Gas turbine experimental device

The equipment manufactured by the American Gas Turbine (Turbine Technologies Ltd.). Mainly used to study the gas turbine cycle process and how it works. Overall MiniLab experimental gas turbine power system summary: The equipment manufactured by the American Gas Turbine (Turbine Technologies Ltd.). Mainly used to study the gas turbine cycle process and how it works. Main features: according to the aviation standard design, manufacture of gas turbine engines, with the highest levels of stability. Designed for engineering design and production of teaching critical system parameters are displayed on the console, with "a key to start" button and LCD display can monitor equipment running status, time and cycles accumulated running, a virtual reality engine pushrod engine design placed in the protective cover (polycarbonate), the gas turbine can be clearly observed before and after the whole process of running the engine can be equipped with a muffler, the noise can be used to study the device can use a variety of types of fuels, including gasoline, kerosene, diesel, etc., and without Preheat can be connected via USB DigiDAQTM data acquisition system, and experiment with LabVIEW software equipment parts all designed and manufactured in the United States, to meet the standard that is to ABET4 and ABET6, no need to purchase or add to the combustion chamber components and other equipment guide vane ring are used Inconel 718 alloy casting, turbine impeller CMR 247 super alloys experimental features: the gas turbine system can be analyzed in compressor components, such as calculating the actual pressure ratio of the compressor, the compressor output, compressor Speed ??and efficiency compressor gas turbine system can be analyzed in turbine components, the total power and the turbine output power, such as computing systems, turbine expansion ratio and turbine efficiency gas turbine system can The combustor components analysis, such as the ratio of the combustion process of air and fuel, the impact of excess air of combustion burners and combustion efficiency of the entire cycle gas turbine system can be analyzed, including the mass flow rate of the system, the compressor turbine inlet and outlet air velocity, temperature and pressure of each measuring point, the combustion efficiency of the system and thermal efficiency, thrust, etc.