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Thermal Performance and Operation of a Solar Tubular Receiver With CO2 as the Heat Transfer Fluid
14
Citations
9
References
2017
Year
EngineeringEnergy EfficiencyEnergy ConversionThermal Energy StoragePhotovoltaicsSolar Radiation PressureHigh-pressure Solar ReceiverSolar Thermal EnergySolar Energy UtilisationElectrical EngineeringEnergy HarvestingAbengoa Solar NtSolar PowerReceiver Cavity ApertureIn-space Electric PowerThermal PerformanceSolar Tubular ReceiverHeat TransferHeat Transfer FluidSolar CoolingThermal EngineeringHeat ExchangerHeat Transfer EnhancementEnergy Recovery
A high-temperature, high-pressure solar receiver was designed as part of the advanced thermal energy storage project carried out in collaboration with Abengoa Solar NT at CSIRO Energy Centre in Newcastle, Australia, with support through the Australian Renewable Energy Agency (ARENA). The cavity-type receiver with tubular absorbers was successfully installed and commissioned, using concentrated solar energy to raise the temperature of CO2 gas to 750 °C at 700 kPa in a pressurized, closed loop system. Stand-alone solar receiver tests were carried out to investigate the thermal characteristics of the 250 kWt solar receiver. The on-sun full-load test successfully achieved an outlet gas temperature of 750 °C while operating below the maximum allowable tube temperature limit (1050 °C) and with a maximum pressure drop of 22 kPa. The corresponding estimated receiver thermal efficiency values at full flow rate were 75% estimated based on measured receiver temperatures and heat losses calculations for both single aim-point and multiple aim-point heliostat control strategies. The use of a quartz glass window affixed to the receiver cavity aperture was tried as a means for improving the receiver efficiency by reducing convective heat losses from the receiver aperture. However, while it did appear to significantly reduce convective losses, a more effective metal support frame design is necessary to avoid damage to the window caused by stresses introduced as a result of distortion of the supports due to heating by the spillage of rays from the heliostat field.
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