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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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Figure number and title Table of Figures 1.2.1 Rankine Cycle process 1.2.2 High efficiency AMS cycle 1.2.3 Effects of pressure ratio on AMS performance for fixed T7 1.2.4 Relative contribution to achieve 40% electrical efficiency 1.2.5 T4-T7 relationship for AMS cycle 1.2.6 Payback years for alternative recuperator technologies 2.1.1 Relative Mach distribution for ceramic vane/rotor Gen 1 design 2.1.2 Steady-state full-power heat transfer coefficients 2.1.3 Sample endwall contouring of blade platform 2.1.4 Convection heat transfer coefficient distribution on blade surface 2.1.5 Circumferentially-averaged convective heat transfer coefficient and driving temperature on the shroud 2.1.6 Cold-day startup transient 2.1.7 Maximum thermal stress in the vane during transient shutdown 2.1.8 Temperature gradients and thermal stress during steady-state 2.1.9 Thermal stress during tip shutdown after 8 sec 2.1.10 Design concept for slotted ceramic shroud 2.1.11 Temperature distribution and thermal stress of the shroud under hot streak conditions 2.1.12 Radial deflection and maximum principle stress for a spinning disk only 2.1.13 Temperature and maximum principle stress for rotor with blade pull 2.1.14 Self sustaining radius determination for ST5+ rotor disk 2.1.15 Cold spin distribution of rotor maximum principle stress 2.1.16 Cold spin rim hoop and radial stress 2.1.17 Hot spin temperature and maximum principle stress 2.1.18 Hot spin radial and hoop rim stress 2.1.19 Startup midspan blade sink temperature and rotor speed in time 2.1.20 Startup rotor maximum principle stress 2.1.21 Emergency shutdown blade and midspan sink temperature and rotor speed in time 2.1.22 Emergency shutdown maximum principle stress with time 2.1.23 Partitioning of IBR FEA into representative data sets for CARES analysis 2.1.24 Predicted cT blade recession over 25,000 hours of microturbine operation 2.1.25 Brazed attachment and wedge attachment 2.1.26 Brazed-Wedge attachment concept 2.1.27 Brazed-Wedge attachment FEA results 2.1.28 Brazing trials specimens 2.1.29 Effect of zirconia TBC spall impact on rotor blade at 100% speed 2.1.30 ST5 andST5+ leading edge FOD impact results 2.1.31 Multi-axis machined vane ring at Kyocera 2.1.32 Multi-axis machined silicone nitride vane rings 2.1.33 Typical defects seen in “reject” vane ring 2.2.1 Isometric view of combustor assembly 6

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