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离心压气机无叶扩压段流路控制扩稳机理
引用本文:王永生,童志庭,林峰,聂超群.离心压气机无叶扩压段流路控制扩稳机理[J].航空动力学报,2012,27(9):2106-2112.
作者姓名:王永生  童志庭  林峰  聂超群
作者单位:1.中国科学院 工程热物理研究所 先进能源动力重点实验室, 北京 100190
基金项目:国家重点基础研究发展计划(2007CB210104); 国家自然科学基金(51010007)
摘    要:为寻求叶轮-扩压器间无叶扩压段流路控制的扩稳机理,选取某离心压气机为研究对象,利用数值模拟的方法,通过流场分析解释其失速机理,并在此基础上重新设计无叶扩压段机匣结构,探讨一种有效流路控制扩稳方式.分析结果表明:将无叶扩压段机匣结构设计为先收缩后扩张型后,离心压气机稳定工作范围提高了2.8%,但绝热效率有所降低. 

关 键 词:无叶扩压段    机匣结构    流路控制    扩稳    离心压气机
收稿时间:2011/10/14 0:00:00

Stall improvement mechanism of vaneless diffuser flow path control in a centrifugal compressor
WANG Yong-sheng,TONG Zhi-ting,LIN Feng and NIE Chao-qun.Stall improvement mechanism of vaneless diffuser flow path control in a centrifugal compressor[J].Journal of Aerospace Power,2012,27(9):2106-2112.
Authors:WANG Yong-sheng  TONG Zhi-ting  LIN Feng and NIE Chao-qun
Institution:1.Key Laboratory of Advanced Energy and Power Chinese Academy of Sciences, Institute of Engineering Thermophysics, Chinese Academy of Sciences, Beijing 100190, China2.Graduate University of Chinese Academy of Sciences, Beijing 100190, China
Abstract:To investigate the stall improvement mechanism of vaneless diffuser flow path control,a centrifugal compressor was simulated and compared with existing experimental data.According to characteristics of flow field and stall mechanism,a convergent-divergent type of impeller-diffuser casing designed was analyzed.The result shows that the stable flow range of centrifugal compressor increases by 2.8%,however,no obvious positive effects are found on the adiabatic efficiency which is slightly lower than that of the prototype.
Keywords:vaneless diffuser  casing structure  flow path control  stall improvement  centrifugal compressor
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