航空发动机风扇/压气机技术发展的若干问题与思考
收稿日期: 2015-05-04
修回日期: 2015-06-19
网络出版日期: 2015-06-19
Some problems and thoughts in the development of aero-engine fan/compressor
Received date: 2015-05-04
Revised date: 2015-06-19
Online published: 2015-06-19
刘永泉 , 刘太秋 , 季路成 . 航空发动机风扇/压气机技术发展的若干问题与思考[J]. 航空学报, 2015 , 36(8) : 2563 -2576 . DOI: 10.7527/S1000-6893.2015.0078
In the next 10 to 20 years, China's aero-engine technology will usher in a golden opportunity for development, which we must be fully prepared for. This paper focuses on the aerodynamic field of the aero-engine core components-fan/compressor. Firstly, from the point of design methods, theories and the still existing questions of aerodynamics, we sort out the international development trend. Then against the fundamental research and innovation, etc., we describe the civil development status and problems; finally we analyze the future development, thoughts and emphasis of fan/compressor, which is expected to offer some reference for the research of China's military and civil aero-engine fan/compressor.
Key words： aero-engine; fan; compressor; technology research; technology system; developing trend
[1] Koff B L, Koff B L. Gas turbine technology evolution: A designers perspective[J]. Journal of Propulsion and Power, 2004, 20(4): 577-595.
[2] Wadia A R. Some advances in fan and compressor aero at GE aircraft engines[R]. Beijing: Tsinghua University, 2005.
[3] Chen M Z. Fan/compressor technology development and the suggestions on future research[C]//Symposium on the Proceedings of Aero-engine in 21st Century. Beijing: Chinese Society of Aeronautics and Astronautics, 2000 (in Chinese). 陈懋章. 风扇/压气机技术发展和对今后工作的建议[C]//21世纪航空动力发展研讨会. 北京: 中国航空学会, 2000.
[4] Chen M Z, Liu B J. Fan/compressor aero design technology and challenge of high bypass ratio turbofan[J]. Journal of Aerospace Power, 2008, 23(6): 961-975 (in Chinese). 陈懋章, 刘宝杰, 风扇/压气机气动设计技术与挑战——用于大型客机的大涵道比涡扇发动机[J]. 航空动力学报, 2008, 23(6): 961-975.
[5] Ji L C. Some understanding and suggestion on internal flow[R]. Beijing: National Natural Science Foundation of China, 2014 (in Chinese). 季路成. 关于内部流动的几点认识和建议[R]. 北京: 国家自然科学基金委员会, 2014.
[6] Jameson A. Optimum aerodynamic design using CFD and control theory, AIAA-1995-1729-CP[R]. Reston: AIAA, 1995.
[7] Giles M B, Pierce N A. Adjoint equations in CFD: duality, boundary conditions and solution behavior, AIAA-1997-1850[R]. Reston: AIAA, 1997.
[8] Wang D X, He L. Adjoint aerodynamic design optimization for blades in multi-stage turbomachines: Part I-methodology and verification, ASME Paper, 2008-GT-50208[R]. New York: ASME, 2008.
[9] Lapworth L, Shahpar S. Design of gas turbine engines using CFD[C]//Proceedings of the European Congress on Computational Methods in Applied Sciences and Engineering (ECCOMAS), 2004: 24-28.
[10] Rick H. Gasturbinen und flugantriebe: grundlagen, betribsverhalten und simulation[M]. Heidelberg: Springer-Verlag, 2013.
[11] Johnsen I A, Bullock R O. Aerodynamic design of axial-flow compressors, NASA SP-36[R]. Washington, D.C.: NASA, 1965.
[12] Seyler D R, Smith L H, Jr. Single stage experimental evaluation of high Mach number compressor rotor blading, Part I, design of rotor blading, NASA CR-54581[R]. Washington, D.C.: NASA, 1967.
[13] Frost G R, Wennerstrom A J. The design of axial compressor airfoils using arbitrary camber lines, ARL 73-0107, AD 765165[R]. Ohio: Aerospace Research Laboratories, Wright-Patterson Air Force Base, 1973.
