Volume 28 Issue 5
May  2013
Turn off MathJax
Article Contents
LIU Shuai, WANG Zhan-xue, CAI Yuan-hu, LIU Zeng-wen. Simulation and analysis of performance for combination of lift fan and turbofan engine power system[J]. Journal of Aerospace Power, 2013, 28(5): 1095-1100.
Citation: LIU Shuai, WANG Zhan-xue, CAI Yuan-hu, LIU Zeng-wen. Simulation and analysis of performance for combination of lift fan and turbofan engine power system[J]. Journal of Aerospace Power, 2013, 28(5): 1095-1100.

Simulation and analysis of performance for combination of lift fan and turbofan engine power system

  • Received Date: 2012-05-19
  • Publish Date: 2013-05-28
  • Based on component matching and multi-point analysis,a turbofan plus lift fan engine performance simulation model was developed.The model was tested by the F135 engine.The simulation results show that the engine performance is the same as the conventional turbofan in cruise mode.When the lift fan is engaged,the matching point between the low pressure turbine,the cruise fan and the lift fan is achieved by adjusting the nozzle throat area,the bypass exit area,and the low pressure turbine throat area.Based on this model,the cycle parameter matching and performance analysis can be achieved for the turbofan plus lift fan engine in different missions.

     

  • loading
  • [1]
    Biesiadny T J,Mcardle J G,Esker B S.Overview of STOVL aircraft propulsion research offtakes and vertical lift systems[R].AIAA 1993-4865,1993.
    [2]
    Wilson S B,White K C.Technology impact on STOVL and CTOL strike fighters[R].AIAA 1993-4851,1993.
    [3]
    Lewis W D.Fundamentals of V/STOL design with joint-strike fighter applications:an international cooperative effort[R].AIAA 2000-0805,2000.
    [4]
    Bevilaqua P M.Inventing the F-35 joint strike fighter[R].AIAA 2009-1650,2009.
    [5]
    郑志成,周洲.垂直起降飞机设计中升力风扇估算模型分析[J].飞行力学,2010,28(3):21-23. ZHENG Zhicheng,ZHOU Zhou.Analysis on the estimation model of lift fan when designing VTOL[J].Flight Dynamics,2010,28(3):21-23.(in Chinese)
    [6]
    PrzedpelskiZ J.Lift fan technology studies[M].Cincinnati,US:General Electric Company,1967.
    [7]
    Przedpelski Z J.Lift fans for advanced V/STOL aircraft[R].AIAA 1965-708,1965.
    [8]
    Hill D C,Wasters M H.Conceptual design of a lift fan plus lift/cruise fighter aircraft[R].AIAA 1974-969,1974.
    [9]
    Bevilaqua P M.Joint strike fighter dual-cycle propulsion system[J].Journal of Propulsion and Power.2005,21(5):778-783.
    [10]
    Philpot M G,Kirk J A,Britton A J.ASTOVL aircraft mission performance sensitivity studies[R].AIAA 1993-4849,1993.
    [11]
    Perez R E,Behdinan K.Effective multi-mission aircraft conceptual design optimization using a hybrid multi-objective evolutionary method[R].AIAA-2002-5464,2002.
    [12]
    Bevilaqua P.Future applications of The JSF variable propulsion cycle[R].AIAA 2003-2614,2003.
    [13]
    Sellers J F,Daniel C J.DYNGEN:a program for calculating steady state and transient performance of turbojet and turbofan engines[R].NASA-TN-D-7901,1975.
    [14]
    Varelis A G.Variable cycle engine for combat STOVL aircraft[D].Cranfield,UK:Cranfield University,2007.
    [15]
    王华青,陈矛章.发动机的涡轮导向器面积、喷口直径等匹配参数调整的计算方法研究和应用[J].航空动力学报,2002,17(2):145-149. WANG Huaqing,CHEN Maozhang.Study and application of calculation method for adjusting the matching parameters of turbine nozzle area and engine nozzle radius[J].Journal of Aerospace Power,2002,17(2):145-149.(in Chinese)
  • 加载中

Catalog

    通讯作者: 陈斌, bchen63@163.com
    • 1. 

      沈阳化工大学材料科学与工程学院 沈阳 110142

    1. 本站搜索
    2. 百度学术搜索
    3. 万方数据库搜索
    4. CNKI搜索

    Article Metrics

    Article views (2095) PDF downloads(1232) Cited by()
    Proportional views
    Related

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return