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Optimization has been carried out by varying turbine inlet pressure, superheated temperature and condenser temperature as design variables.
Turbine inlet pressure, superheated temperature and condenser temperature are assumed to be 29.5 bar, 410 K and 386.6 K respectively as the values assigned to this point.
However, in the case of low superheated temperature, the liquid argon films evaporate gradually with no explosive boiling.
For the case of high superheated temperature, the phase transition of argon films is so rapid that the explosive boiling occurs at the initial variation period.
Consequently, the calculated heat loss is based on the exposure of 100%% depleted model, filled with steam either at the saturation or superheated temperature, to the surrounding environment.
(a) Surface 0, (b) surface 1, (c) surface 3, and (d) surface 4. Figure 13 shows the net evaporation number for the case of low superheated temperature.
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The amount of Laves phase decreases with increasing of melt superheating temperature from 1380 to 1680 °C.
The optimum superheat temperature is found to be 600 °C for a backpressure turbine with single extraction.
At low wall superheat temperatures, the heat sink operates under the thin film evaporation heat transfer mode and then transitions to the boiling heat transfer mode when the wall superheat temperature increases.
For each particular micromodel, range of the steam temperature was considered from the dry saturated steam temperature (100 °C) to maximum experienced superheating temperature.
The system COP sensitivity with regard to inlet single-phase temperatures, superheat temperature and conductance of heat exchangers (UA), is examined.
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