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Optimised Radial Turbine Design D1.8

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Optimised Radial Turbine Design D1.8 ( optimised-radial-turbine-design-d18 )

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called scalloping. Scalloping is used to reduce the mass and the inertia of the turbine rotor and also to reduce the stresses at the point of contact between the back face of the rotor and the rotating shaft. 2.1- GAS TURBINE CYCLE ANALYSIS: The overall specifications of the micro-gas turbine requires for the demonstration plant have been decided by the project consortium based on overall system considerations. Following this step, Cycle analysis and optimisation was performed at City University London to determine cycle parameters required for the design of the micro-gas turbine components. This subsection outlines the main outcomes of the cycle analysis pertinent to the design of the turbine. The micro-gas turbine is based on a simple recuperated cycle as shown in Figure 3, where the receiver replaces the combustion chamber. A design point Turbine Inlet Temperature (TIT) of 800oC was specified by KTH as the maximum achievable for the demonstration plant. However, higher temperatures will be targeted for the final optimised system. Figure 3: Schematic diagram of the micro-gas turbine cycle. Table 1 shows the component parameters specified for the cycle analysis based on estimated achievable component efficiencies. Table 1: Micro-gas turbine components parameters Parameter value Ambient temperature Ambient pressure Compressor efficiency 74% Turbine efficiency 80% Recuperator effectiveness 85% Receiver efficiency 80% Electrical efficiency 90% Using these parameters, cycle analysis was performed for a range of compressor pressure ratios (PRc), (TIT) and turbine exit temperature (TET). Estimated component pressure losses were also taken into consideration. Figure 4 shows a summary of the cycle analysis results which allowed for specifications required for the turbine design. 288.15K 1.01325bar 4

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