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DEVELOPMENT OF AN ULTRA-HIGH EFFICIENCY GAS TURBINE ENGINE (UHEGT

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DEVELOPMENT OF AN ULTRA-HIGH EFFICIENCY GAS TURBINE ENGINE (UHEGT ( development-an-ultra-high-efficiency-gas-turbine-engine-uheg )

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over the injectors, uses the lowest number of injectors per blade, generates almost the same amount of power as other configurations, and it is the easiest configuration to manufacture. No further cooling would be required while using this configuration. Therefore, configuration 2 can be considered as the best option in reducing the stator blade surface temperature among the cases studied in this research. However, it should be noted that higher NUI in configuration 2 compared to other configurations leads to more hotspots in rotor which could negatively affect the rotor blade material and blade life [66], [69]. Therefore, if this configuration is used, rotor surface temperature should be studied closely, and appropriate cooling strategy should be employed. The second-best option would be configuration 4 which uses film cooling and effectively reduces the average surface temperature by more than 100 degrees. This configuration produces a highly uniform temperature distribution at the rotor inlet as well. Finally, it should be mentioned that for the second and third turbine stages with stator internal combustion, a similar approach could be used to optimize the temperature distribution. Based on the results presented in section V.4, the temperature distribution in each stage is mainly dependent on the arrangement of the burners in the same stage. That means most hotspots are damped and the temperature distribution is more uniform at the exit of each stage due to the interactions with rotor. Therefore, the fuel injectors need to be indexed based on the flow patterns and temperature distribution in each stage. Moreover, use of film cooling is recommended for the rotor blades. 112

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