航空发动机风扇/压气机技术发展的若干问题与思考

doi:10.7527/S1000-6893.2015.0078

流体力学与飞行力学

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航空发动机风扇/压气机技术发展的若干问题与思考

刘永泉¹, 刘太秋¹, 季路成²

1. 中航工业沈阳发动机设计研究所, 沈阳 110015;
2. 北京理工大学宇航学院, 北京 100081

收稿日期:2015-05-04 修回日期:2015-06-19 出版日期:2015-08-15 发布日期:2015-06-19
通讯作者: 刘永泉男, 博士, 研究员。《航空学报》第八届编委。主要研究方向: 航空发动机气体动力学, 机械动力学, 整机振动诊断与控制, 构件寿命及可靠性评估技术。Tel: 024-24281618 E-mail: yqliu606@vip.sina.com E-mail:yqliu606@vip.sina.com

Some problems and thoughts in the development of aero-engine fan/compressor

LIU Yongquan¹, LIU Taiqiu¹, JI Luchen²

1. AVIC Shenyang Engine Design and Research Institute, Shenyang 110015, China;
2. School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, China

Received:2015-05-04 Revised:2015-06-19 Online:2015-08-15 Published:2015-06-19
Contact: 10.7527/S1000-6893.2015.0078 E-mail:yqliu606@vip.sina.com

摘要/Abstract

摘要：

未来10~20年我国航空发动机科技将迎来千载难逢的发展机遇,必须做好充分准备。以航空发动机核心部件——风扇/压气机气动领域为重点,首先,从设计方法、理论、设计性能指标发展以及气动力学仍存在的疑问角度出发,梳理了其国际发展态势;随后,针对基础研究、创新能力等方面,阐述国内发展现状与存在的问题;最后,分析给出关于风扇/压气机后续发展的方向、思路和重点,力求为我国军民航空发动机风扇/压气机的技术研制思路提供参考。

关键词: 发动机, 风扇, 压气机, 技术研究, 技术体系, 发展态势

Abstract:

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

中图分类号:

V231

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.

LIU Yongquan, LIU Taiqiu, JI Luchen. Some problems and thoughts in the development of aero-engine fan/compressor[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2015, 36(8): 2563-2576.

参考文献

[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/

E-mail：hkxb@buaa.edu.cn

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航空发动机风扇/压气机技术发展的若干问题与思考

Some problems and thoughts in the development of aero-engine fan/compressor

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