[14] Hobbs D E, Weingold H D. Development of controlled diffusion airfoils for multistage compressor application[J]. Journal of Engineering for Gas Turbines and Power, 1984, 106(2): 271-278.
[15] Ji L C, Li J B, Yi W L. The way to the third generation of 3-D blades[C]//Conference on Aerothermophysics, Chinese Society of Thermophysics, 2014: 142152 (in Chinese). 季路成, 李嘉宾, 伊卫林. 第三代三维叶片技术思路分析[C]//中国工程热物理学会热机气动热力学学术会议, 2014: 142152.
[16] Rabe D, Hoying D, Koff S. Application of sweep to improve the efficiency of a transonic fan, Part Ⅱ-performance and laser test results, AIAA-1991-2544[R]. Reston: AIAA, 1991.
[17] Ji L C. Trend of full three-dimensional blading techniques for high performance turbomachinery[J]. Aeroengine, 2013, 39(4): 9-18 (in Chinese). 季路成. 高性能叶轮机全3维叶片技术趋势展望[J]. 航空发动机, 2013, 39(4): 9-18.
[18] Ji L C. Research on supersonic compressor[R]. Beijing: China Aviation Power Machinery Institute, 2012: 1-20 (in Chinese). 季路成. 全超声压气机研究[R]. 北京: 中国航空动力机械研究所, 2012: 1-20.
[19] Biollo R, Benini E. Recent advances in transonic axial compressor aerodynamics[J]. Progress in Aerospace Sciences, 2013, 56: 1-18.
[20] Shao W W. Exploration on maximum loading design techniques for fan and axial-flow compressor[D]. Beijing: Graduate University of the Chinese Academy of Sciences, 2008 (in Chinese). 邵卫卫. 风扇/轴流压气机最大负荷设计技术探索[D]. 北京: 中国科学院研究生院, 2008.
[21] Rose M G. Non-axisymmetric endwall profiling in the HP NGV's of an axial flow gas turbine[C]//ASME 1994 International Gas Turbine and Aeroengine Congress and Exposition. New York: ASME, 1994.
[22] Ji L C. Design method on blended blade and endwall technique: China, ZL201010623606[P]. 2012-10-24 (in Chinese). 季路成. 一种叶轮机械叶片与端壁融合设计方法: 中国, ZL201010623606[P]. 2012-10-24.
[23] Ji L C, Ke H Y, Li W. A new freedom for turbomachinery design-edge-matching technique, ISABE Paper, No.1100[R]. 2003.
[24] Yao J, Cargill P L, Holmes D G, et al. Aspects of numerical analysis for unsteady flows in aircraft engines[C]//Proceedings of the 48th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, 2010.
[25] Yu Q, Li Q S, Li L. The experimental research on improving operating stability of a single-stage transonic fan, ASME Paper, 2002-GT-30640[R]. New York: ASME, 2002.
[26] Chen B S, Hu G R, Wei Y B, et al. Design and test research of highly loaded single-stage fan[J]. Aeroengine, 2000(3): 28-35 (in Chinese). 陈葆实, 胡国荣, 魏玉冰, 等. 高马赫数、高负荷单级风扇设计和试验研究[J]. 航空发动机, 2000(3): 28-35.
[27] Ji L C, Chen J. Technical direction analysis from IHPTET TO VAATE[C]//Conference on Aerothermophysics, Chinese Society of Thermophysics, 2005: 052086 (in Chinese). 季路成, 陈江. 从IHPTET到VAATE的技术方向探析[C]//中国工程热物理学会热机气动热力学2005年学术会议, 2005: 052086.
[28] Ji L C. Discussion on the technology development of aero engine and vane turbine components[R]. Mianyang: Institute of Air Dynamics in China, 2014 (in Chinese). 季路成. 航空发动机及其叶轮机部件技术发展探讨[R]. 绵阳: 中国空气动力学研究院, 2014.
[29] Koch C C. The stall pressure-rise capability of axial compressors[J]. Journal of Engineering for Gas Turbines Power, 1981, 103: 645-656.
[30] FUN3D manual[EB/OL]. [2015-03-24]. http://fun3d.larc.nasa.gov/
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