首页> 外文会议>ASME international mechanical engineering congress and exposition >COMPARATIVE ENERGY AND EXERGY ANALYSIS OF PROPOSED GAS TURBINE CYCLE WITH SIMPLE GAS TURBINE CYCLE AT SAME OPERATIONAL COST
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COMPARATIVE ENERGY AND EXERGY ANALYSIS OF PROPOSED GAS TURBINE CYCLE WITH SIMPLE GAS TURBINE CYCLE AT SAME OPERATIONAL COST

机译:拟议的燃气轮机与简单燃气轮机以相同的运营成本进行比较的能量和能量分析

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Environmentally friendly and effective power systems have been receiving increased investigation due to the aim of addressing global warming, energy expansion, and economic growth. Gas turbine cycles are perceived as a useful technology that has advanced power capacity. In this research, a gas turbine cycle has been proposed and developed from a simple and regenerative gas turbine cycle to enhance performance and reduce Specific fuel consumption. The impact of specific factors regarding the proposed gas turbine cycle on thermal efficiency, net output, specific fuel consumption, and exergy destruction, have been inspected. The assessments of the pertinent parameters were performed based on conventional thermodynamic energy and exergy analysis. The results obtained indicate that the peak temperature of the Proposed Gas Turbine Cycle increased considerably without affecting fuel consumption. The results show that at Pressure Ratio (r_p =6) the performance of the Proposed Gas Turbine Cycle is much better than Single Gas Turbine Cycle but the total exergy destruction of Proposed Gas Turbine Cycle higher than the SGTC.
机译:为了解决全球变暖,能源膨胀和经济增长的目的,环保,有效的电力系统已受到越来越多的研究。燃气轮机循环被认为是具有先进功率能力的有用技术。在这项研究中,提出了一种燃气轮机循环,并从一种简单的再生式燃气轮机循环中发展出来,以提高性能并降低比燃料消耗。已经检查了有关提议的燃气轮机循环的特定因素对热效率,净输出,比燃料消耗和火用破坏的影响。相关参数的评估是基于常规热力学能量和火用分析进行的。获得的结果表明,拟议的燃气轮机循环的峰值温度显着增加,而不会影响燃料消耗。结果表明,在压力比(r_p = 6)时,拟议的燃气轮机循环的性能远优于单燃气轮机循环,但拟议的燃气轮机循环的总火用破坏度高于SGTC。

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