Optimization design of centrifugal/oblique flow compressor two-dimensional blade profiles in three-dimensional environment
-
摘要: 考虑离心/斜流压气机转子叶片通道内流动的强三维性,提出在三维环境下进行二维叶型优化设计.通过对能量方程中黏性耗散项改进,解决了Denton黏性体积力方法模拟离心/斜流叶轮三维流场效率偏高的不足.将改进流场计算模块与并行遗传算法寻优模块相结合,构成离心/斜流压气机二维叶型优化设计软件.采用所研制的软件,分别对离心叶轮和斜流叶轮叶尖处叶型进行优化设计.优化叶片基本达到目标流量和压比,在整个工作范围内效率都提高明显:在设计点离心叶轮效率由0.938提高到0.947,斜流叶轮效率由0.899提高到0.918.Abstract: As for strong three-dimensional flow in centrifugal/oblique flow compressor rotor blade passages, the two-dimensional blade profiles were optimally designed in three-dimensional environment. The efficiency of centrifugal/oblique flow compressor calculated by the Denton viscous volume force method was obviously higher, and the problem was solved by modifying the viscous dissipation in the energy equation. Then, optimization design software of two-dimensional blade profiles was built by combining the modified flow field calculation module with the parallel genetic algorithm. The software was used for designing tip profiles of centrifugal impeller and oblique flow impeller. The mass flow and pressure ratio of these two optimized impellers are very close to objective values, and the efficiency in whole working range is significantly improved. At the design point, the efficiency of centrifugal impeller is improved from 0.938 to 0.947, and the efficiency of oblique flow impeller is improved from 0.899 to 0.918.
-
[1] 朱方元,周新海.轴流跨音速压气机级的气动设计方法[J].西北工业大学学报,1979(1):5-25. ZHU Fangyuan,ZHOU Xinhai.An aerodynamic design method for transonic axial-flow compressor stage[J].Journal of Northwestern Polytechnical University,1979(1):5-25.(in Chinese) [2] 程荣辉.轴流压气机设计技术的发展[J].燃气涡轮试验与研究,2004,17(2):1-8. CHENG Ronghui.Development of design technology for axial compressor[J].Gas Turbine Experiment and Research,2004,17(2):1-8.(in Chinese) [3] Pitigala D B A,Zangeneh M,Li Y.Redesign of a transonic compressor rotor by means of a three-dimensional inverse design method:a parametric study[R].ASME Paper GT2007-27486,2007. [4] Ashihara K,Goto A.Turbomachinery blade design using 3-D inverse method,CFD and optimization algorithm[R].ASME Paper GT2001-358,2001. [5] Sanger N L.The use of optimization techniques to design controlled diffusion compressor blading[J].Journal of Engineering for Power,1983,105(2):256-264. [6] 周正贵.压气机/风扇叶片自动优化设计的研究现状和关键技术[J].航空学报,2008,29(2):257-266. ZHOU Zhenggui.Current situations and key techniques of automatic aerodynamic design of compressor/fan blades[J].Acta Aeronautica et Astronautica Sinica,2008,29(2):257-266.(in Chinese) [7] Frank S,Beat R.Design of industrial axial compressor blade sections for optimal range and performance[J].Journal of Turbomachinery,2004,126(2):323-331. [8] Benini E,Toffolo A.Development of high-performance airfoils for axial flow compressors using evolutionary computation[J].Journal of Propulsion and Power,2002,18(3):544-554. [9] 周正贵.高亚音速压气机叶片优化设计[J].推进技术,2004,25(1):58-61. ZHOU Zhenggui.Optimization of high subsonic axial compressor blades[J].Journal of Propulsion Technology,2004,25(1):58-61.(in Chinese) [10] Oyama A,Liou M S.High-fidelity swept and leaned rotor blade design optimization using evolutionary algorithm[R].AIAA-2003-4091,2003. [11] Benimi E.Three-dimensional multi-objective design optimization of a transonic compressor rotor[R].AIAA-2003-4090,2003. [12] 徐夏.叶轮机械流场计算与任意回转面叶型设计[D].南京:南京航空航天大学,2010. XU Xia.Calculation of turbomachinery flow fields and design of blade profile on arbitrariay rotational surfaces[D].Nanjing:Nanjing University of Aeronautics and Astronautics,2010.(in Chinese) [13] Krain H,Hoffman W.Verification of an impeller design by laser measurements and 3D-viscous flow calculations[R].Toronto,Canada:ASME Gas Turbine and Aeroengine Congress and Exposition,1989. [14] 周正贵.压气机/风扇二维叶型自动优化设计[J].航空学报,2011,32(11):1987-1997. ZHOU Zhenggui.Automatic optimization design of compressor/fan 2D blade profiles[J].Acta Aeronautica et Astronautics Sinica,2011,32(11):1987-1997.(in Chinese) [15] 汪光文.基于并行遗传算法的风扇/压气机叶片气动优化[D].南京:南京航空航天大学,2009. WANG Guangwen.Research on aerodynamic optimization design of fan/compressor blade using parallel genetic algorithm[D].Nanjing:Nanjing University of Aeronautics and Astronautics,2009.(in Chinese) [16] 周旭.民用大涵道风扇叶片气动优化设计研究[D].南京:南京航空航天大学,2013. [17] Krain H,Karpinski G,Beversdorff M.Flow analysis in a transonic centrifugal compressor rotor using 3-component laser velocimetry[R].ASME Paper 2001-GT-0315,2001.
点击查看大图
计量
- 文章访问数: 1402
- HTML浏览量: 2
- PDF量: 1067
- 被引次数: 0