A high-fidelity component-type model and real-time digital simulation of the General Electric T700-GE-700 turboshaft engine were developed for use with current generation real-time blade-element rotor helicopter simulations. A control system model based on the specification fuel control system used in the UH-60A Black Hawk helicopter is also presented. The modeling assumptions and real-time digital implementation methods particular to the simulation of small turboshaft engines are described. The validity of the simulation is demonstrated by comparison with analysis-oriented simulations developed by the manufacturer, available test data, and flight-test time histories.


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    Title :

    High Fidelity Real-Time Simulation of a Small Turboshaft Engine


    Contributors:

    Publication date :

    1988


    Size :

    95 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English






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