Volume 26 Issue 10
Oct.  2011
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ZHONG Jing-jun, HAN Ji-ang, YANG Ling. Research progress and development prospects of the ram-rotor[J]. Journal of Aerospace Power, 2011, 26(10): 2293-2301.
Citation: ZHONG Jing-jun, HAN Ji-ang, YANG Ling. Research progress and development prospects of the ram-rotor[J]. Journal of Aerospace Power, 2011, 26(10): 2293-2301.

Research progress and development prospects of the ram-rotor

  • Received Date: 2010-11-03
  • Rev Recd Date: 2011-02-10
  • Publish Date: 2011-10-28
  • Based on analysis of the concept,principle and structure characteristics about the ram-rotor that adopts the technology of shock compression,the research progress both at home and abroad in this field was summarized,and technical difficulties and development prospects of the new compression system were also analyzed and discussed.

     

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  • [1]
    张恩和.对我国军用航空发动机发展的思考[J].航空发动机,2001(3):1-3.
    [2]
    于达仁,刘金福,徐基豫.面向21世纪的燃气轮机技术的发展[J].燃气轮机技术,2001,14(1):14-21,53. YU Daren,LIU Jinfu,XU Jiyu.Facing the development of GT technology in the 21th century[J].Gas Turbine Technology,2001,14(1):14-21,53.(in Chinese)
    [3]
    林汝谋.工业燃气轮机发展的关键技术[J].热力发电,1999(1):26-28. LIN Rumou.Key development of industrial gas turbine[J].Thermal Power Generation,1999(1):26-28.(in Chinese)
    [4]
    Lawlor S P,Hinkey J B,Mackin S G,et al.Supersonic compressor stage design & test results .IMECE 2004-59914,2004.
    [5]
    Draper R,Steele R. Design of diffuser for high Mach and high swirl applications .2003.http:// www.cl-emson.edu/scies/UTSRPeerReview/Proceeding 20content/ Poster20session/Poster-Draper.pdf.
    [6]
    Broichhausen K D,Ziegler K U.Supersonic and transonic compressors:past,status and technology trends .ASME Paper GT2005-69067,2005.
    [7]
    Victor D B.485-kW turbine rated 35% simple cycle at 1700F firing temperature[J].Gas Turbine World,2002,32(5):13-16.
    [8]
    Victor D B.Adapting ramjet technology to 3-to-9-MW ram genset designs[J].Gas Turbine World,2002,32(3):16-19.
    [9]
    Ramgen Power Systems.Low-cost,high-efficiency CO2 compressor .2007-12-05.http://www.carboncouncil.org/pdf/presentations/technologies_baldwin.pdf.
    [10]
    Steele R,Baldwin P,Kesseli J.Insertion of shock wave compression technology into micro turbine for increased efficiency and reduced costs .ASME Paper GT2005-68203,2005.
    [11]
    Lawlor S P,Baldwin P.Conceptual design of a supersonic CO2 compressor .ASME Paper GT2005-68349,2005.
    [12]
    Grosvenor A D,Brown P M,Lawlor S P.Design methodology and predicted performance for a supersonic compressor stage .ASME Paper GT2006-90409,2006.
    [13]
    Grosvenor A D,Taylor D A,Bucher J R,et al.Measured and predicted performance of a high pressure ratio supersonic compressor rotor .ASME Paper GT2008-50150,2008.
    [14]
