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To start the mean line design calculation; two sets of data need to be provided to the design program. The first is taken from the gas turbine cycle analysis; the parameters needed from the cycle analysis are: Turbine inlet total temperature. Turbine inlet total pressure. Mass flow rate. Required output shaft power. The second set comprises empirical relations that are combination of performance and dimensionless ratios available. In the next sub sections those sets of data would be discussed in more details. Based on the data gained from cycle analysis and literature, the velocity triangle (figure 5), stagnation and static temperature and pressure and rotor inlet diameter and blade height can be calculated. The majority of the internal rotor losses are functions of the fluid velocity, and to improve the efficiency of the rotor the velocity at rotor inlet should be reduced as much as possible to reduce the incidence loss occurring at the rotor inlet. The loading coefficient would be used to minimise the fluid velocity at the rotor inlet. Figure 5: Velocity triangle at rotor inlet. The velocity triangle components at the rotor inlet are related by the following equation: And from the definition of the loading coefficient ( ) the previous equation become: The solution for this equation is [ ( )]=0 √( ) 6PDF Image | Optimised Radial Turbine Design D1.8
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