Gas Turbine Simulation Program
Dear,I am Using GSP software to simulate a turbojet engine.I combined all the main components and I want to plot the speed with thrust so I added two components ('Rotor Speed ctrl' and 'Thrust ctrl' )Then the Program asked me (Nr. 0 component Rotor Speed Ctrl and Thrust Ctrl are a deprecated component! Recommended to use generic equation schedule components).So I added Generic schedule control with a combined equation, but I don't know how to connect between it and Speed and thrust components. Also, there an equation I have to write it.Is anyone familiar with the GSP program please give me your advice on what should I do to solve this hint from software and run the components?I hope if there is training for this software or videosKindly.
This example models a gas turbine auxiliary power unit (APU) based on the Brayton Cycle. The Compressor and Turbine blocks are custom components based on the Simscape™ Foundation Gas Library. The power input to the system is represented by heat injection into the combustor; actual combustion chemistry is not modeled. A single shaft connects the compressor and the turbine so that the power from the turbine drives the compressor.
Gas Turbine Simulation Software
The APU is a free turbine that further expands the exhaust stream to produce output power.Three PID controllers regulate the shaft speed, the turbine inlet temperature, and the compressor surge margin. System inputs are defined for three scenarios: varying shaft speed, varying surge margin, and varying APU vane opening. Running the first scenario produces the typical operating line on the compressor map. Running the second and third scenarios show where the maximum power output and maximum global efficiency occurs.