Design of a Rotary Engine Based High-Power Density Hybrid-Electric Power Generation Testbed

Roydon Fernandes, Jayaprakash Shivakumar, Mariana Gehrmann, N. Miller, Kule Collins, P. Currier, R. Anderson
{"title":"Design of a Rotary Engine Based High-Power Density Hybrid-Electric Power Generation Testbed","authors":"Roydon Fernandes, Jayaprakash Shivakumar, Mariana Gehrmann, N. Miller, Kule Collins, P. Currier, R. Anderson","doi":"10.4050/f-0078-2022-17532","DOIUrl":null,"url":null,"abstract":"\n This paper details the design and components of a high-power density Hybrid-Electric Power generation testbed that is being built by the Eagle Flight Research Center at Embry-Riddle Aeronautical University, Florida. The system consists of a twin-rotor rotary Wankel engine, a radial flux Permanent Magnet Synchronous Machine used as the generator along with its inverter/controller, a 400 V Lead-acid battery pack, a vehicle control unit, and the associated thermal systems. The system weighs 324 lbs. (147 kg) before fuel and is estimated to achieve peak power of 134 hp (100 kW) with the High-Voltage battery and sustained power of 70 hp (52 kW) with just the hybrid-electric system. With 8 gallons of fuel, the system is estimated to realize a specific energy of 0.37 hp-h/lb. (0.61 kWh/kg), and a specific power of 0.46 hp/lb. (0.76 kW/kg). The system control was implemented on the Vehicle Control Unit using a feedforward-feedback control loop with user-defined speed and output power values.\n","PeriodicalId":223727,"journal":{"name":"Proceedings of the Vertical Flight Society 78th Annual Forum","volume":"66 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2022-05-10","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"Proceedings of the Vertical Flight Society 78th Annual Forum","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.4050/f-0078-2022-17532","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 0

Abstract

This paper details the design and components of a high-power density Hybrid-Electric Power generation testbed that is being built by the Eagle Flight Research Center at Embry-Riddle Aeronautical University, Florida. The system consists of a twin-rotor rotary Wankel engine, a radial flux Permanent Magnet Synchronous Machine used as the generator along with its inverter/controller, a 400 V Lead-acid battery pack, a vehicle control unit, and the associated thermal systems. The system weighs 324 lbs. (147 kg) before fuel and is estimated to achieve peak power of 134 hp (100 kW) with the High-Voltage battery and sustained power of 70 hp (52 kW) with just the hybrid-electric system. With 8 gallons of fuel, the system is estimated to realize a specific energy of 0.37 hp-h/lb. (0.61 kWh/kg), and a specific power of 0.46 hp/lb. (0.76 kW/kg). The system control was implemented on the Vehicle Control Unit using a feedforward-feedback control loop with user-defined speed and output power values.
基于旋转发动机的大功率密度混合动力发电试验台设计
本文详细介绍了佛罗里达州Embry-Riddle航空大学Eagle飞行研究中心正在建造的高功率密度混合动力发电试验台的设计和组件。该系统由一个双转子旋转万克尔发动机、一个用作发电机的径向磁通永磁同步机及其逆变器/控制器、一个400 V铅酸电池组、一个车辆控制单元和相关的热系统组成。该系统重324磅。(147公斤),不含燃料,估计使用高压电池可达到134马力(100千瓦)的峰值功率,使用混合动力系统可达到70马力(52千瓦)的持续功率。在8加仑燃料的情况下,该系统的比能量估计为0.37 hp-h/lb。(0.61 kWh/kg),比功率为0.46 hp/lb。(0.76千瓦/公斤)。系统控制在车辆控制单元上实现,使用具有用户定义的速度和输出功率值的前馈-反馈控制回路。
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
小红书