Opportunities and challenges for electric propulsion of airliners

IF 0.5 Q4 ENGINEERING, AEROSPACE International Journal of Sustainable Aviation Pub Date : 2020-01-01 DOI:10.1504/ijsa.2020.10034603
D. Lentini, H. Tacca
{"title":"Opportunities and challenges for electric propulsion of airliners","authors":"D. Lentini, H. Tacca","doi":"10.1504/ijsa.2020.10034603","DOIUrl":null,"url":null,"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.","PeriodicalId":42251,"journal":{"name":"International Journal of Sustainable Aviation","volume":"1 1","pages":""},"PeriodicalIF":0.5000,"publicationDate":"2020-01-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"International Journal of Sustainable Aviation","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1504/ijsa.2020.10034603","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q4","JCRName":"ENGINEERING, AEROSPACE","Score":null,"Total":0}
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.
查看原文
分享 分享
微信好友 朋友圈 QQ好友 复制链接
本刊更多论文
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。
求助全文
约1分钟内获得全文 去求助
来源期刊
CiteScore
0.20
自引率
0.00%
发文量
34
期刊最新文献
Effects of battery degradation on a hybrid electric propulsive system management Performance analysis of more electric aircraft starter/generator by different electric loads Performing trajectory tracking control of an unmanned ground vehicle using fractional order terminal sliding mode controller Design and analysis of a two-tier stretcher frame Two-phase heat transfer devices for passive cooling of electric and hybrid aircraft onboard equipment
×
引用
GB/T 7714-2015
复制
MLA
复制
APA
复制
导出至
BibTeX EndNote RefMan NoteFirst NoteExpress
×
×
提示
您的信息不完整,为了账户安全,请先补充。
现在去补充
×
提示
您因"违规操作"
具体请查看互助需知
我知道了
×
提示
现在去查看 取消
×
提示
确定
0
微信
客服QQ
Book学术公众号 扫码关注我们
反馈
×
意见反馈
请填写您的意见或建议
请填写您的手机或邮箱
已复制链接
已复制链接
快去分享给好友吧!
我知道了
×
扫码分享
扫码分享
Book学术官方微信
Book学术文献互助
Book学术文献互助群
群 号:481959085
Book学术
文献互助 智能选刊 最新文献 互助须知 联系我们:info@booksci.cn
Book学术提供免费学术资源搜索服务,方便国内外学者检索中英文文献。致力于提供最便捷和优质的服务体验。
Copyright © 2023 Book学术 All rights reserved.
ghs 京公网安备 11010802042870号 京ICP备2023020795号-1