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    Please use this identifier to cite or link to this item: http://chur.chu.edu.tw/handle/987654321/33785


    Title: Dynamica Measurement and Real Time Simulation of a Micro Turbojet Engine
    Authors: 楊一龍
    Yang, Yi-Lung
    Contributors: 機械工程學系
    Mechanical Engineering
    Keywords: 小型渦輪噴射引擎;bode plot;一 階系統;步階上升推力動態反應
    micro turbojet engine;bode plot;first order system;step change of engine thrust
    Date: 2005
    Issue Date: 2014-06-27 02:30:16 (UTC+8)
    Abstract: 本研究以雷虎小型渦輪噴射引擎做一動態性
    能之量測與模擬驗證,以做為噴射引擎推力輸出之
    動態模型開發之基礎。研究初期量測此引擎之穩態
    性能,並建構輸入油門電壓之大小與燃油率、推力
    與轉速之關連。其結果在高轉速由80000rpm 至
    120000rpm 之間接近一線性正比之關係式。在動態
    性能描述上採用Bode Plot 之頻率響應圖來建立引
    擎動態系統之轉移函數,透過其振幅之衰減與相位
    角之落後情形發現引擎轉速與推力之動態變化可
    以一階系統近似之,排氣溫則接近二階系統,而轉
    速與推力之反應幾乎同步,故以轉速
    In this study, a micro gas turbine engine
    (Thunder Tiger P-15) is used to formulate its dynamic transfer function and compare with the test
    data to understand the dynamic response of an engine.
    The steady-state performance of the jet engine is
    studied fir
    Appears in Collections:[Department of Mechanical Engineering] Journal Articles

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