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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. Ballin, Mark G. Ames Research Center DIGITAL SIMULATION; FLIGHT SIMULATION; HELICOPTERS; REAL TIME OPERATION; TURBINE ENGINES; TURBOSHAFTS; CONTROL SYSTEMS DESIGN; MODELS; ROTOR BLADES...
A hybrid computer simulation of an Advanced Automotive Gas Turbine Powertrain System is reported. The system consists of a gas turbine engine, an automotive drivetrain with four speed automatic transmission, and a control system. Generally, dynamic performance is simulated on the analog portion of the hybrid computer while most of the steady state performance characteristics are calculated to run faster than real time and makes this simulation a useful tool for a variety of analytical studies. Costakis, W. and Merrill, W. C. Glenn Research Center NASA-TM-83593, E-1994, DOE/NASA/51040-52, NAS 1.15:83593 DE-AI01-77CS-51040; RTOP 505-34-02...