Turbine Technologies Ltd - MiniLab Gas Turbine Power System

Description

MiniLabTM is a self-contained turbojet engine laboratory that's utilized globally by hundreds of leading educational, research and testing institutions. The systems National InstrumentsTM based data acquisition hardware and software displays and records compressor inlet temperature and pressure, turbine inlet temperature and pressure, turbine exit temperature and pressure, thrust and fuel flow and makes possible studies of: Brayton Cycle Compressor Performance Turbine Performance - work & power, expansion ratio, turbine efficiency Combustion/Emissions Analysis All engine support systems are fully integrated. The system is easily rolled to any convenient location. No dedicated test cell or facilities modifications are required. The time between delivery and first run is measured in minutes. The included data acquisition system makes real-time engine data display and recording effortless. A CAD models software package is also available to support CFD, FEA, or other turbomachinery related analysis activities. Equipped with the OneTouch Auto Start System, virtually anyone can operate the MiniLab. Start sequencing is completely automatic with all critical engine parameters monitored during operation. In the unlikely event of an engine fault, the OneTouch system will stop the engine and alert the operator to the problem.