来高负荷扩压叶栅发展的一个研究方向. 

关 键 词:缝隙叶片  扩压因子  叶片负荷
收稿时间:2008-07-24
修稿时间:2008-11-28

Experimental investigation on the span loading in compound lean compressor cascades with slots air injection
CHEN Huan-long,CHEN Fu and SONG Yan-ping. Experimental investigation on the span loading in compound lean compressor cascades with slots air injection[J]. Journal of Aerospace Power, 2009, 24(2): 420-426
Authors:CHEN Huan-long  CHEN Fu  SONG Yan-ping
Affiliation:School of Energy Science and Engineering, Harbin Institute of Technology, Harbin 150001, China
Abstract:An experimental investigation was conducted for the influence on the loading of span by 60° turning angle plane compound lean compressor cascade,which was designed with tangent air injection slots in different inflow incidences.The experimental results show that not only the diffusion factor of cascades is increased and the turning of airflow is improved effectively,but also the static pressure of outlet in negative lean cascades presents a C distribution from hub to shroud by tangent air injection.The integration of slots injection and compound lean blade technologies will be an investigation direction in the future.
Keywords:slot blade  diffusion factor  blade loading  
本文献已被 CNKI 万方数据 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