    王云.新概念旋转冲压发动机基础性探索研究 .南京:南京航空航天大学,2005. WANG Yun.Primary research of new conceptive internal-rotor burnt rotating ramjet .Nanjing:Nanjing University of Aeronautics and Astronautics,2005.(in Chinese)
    [15]
    于达仁,何保成,吕晓武,等.旋转冲压发动机进气道压比特性分析[J].推进技术,2008,29(3):329-333. YU Daren,HE Baocheng,LV Xiaowu,et al.Characteristics analysis of pressure ratios for rotated ramjet inlets[J].Journal of Propulsion Technology,2008,29(3):329-333.(in Chinese)
    [16]
    田新,刘占生.旋转冲压发动机进气道流场及气流对转子的作用力研究[J].振动与冲击,2008,27(Suppl.):32-35. TIAN Xin,LIU Zhansheng.Research on the flow field of rotating ramjet inlet and the airflow force on the rotor[J].Journal of Vibration and Shock,2008,27(Suppl.):32-35.(in Chinese)
    [17]
    张广辉,刘占生.旋转冲压发动机高速动静混合气体轴承性能分析[J].推进技术,2009,30(5):610-617. ZHANG Guanghui,LIU Zhansheng.Performance analysis of high-speed hybrid gas bearings for rotating ramjet[J].Journal of Propulsion Technology,2009,30(5):610-617.(in Chinese)
    [18]
    张广辉,刘占生,章正传.旋转冲压发动机高速动静压混合气体轴承转子动力学特性试验研究[J].振动与冲击,2009,28(9):74-78. ZHANG Guanghui,LIU Zhansheng,ZHANG Zhengchuan. Dynamic behavior of a high-speed hybrid gas bearing-rotor system for a rotating ramjet[J].Journal of Vibration and Shock,2009,28(9):74-78.(in Chinese)
    [19]
    肖翔,赵晓路,徐建中.高压比旋转冲压叶轮研究[J].工程热物理学报,2008,29(5):759-762. XIAO Xiang,ZHAO Xiaolu,XU Jianzhong.A new kind of high performance shock-in impleller[J].Journal of Engineering Thermophysics ,2008,29(5):759-762.(in Chinese)
    [20]
    肖翔,刘锡阳,赵晓路,等.对转冲压压气机冲压叶栅实验研究[J].工程热物理学报,2009,30(11):1837-1840. XIAO Xiang,LIU Xiyang,ZHAO Xiaolu,et al.The cascade experimental investigation of counter-rotating ram-pressor[J].Journal of Engineering Thermophysics,2009,30(11):1837-1840.(in Chinese)
    [21]
    肖翔.对转冲压压气机冲压叶轮内部流动分析研究 .北京:中国科学院研究生院,2008. XIAO Xiang.The aerodynamic design and analysis of couter-rotating compressor's shock-in impeller .Beijing:Graduate University of Chinese Academy of Sciences,2008.(in Chinese)
    [22]
    钟兢军,韩吉昂.基于激波压缩技术的中空轴旋转冲压压缩转子:中国,ZL200710157305.3 .2009-12-16.
    [23]
    韩吉昂.旋转冲压压缩转子进气流道数值仿真及性能研究 .哈尔滨:哈尔滨工业大学,2009. HAN Ji'ang.Numerical simulation and performance research of flow-path in a ram-rotor .Harbin:Harbin Institute of Technology,2009.(in Chinese)
    [24]
    韩吉昂,钟兢军,卜方.旋转冲压压气机压缩转子技术分析及展望[J].飞航导弹,2007(7):52-56.
    [25]
    韩吉昂,严红明,钟兢军,等.旋转冲压压缩转子二维进气流道数值研究[J].航空动力学报,2008,23(6):1054-1060. HAN Ji'ang,YAN Hongming,ZHONG Jingjun,et al.Numerical research of two-dimensional flow-path in ram-rotor[J].Journal of Aerospace Power,2008,23(6):1054-1060.(in Chinese)
    [26]
    韩吉昂,钟兢军,严红明,等.旋转冲压压缩转子三维进气流道数值研究[J].航空动力学报,2009,24(5):1079-1088. HAN Ji'ang,ZHONG Jingjun,YAN Hongming,et al.Numerical research of three dimensional flow-path in a ram-rotor[J].Journal of Aerospace Power,2009,24(5):1079-1088.(in Chinese)
    [27]
    韩吉昂,孙鹏,钟兢军,等.旋转冲压压缩转子中压缩面的数值研究[J].工程热物理学报,2010,31(2):227-230. HAN Ji'ang,SUN Peng,ZHONG Jingjun,et al.Numerical research of compression ramp in a ram-rotor[J].Journal of Engineering Thermophysics,2010,31(2):227-230.(in Chinese)
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