高轮毂比离心压气机改型设计及分析Redesign and Analysis of a High Hub/tip Ratio Centrifugal Compressor
龙双喜,王毅
LONG Shuang-xi1,WANG Yi2(1.Guangdong Huizhou LNG Power Co.
摘要(Abstract)：
以某高轮毂比离心压气机为研究对象,在给定的轴向尺寸限定下,进行离心压气机改型设计,提出了离心叶轮和径向扩压器子午流道倾斜的设计方法以提高离心压气机性能,并借助数值模拟手段,揭示了该设计方法提高高轮毂比离心压气机性能的机理,可为高轮毂比离心压气机改型气动设计提供借鉴。
The hub and shroud contours are redesigned for a high hub/tip ratio centrifugal compressor with the same axial dimension.Detailed analyses of the flow visualization have exposed flow topologies between the cases with original compressor and modified compressor by numerical simulation,therefore led to some preliminary conclusions as to the flow physics involved in the compressor performance improvements afforded by the redesign of hub and shroud contours.
关键词(KeyWords)：
高轮毂比;离心压气机;改型设计;数值模拟
high hub/tip ratio;centrifugal compressor;remodel design;numerical simulation
基金项目(Foundation):
作者(Author):
龙双喜,王毅
LONG Shuang-xi1,WANG Yi2(1.Guangdong Huizhou LNG Power Co.
参考文献(References)：
- [1]Rodgers C,Brown D.High Hub/Tip Ratio CentrifugalCompressors[R].ASME Paper,GT2009-59012.
- [2]Klassen H K,Wood J R,Schumman L F.ExperimentalPerformance of a 13.65cm Tip Diameter Tandem Blad-ed Centrifugal Compressor Designed for a Pressure Ra-tio of 6.0[R].1977,NASA TP-1091.
- [3]Palmer D L,Watermann W F.Design and Developmentof an Advanced Two-Stage Centrifugal Compressor[J].ASME Journal of Turbomachinery,1995,117(2):118-126.
- [4]Kalogiannis M H,Leblanc A D,Przybytkowski S M.Advanced Small High Pressure Ratio Centrifugal Com-pressor[R].AGARD-CP-537,1994.
- [5]Oana M.Approach to High Performance Transonic Ce-ntrifugal Compressor[R].AIAA Propulsion Confer-ence,2002.
- [6]Rodgers C.Compact Diffusers for Small Transonic Co-mpressors[R].1994,AGARD CP 537.
- [7]Rodgers C.The Centrifugal Compressor Inducer[R].ASME paper 98-GT-32.
- [8]Takehara I Tatsumi T Ichikawa Y.Summary of CGT302Ceramic Gas Turbine Reseach and Development Pro-gram[J].Journal of Engineering for Gas Turbine andPower,2002,124:627-635.
- [9]Ortiz Duenas C,Miller R J,Hodson H P,et al.Effectof length on compressor inter-stage duct performance[R].ASME Paper 2007-GT-27752.
- [10]Zoccoli M J,Klassen D D.1990.T407/GLC:AModern Technology Powerplant[R].ASME 90-GT-242.
- [11]高星.斜流-离心双级压气机内部复杂流动与设计方法研究[D].北京:北京航空航天大学博士论文,2008.