微型离心压气机扩压器设计与分析

宋寅, 李雪松, 顾春伟

分布式能源 ›› 2016, Vol. 1 ›› Issue (3) : 18-22.

PDF(2448 KB)
PDF(2448 KB)
分布式能源 ›› 2016, Vol. 1 ›› Issue (3) : 18-22. DOI: 10.16513/j.cnki.10-1427/tk.2016.03.003

微型离心压气机扩压器设计与分析

作者信息 +

Design and Analysis for the Diffuser of a Micro Centrifugal Compressor

Author information +
文章历史 +

摘要

微型燃气轮机是微小型分布式供能系统的核心设备,叶片扩压器对于微型燃机离心压气机的性能有重要影响。该文对某kW级微型燃机的扩压器进行了设计,对带扩压器的微型离心压气机进行数值模拟,着重探讨了扩压器进口冲角对压气机性能的影响。数值模拟结果表明,扩压器进口负冲角很大时,在小流量的工况下压比和效率很高,在大流量工况下压比和效率迅速降低,特性曲线陡峭,工作范围变窄。扩压器进口冲角绝对值较小时,压气机特性曲线较为平坦,工作范围宽广,冲角的较小变化对于压气机性能的影响不显著;正冲角情况下,扩压器的静压恢复系数最高,负冲角越大,静压恢复系数越小。由此可见,扩压器进口冲角的最优值并不固定,应当根据压气机具体工作要求进行选择,同时还需要考虑为保证燃烧器有较高的燃烧效率而带来的对静压恢复系数的要求。

Abstract

Micro gas turbine is the core device of micro distributed energy system, and the vaned diffuser has significant influence on the compressor performance of micro gas turbine. The diffuser of a kW-class micro gas turbine was designed, and the numerical simulation was made on the micro compressor with vaned diffuser, especially the influence of vane incidence on the compressor performance. The results show that the pressure ratio and efficiency of compressor are very high in the case of large negative incidence at small flow rate, while the parameters drop quickly at large flow-rate condition with steep characteristic curve and narrowed working range. When the absolute value of diffuser incidence is relative small, the compressor shows a relative flat characteristic curve and wide working range. The slight variation of incidence contributes less to the performance of compressor. The static recovery coefficient is higher under positive incidence condition, and it becomes lower as the incidence decreases. The optimum incidence of vaned diffuser is not fixed and should be determined according to the specific working condition and the requirements for higher combustion efficiency.

关键词

微型燃机 / 扩压器 / 冲角 / 数值模拟 / 设计原则

Key words

micro gas turbine / diffuser / incidence / numerical simulation / design principle

引用本文

导出引用
宋寅, 李雪松, 顾春伟. 微型离心压气机扩压器设计与分析[J]. 分布式能源. 2016, 1(3): 18-22 https://doi.org/10.16513/j.cnki.10-1427/tk.2016.03.003
Yin SONG, Xuesong LI, Chunwei GU. Design and Analysis for the Diffuser of a Micro Centrifugal Compressor[J]. Distributed Energy Resources. 2016, 1(3): 18-22 https://doi.org/10.16513/j.cnki.10-1427/tk.2016.03.003
中图分类号:     

参考文献

[1]
陈杰钟榈黄国平. 微型离心叶轮流动损失分析与削弱[J]. 推进技术2013, 34(7): 904-910.
CHEN Jie, ZHONG Lyu, HUANG Guoping. Analysis and reduction of flow loss in a micro centrifugal impeller[J]. Journal of Propulsion Technology, 2013, 34(7): 904-910.
[2]
聂振宇苗福祥. 某微型离心压气机的流场计算与分析[J]. 战术导弹技术2014(5): 58-69.
NIE Zhenyu, MIAO Fuxiang. Flow field computation and analysis on a centrifugal compressor[J]. Tactical Missile Technology, 2014(5): 58-69.
[3]
李德雄. 某型微型离心压气机流场分析及其改型研究[D]. 哈尔滨:哈尔滨工业大学,2015.
LI Dexiong. Internal flow field analysis and redesign of micro centrifugal compressor[D]. Harbin:Harbin Institute of Technology, 2015.
[4]
刘小民席光王尚锦. 叶片扩压器进口角度对离心压缩机性能的影响[J]. 流体机械1998, 26(1): 3-5.
LIU Xiaomin, XI Guang, WANG Shangjin. Influence of the diffuser inlet angle on the centrifugal compressor performance[J]. Fluid Machinery, 1998, 26(1): 3-5.
[5]
席光周莉丁海萍,等. 叶片扩压器进口安装角对离心压缩机性能影响的数值与实验研究[J]. 工程热物理学报2006, 27(1): 61-64.
XI Guang, ZHOU Li, DING Haiping, et al. Numerical and experimental study of the effects of the stagger angles of vane diffuser on the performance of centrifugal compressors[J]. Journal of Engineering Thermophysics, 2006, 27(1): 61-64.
[6]
李燕生陆桂林. 向心透平与离心压气机[M]. 北京:机械工业出版社,1987: 262-273.
LI Yansheng, LU Guilin. Radial turbine and centrifugal compressor[M]. Beijing: China Machine Press, 1987: 262-273.
[7]
舒士甄朱力柯玄龄,等. 叶轮机械原理[M]. 北京:清华大学出版社,1991: 287-319.
SHU Shizhen, ZHU Li, KE Xuanling, et al. Principle of turbomachinery[M]. Beijing:Tsinghua University Press, 1991: 287-319.
[8]
KAI U ZGALLUS H ENIEHUIS R. A study on impeller-diffuser interaction-Part Ⅰ:Influence on the performance[J]. Journal of Turbomachinery, 2003, 125(1): 173-182.
[9]
SMIRNOV P E, HANSEN T, MENTER F R. Numerical simulation of turbulent flows in centrifugal compressor stages with different radial gaps[C]//ASME Turbo Expo: Power for Land, Sea & Air. Montreal, Canada: International Gas Turbine Institute, 2007: 1029-1038.
[10]
DENIZ S, GREITZER E M, CUMPSTY N A. Effects of inlet flow field conditions on the performance of centrifugal compressor diffusers-Part 2-Straight-channel diffuser[J]. Journal of Turbomachinery, 2000122(1): 11-21.
[11]
TAMAKI H, NAKAO H, SAITO M. The experimental study of matching between centrifugal compressor impeller and diffuser[J]. Journal of Turbomachinery1999121(1):113-118.

编辑: 蒋毅恒
PDF(2448 KB)

Accesses

Citation

Detail

段落导航
相关文章

/