Design and Implementation of On-board Hybrid Generator for Rotary Wing Drone

Muhammad Fathoni Nurrohaman, Benita Angela Titalim, Teddy Hadi Utama, W. Adiprawita
{"title":"Design and Implementation of On-board Hybrid Generator for Rotary Wing Drone","authors":"Muhammad Fathoni Nurrohaman, Benita Angela Titalim, Teddy Hadi Utama, W. Adiprawita","doi":"10.1109/ICEEI47359.2019.8988811","DOIUrl":null,"url":null,"abstract":"Drone which power up with Lithium Polymer (LiPo) battery doesn't have long duration flight time. The average enterprise-class rotary wing drone that weighs more than 10kg has a flight duration of less than 20 minutes. By developing an on-board generator system, it is expected that flight time of enterprise-class drone increase significantly. This development has many challenges such as the output of generator must have a large amount of power, the system needs a battery as fail-backup system so the charging system must be developed. The weight of developed system is one of consideration whether this system can be used as an on-board system or not. This paper discuss how the process of power generation that used by propeller done and how charging system work with Lithium Polymer.","PeriodicalId":236517,"journal":{"name":"2019 International Conference on Electrical Engineering and Informatics (ICEEI)","volume":"15 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2019-07-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"2","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"2019 International Conference on Electrical Engineering and Informatics (ICEEI)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/ICEEI47359.2019.8988811","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 2

Abstract

Drone which power up with Lithium Polymer (LiPo) battery doesn't have long duration flight time. The average enterprise-class rotary wing drone that weighs more than 10kg has a flight duration of less than 20 minutes. By developing an on-board generator system, it is expected that flight time of enterprise-class drone increase significantly. This development has many challenges such as the output of generator must have a large amount of power, the system needs a battery as fail-backup system so the charging system must be developed. The weight of developed system is one of consideration whether this system can be used as an on-board system or not. This paper discuss how the process of power generation that used by propeller done and how charging system work with Lithium Polymer.
旋翼无人机机载混合动力发电机的设计与实现
用锂聚合物(LiPo)电池供电的无人机飞行时间不长。重量超过10公斤的普通企业级旋翼无人机的飞行时间不到20分钟。通过开发机载发电机系统,预计企业级无人机的飞行时间将大幅增加。这种发展面临着许多挑战,如发电机的输出功率必须很大,系统需要电池作为故障备份系统,因此必须开发充电系统。所开发系统的重量是该系统能否作为车载系统使用的考虑因素之一。本文讨论了利用锂聚合物进行螺旋桨发电的过程及充电系统的工作原理。
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 求助全文
来源期刊
自引率
0.00%
发文量
0
×
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
确定
请完成安全验证×
copy
已复制链接
快去分享给好友吧!
我知道了
右上角分享
点击右上角分享
0
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 布克学术 All rights reserved.
京ICP备2023020795号-1
ghs 京公网安备 11010802042870号
Book学术文献互助
Book学术文献互助群
群 号:604180095
Book学术官方微信