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15 FIGURE 6-19: VELOCITY VECTORS (A) NEAR HUB AND (B) NEAR SHROUD, AT DESIGN POINT (N=40,000 RPM, PR=6.9).................................................................................................................................... 187 FIGURE 6-20: MACH NUMBER DISTRIBUTION AT OFF-DESIGN CONDITIONS (N=40,000 RPM, PR=3)..... 189 FIGURE 6-21: VELOCITY STREAMLINES AT OFF-DESIGN CONDITIONS (N=40,000 RPM, PR=3)................190 FIGURE 6-22: MACH NUMBER DISTRIBUTION AT OFF-DESIGN CONDITIONS (N=30,000 RPM, PR=3)..... 190 FIGURE 6-23: VELOCITY STREAMLINES AT OFF-DESIGN CONDITIONS (N=30,000 RPM, PR=3)................191 FIGURE 6-24: MACH NUMBER DISTRIBUTION AT OFF-DESIGN CONDITIONS (N=30,000 RPM, PR=7)..... 191 FIGURE 6-25: VELOCITY STREAMLINES AT OFF-DESIGN CONDITIONS (N=30,000 RPM, PR=7)................192 FIGURE 6-26: PARAMETRIC STUDY USING ANSYS FOR THE PROPOSED TURBINE. .................................. 192 FIGURE 7-1: SCHEMATIC OF THE TEST BENCH. ........................................................................................ 199 FIGURE 7-2: DESCRIPTION OF THE TEST COMPONENTS. ......................................................................... 201 FIGURE 7-3: DESCRIPTION OF THE ORC COMPONENTS. .......................................................................... 201 FIGURE 7-4: : (TOP) EXHAUST HEAT DIESEL ENGINE MAP, (BOTTOM) THE NON-ROAD TRANSIENT CYCLE (NRTC) PROTOCOL............................................................................................................................203 FIGURE 7-5: THERMAL OIL–EXHAUST GAS HEAT EXCHANGER (MAIN HEAT EXCHANGER). .................... 204 FIGURE 7-6: HEAT EXCHANGERS (TOP) AND FLOW CONFIGURATION (BOTTOM). .................................. 205 FIGURE 7-7: COMPONENTS OF THE RADIAL-INFLOW TURBINE. .............................................................. 206 FIGURE 7-8: TURBO-GENERATOR UNIT. ................................................................................................... 207 FIGURE 7-9: INSTRUMENTATIONS APPLIED IN THE TEST RIG. ................................................................. 208 FIGURE 7-10: EFFECT OF HEAT SOURCE TEMPERATURE ON WORKING FLUID AND OIL TEMPERATURE. 210 FIGURE 7-11: EFFECT OF HEAT SOURCE TEMPERATURE ON WORKING FLUID AND OIL PRESSURES. ..... 210 FIGURE 7-12: EFFECT OF WORKING FLUID MASS FLOW RATE ON TURBINE INLET PRESSURE. ............... 211 FIGURE 7-13: RELATIONSHIP BETWEEN OIL POWER AND ELECTRICAL POWER....................................... 211 FIGURE 7-14: ENERGY BALANCE THROUGH THE MAIN HEAT EXCHANGER. ............................................ 212 FIGURE 7-15: CYCLE EFFICIENCY EVOLUTION WITH TIME. ...................................................................... 213 FIGURE 7-16: POWER GENERATION WITH SPEED. ................................................................................... 214 FIGURE 7-17: POWER GENERATION WITH TURBINE PRESSURE RATIO AT 20,000 RPM. ......................... 214 FIGURE 7-18: TURBINE ISENTROPIC EFFICIENCY AT TWO SPEEDS. .......................................................... 216 FIGURE 7-19: VARIATION OF POWER WITH WORKING FLUID MASS FLOW RATES. ................................ 217 FIGURE 7-20: VARIATION OF POWER WITH TURBINE SPEED................................................................... 217 FIGURE A-0-1: CREATION OF STATOR 3D MODEL. ................................................................................... 248PDF Image | Automotive Radial Turbine Expander Design WHR
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