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Exergy-based sustainability analysis of a low-bypass turbofan engine: A case study for JT8D

机译:基于电气的低通基础涡扇发动机的可持续性分析:JT8D的案例研究

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The growth in demand for air transport is a problem for the global and local environment. There are, moreover, fundamental conflicts with sustainable development objectives. Sustainability demands a sustainable supply of energy without causing negative environmental impacts of aircrafts and its engines. In this paper, an investigation of exergo-sustainability indicators is reported for a low bypass (0.96 to 1) turbofan engine with 72 kN thrust force. Six selected exergetic indicators are selected for the analysis. The study is based on three approaches: energy, exergy and sustainability. In this regard, considering thermodynamics laws and Brayton cycle equations, the exergy efficiency of the engine is 11 % having waste exergy ratio of 0.348. In addition, exergetic sustainability index of the low bypass turbofan engine is found to be 0.316, while environmental effect factor is calculated to be 3.163. On the other hand, the recoverable exergy amount of the engine is zero since the emissions released from fan bypass duct and core engine exhaust cannot be recoverable in the engine.
机译:空运需求的增长是全球和当地环境的问题。此外,与可持续发展目标有根本的冲突。可持续性要求提供可持续的能源供应,而不会导致飞机及其发动机的负面环境影响。本文据报道,对具有72 kN推力力的低旁路(0.96至1)涡轮机发动机进行了exergo可持续性指标的调查。选择六种选定的exergetic指标进行分析。该研究基于三种方法:能源,走势和可持续性。在这方面,考虑到热力学法律和布雷顿周期方程,发动机的高度效率为11%,浪费余量为0.348。此外,低旁路涡扇发动机的防辐射可持续性指数为0.316,而环境效果因子计算为3.163。另一方面,由于风扇旁路管道和芯发动机排气释放的排放不能在发动机中可以恢复,所可收回的发动机的恢复量为零。

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