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An exergy way to quantify sustainability metrics for a high bypass turbofan engine

机译:一种量化高旁路涡扇发动机可持续性指标的火用方法

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As fuel efficiency becomes a greater concern in aero engine design and operation. To meet this need, a new methodology is being developed here that proposes the use of exergetic metrics for mapping the exergy flows throughout high bypass turbofan engine at maximum thrust level for its sustainability assessment. The engine (net thrust force of 206 kN) studied here is used in the first wide body, dual-aisle, and the largest commercial aircraft. The findings of sustainability analysis reveal that exergy efficiency of the engine is 29.6% having exergy destruction factor of 0.5037. In addition, environmental effect factor of the turbofan engine is found to be 0.675, while exergetic sustainability index is calculated to be 1.48. In the case study, recoverable exergy amount of the engine is zero since the emissions released from exhaust cannot be recoverable in the engine. As a conclusion, exergetic sustainability method is an effective way to assess the sustainability of aircraft and aero engines and provides a good tool for designers, users, decision makers and researchers in green air transportation. Hence, these parameters make the engine and aircraft more environmentally benign and more sustainable. (C) 2015 Elsevier Ltd. All rights reserved.
机译:随着燃油效率成为航空发动机设计和运行中的更大关注点。为了满足这一需求,这里正在开发一种新的方法,该方法建议使用能效度量标准来绘制高推力涡扇发动机在最大推力水平时整个火用能流的映射图,以进行可持续性评估。这里研究的发动机(净推力为206 kN)用于第一架宽体,双通道和最大的商用飞机。可持续性分析的结果表明,发动机的火用效率为29.6%,火用破坏因子为0.5037。另外,涡轮风扇发动机的环境影响因子被发现为0.675,而高能持续性指数被计算为1.48。在案例研究中,发动机的可回收火用量为零,因为从排气中释放的排放物无法在发动机中回收。结论是,高能持续性方法是评估飞机和航空发动机可持续性的有效方法,并且为绿色航空运输中的设计人员,用户,决策者和研究人员提供了良好的工具。因此,这些参数使发动机和飞机对环境更无害且更具可持续性。 (C)2015 Elsevier Ltd.保留所有权利。

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