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FIGURE 3-49 STRESS AND DISPLACEMENT DISTRIBUTION CONTOUR PLOTS, (TOP) DUE TO PRESSURE, (BOTTOM) DUE TO ROTATION .............................................................................................................. 118 FIGURE 4-1 FEA OF THE COMPLETE TURBINE ASSEMBLY................................................................... 123 FIGURE 4-2 CAD MODEL OF THE COMPLETE TURBINE ASSEMBLY, (LEFT) SECTION VIEW, (RIGHT) ISOMETRIC VIEW.................................................................................................................................. 124 FIGURE 4-3 CAD MODEL OF THE COMPLETE TURBINE ASSEMBLY EXPLODED VIEW .......................... 125 FIGURE 4-4 MANUFACTURED TURBINE COMPONENTS WITH 3-D PRINTING ....................................... 127 FIGURE 4-5 SCHEMATIC OF THE EXPERIMENTAL COMPRESSED AIR RIT TEST FACILITY .................... 129 FIGURE 4-6 FABRICATED EXPERIMENTAL FACILITY FOR TESTING THE COMPRESSED AIR RIT........... 130 FIGURE 4-7 ELECTRICAL WIRING DIAGRAM OF THE PRESSURE TRANSDUCER .................................... 135 FIGURE 4-8 APPARATUS FOR CALIBRATION OF THE THERMOCOUPLES............................................... 137 FIGURE 4-9 CALIBRATION CURVE FOR THERMOCOUPLE-1 ................................................................. 137 FIGURE 4-10 APPARATUS FOR CALIBRATION OF THE PRESSURE TRANSDUCERS ................................ 138 FIGURE 4-11 CALIBRATION CURVE FOR ONE OF GE UNIK 5000 TRANSDUCER ................................. 138 FIGURE 4-12 VALIDATION OF CFD MODEL WITH EXPERIMENTAL RESULTS (POWER AND EFFICIENCY) FOR THE TURBINE INLET TEMPERATURE OF 20°C ............................................................................... 144 FIGURE 4-13 VALIDATION OF CFD MODEL WITH EXPERIMENTAL RESULTS (POWER AND EFFICIENCY) FOR THE TURBINE INLET TEMPERATURE OF 25°C ............................................................................... 145 FIGURE 4-14 VALIDATION OF CFD MODEL WITH EXPERIMENTAL RESULTS (POWER AND EFFICIENCY) FOR THE TURBINE INLET TEMPERATURE OF 30°C ............................................................................... 146 FIGURE 4-15 VALIDATION OF CFD MODEL WITH EXPERIMENTAL RESULTS (POWER AND EFFICIENCY) FOR THE TURBINE INLET TEMPERATURE OF 35°C ............................................................................... 147 FIGURE 4-16 VALIDATION OF CFD MODEL WITH EXPERIMENTAL RESULTS (POWER AND EFFICIENCY) FOR THE TURBINE INLET TEMPERATURE OF 40°C ............................................................................... 148 FIGURE 4-17 COMPARISON OF EFFICIENCY FROM CFD SIMULATIONS WITH EXPERIMENTS FOR ALL DATA POINTS ................................................................................................................................................. 150 FIGURE 4-18 COMPARISON OF POWER FROM CFD SIMULATIONS WITH EXPERIMENTS FOR ALL DATA POINTS ................................................................................................................................................. 151 FIGURE 5-1 TEMPERATURE-ENTROPY DIAGRAM OF THE SELECTED FLUIDS ....................................... 159 FIGURE 5-2 SCHEMATIC OF SIMPLE ORC LAYOUT.............................................................................. 160 FIGURE 5-3 SCHEMATIC OF THE ROTOR BLADE PROFILES AND VELOCITY TRIANGLES, ROTOR WITH ZERO INLET BLADE ANGLE (A), ROTOR WITH NON-ZERO INLET BLADE ANGLE (B AND C)............................ 165 FIGURE 5-4 SCHEMATIC OF THE VOLUTE GEOMETRY ......................................................................... 168 FIGURE 5-5 ALGORITHM FOR INTEGRATION OF ORGANIC RIT MODEL AND ORC MODEL BASED ON REAL- GAS FORMULATION.............................................................................................................................. 171 XIIPDF Image | SMALL-SCALE RADIAL INFLOW TURBINE FOR WHR ORC
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