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ADVANCED MICROTURBINE SYSTEMS Final Report for Tasks 1 Through 4 and Task 6

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ADVANCED MICROTURBINE SYSTEMS Final Report for Tasks 1 Through 4 and Task 6 ( advanced-microturbine-systems-final-report-tasks-1-through-4 )

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Data were acquired to characterrize each microturbine and the ORC components. It became apparent that characterizing the C200 electrical power, exhaust energy, and energy losses from the C200 cabinet was important. Individual electrical power meters were used for each microturbine, and the exhaust energy was determined from individual measurements of temperature and flow at the locations shown in Figure 3.1.3. Also indicated are the two roof vents on each microturbine enclosure. Internal blowers draw outside air through the electronic or engine compartments and discharge it through the respective vent. Energy loss through the vents was calculated from integrating temperature and velocity measurements made over the vent exit area. Auxilary cooling vents #4 metering probe (VOLU-probe) #3 metering probe T3 #4 #3 T4 Figure 3.1.3 Microturbine measurements for exhaust and lost energy 3.2 C200 Performance Figure 3.2.1 plots C200 electrical efficiency data for a modest range of ambient temperature and backpressure. Both plots include the predictions of the same according to Capstone’s Design Review document. In the first plot, the data show that the turbine efficiency is 33 % at about 37F ambient temperature without backpressure. This is very consistent with prediction. Efficiency levels with backpressure were reduced by 1⁄2%. The second plot recasts the same data according to backpressure. The 4 to 5 in H2O positive backpressure variation was achieved by varying the blower speed. The prediction for loss of efficiency with backpressure is extremely accurate. 73 Power electronics Engine compartment

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