Opportunities and challenges for electric propulsion of airliners

IF 0.5 Q4 ENGINEERING, AEROSPACE
D. Lentini, H. Tacca
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引用次数: 0

Abstract

The growth of air traffic implies an increase of emissions (greenhouse and ozone depleting gases) from the global air fleet. Innovative solutions are therefore urgently required. Among them, electric aviation is the object of much current interest. The present paper discusses the accompanying opportunities as well as challenges, with a focus on costs and operability. In order to take full advantage of electric propulsion, dedicated airframes are indicated, featuring boundary layer ingestion, distributed propulsion and other elements. Different options for electric propulsion are reviewed, and their pros and cons highlighted. In particular, all electric aircrafts suffer from severe range limitations, turbo electric aircrafts become appealing only if fed with liquid hydrogen (with the accompanying problems), while hybrid-electric aircrafts can lead to a somewhat reduced wing area (then weight). Other economical and operational issues are also considered, including cost per kWh (however shown to be a misleading indicator) and that per unit payload mass, maintenance, sources of electric energy for recharge.
飞机电力推进的机遇与挑战
空中交通的增长意味着全球飞机的排放量(温室气体和消耗臭氧气体)的增加。因此,迫切需要创新的解决办法。其中,电动航空是当前备受关注的对象。本文讨论了随之而来的机遇和挑战,重点是成本和可操作性。为了充分发挥电力推进的优势,设计了专用机身,具有边界层吸入、分布式推进等特点。对电力推进的不同选择进行了回顾,并强调了它们的优缺点。特别是,所有的电动飞机都有严重的航程限制,涡轮电动飞机只有在使用液氢的情况下才有吸引力(伴随的问题),而混合动力飞机可能会导致机翼面积(然后是重量)有所减少。还考虑了其他经济和操作问题,包括每千瓦时的费用(但这是一个误导性的指标)和每单位有效载荷质量、维修、充电的电能来源。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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CiteScore
0.20
自引率
0.00%
发文量
34
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