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Jet Engine Testing Application Summary One company located in Chetek, Wisconsin, supplies a full working gas turbine, called the MiniLab Gas Turbine Power System, specifically intended for universities and technical institutes. Turbine Technologies, Ltd. developed the SR-30 engine and test stand based on its experience working in the aerospace industry. Over 100 universities, colleges, and research institutes are currently using the turbines for various studies. Potential Solution IOtechs Solution Turbine Technologies customers are sophisticated and extremely discerning and expect to have the best system they can possibly obtain, says Kutrieb. In order to satisfy these users, Turbine Technologies supplied the Minilab embedded with IOtechs hardware and software which lets them design their own Virtual Instruments and customize graphics. Personal Daqs are supplied with Personal DaqView, IOtechs Windows®-based data logging application software that lets users set up their own acquisition applications and save acquired data directly to disk. The system also includes eZ-PostView, a post-acquisition application, drivers for Visual Basic®, and C/C++® for Windows®. Users can obtain drivers for icon-based software packages LabVIEW® and DASYLab®. Many customers also download their data to Excel® spreadsheets. Turbine Technologies customers use the Minilab for many research projects, which include biodiesel fuel studies, comparing Proportional-Integral-Derivative (PID) with Fuzzy Logic Controls (FLC), Brayton cycle studies, basic principles of operation, inlet cooling studies, large scale scientific computing, and various fuel studies, to name a few. Such a wide variety of diverse tests are made possible with the Minilabs OneTouch Auto Start System, says Kutrieb. It provides an automatic start sequence with all critical engine parameters monitored during operation. In the event of a problem, the engine will automatically stop safely and alert the operator. No special training is required to operate the MiniLab system. Biodiesel fuel studies employed new and used vegetable oil and the students collected data, which allowed them to appreciate the engines flexibility to accommodate alternate fuels, and compute its efficiency and temperature, among other parameters. The PID vs. FLC studies were undertaken to provide alternative methods in improving overall engine control. In this study, soft-computing technologies were demonstrated in a real hardware-in-the-loop environment. Brayton cycle studies required pressure sensors for measuring compressor inlet static pressure, compressor stage exit stagnation pressure, combustion chamber pressure, turbine exit stagnation pressure, and thrust nozzle exit stagnation pressure. The studies also used thermocouples to measure, compressor inlet static temperature, compressor stage exit stagnation temperature, turbine stage inlet stagnation temperature, turbine stage exit stagnation temperature, and thrust nozzle exit stagnation temperature. Numerous universities and colleges currently use the Minilab for special and general studies, including Auburn University, Auburn, Ala.; the University of Wisconsin, Platteville, Wis.; India Institute of Technology, Bombay, India; Cairo University, Cairo, Egypt; and NASAs Marshall Space Flight Center, Huntsville, Ala. Additional programs concerning basic principles of turbine operation, inlet cooling studies, large scale scientific computing, and various fuel studies, can be reviewed in the respective technical papers listed at Turbine Technologies Web site, www.turbinetechnologies.com. Conclusion |