Volume 28 Issue 2
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CHAN Shi-ning, LIU Huo-xing, HU Xiao-yu. Wave system analyses of four-port through-flow wave rotors[J]. Journal of Aerospace Power, 2013, 28(2): 410-417.
Citation: CHAN Shi-ning, LIU Huo-xing, HU Xiao-yu. Wave system analyses of four-port through-flow wave rotors[J]. Journal of Aerospace Power, 2013, 28(2): 410-417.
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Wave system analyses of four-port through-flow wave rotors

  • 1.

    National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics, School of Energy and Power Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China

  • 2.

    Project Department, Aviation Industry Corporation of China, Beijing 100012, China

  • Received Date: 2012-03-01
  • Publish Date: 2013-02-28
    Abstract
  • Aiming at four-port through-flow wave rotors used in gas turbines,the pressure wave system inside the channels was simplified,and analytic models were established and proved with foreign experimental results.The analytic wave system models were finally used to analyze the relationships among boundary conditions,wave structures,wave rotor performances,and parameters of other components such as compressors,turbines or combustors.The results show that:the rise of high pressure air (HPA) static pressure could effectively increase the wave rotor pressure ratio,as a result of strengthened entire wave system;the wave rotor performances could be optimized by properly designing the compressors and turbines;the matching of wave rotors and combustors could restrict the combustor design,while the rise of combustor total pressure recovery could enhance the wave rotor compression efficiency.

     

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    • References(16)
  • [1]
    Akbari P,Nalim R,Müller N.A review of wave rotor technology and its applications[C]//Proceedings of 2004 ASME International Mechanical Engineering Congress.California,USA:ASME,2004:1-23.
    [2]
    Iancu F,Müller N.Efficiency of shock wave compression in a microchannel[J].Microfluid Nanofluid,2006,2(1):50-63.
    [3]
    Iancu F,Akbari P,Müller N.Feasibility study of integrating four-port wave rotors into ultra-micro gas turbines (UμGT)[C]//Proceedings of 40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit.Florida,USA:AIAA,2004:1-12.
    [4]
    Akbari P,Müller N.Performance investigation of small gas turbine engines topped with wave rotors[C]//Proceedings of 39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit.Alabama,USA:AIAA,2003:1-11.
    [5]
    Dempsey E,Müller N,Akbari P,et al.Performance optimization of gas turbines utilizing four-port wave rotors[C]//Proceedings of 4th International Energy Conversion Engineering Conference and Exhibit.San Diego,California,USA:AIAA,2006:1-14.
    [6]
    Welch G E.Macroscopic balance model for wave rotors[C]//Proceedings of 34th Aerospace Sciences Meeting and Exhibit.Reno,Nevada:AIAA,1996:1-20.
    [7]
    Wilson J,Welch G E,Paxson D E.Experimental results of performance tests on a four-port wave rotor[C]//Proceedings of 45th AIAA Aerospace Sciences Meeting and Exhibit.Reno,Nevada:AIAA,2007:1-16.
    [8]
    Akbari P,Nalim R,Donovan E S,et al.Leakage assessment of pressure-exchange wave rotors[J].Journal of Propulsion and Power,2008,24(4):732-740.
    [9]
    Edwin L R J,Mocsari J C,Nalim M R.Analytic methods for design of wave cycles for wave rotor core engines[C]//Proceedings of AIAA/SAE/ASME/ASEE 29th Joint Propulsion Conference and Exhibit.Monterey,CA:AIAA,1993:1-12.
    [10]
    Akbari P,Müller N.Gas dynamic design analyses of charging zone for reverse-flow pressure wave superchargers[C]//Proceedings of 2003 Spring Technical Conference of the ASME Internal Combustion Engine Division.Salzburg,Austria:ASME,2003:1-11.
    [11]
    Iancu F,Piechna J,Müller N.Basic design scheme for wave rotors[J].Shock Waves,2008,18(5):365-378.
    [12]
    Poho r ˇ elskL,San P,Rozsas T,et al.Wave rotor design procedure for gas turbine enhancement[C]//Proceedings of ASME Turbo Expo 2008:Power for Land,Sea and Air.Berlin,Germany:ASME,2008:1-14.
    [13]
    Iancu F,Zhu X,Tang Y,et al.Design and fabrication of microchannel test rig for ultra-micro wave rotors[J].Microsyst Technol,2007,14(1):79-88.
    [14]
    Piechna J,Cerpa R,Marcin S,et al.Numerical analysis of the wave topping unit for small turbojet[C]//Proceedings of ASME Turbo Expo 2010:Power for Land,Sea and Air.Glasgow,UK:ASME,2010:1-9.
    [15]
    Spring P,Onder C H,Guzzella L.EGR control of pressure-wave supercharged IC engines[J].Control Engineering Practice,2007,15(12):1520-1532.
    [16]
    Paxson D E,Wilson J,Welch G E.Comparison between simulated and experimentally measured performance of a four port wave rotor[C]//Proceedings of 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.Cincinnati,OH:AIAA,2007:1-16.
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