A fault-tolerant electric motor for more electric aircraft by Lim, Sebastin Choon Huat

“…The growing momentum in the aircraft industry toward the idea of a hybrid electric-powered or more electric aircraft (MEA), and eventually an all-electric aircraft, exemplifies the industry's efforts to improve aircraft performance, lower operating and maintenance costs, boost dispatch reliability, and lower gas emissions. …”
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Predictive energy management for hybrid electric aircraft propulsion systems by Doff-Sotta, M, Cannon, M, Bacic, M

Large-Scale Piezoelectric-Based Systems for More Electric Aircraft Applications by Tran Vy Khanh Vo, Tomasz Marek Lubecki, Wai Tuck Chow, Amit Gupta, King Ho Holden Li

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Aeroelastic Stability Analysis of Electric Aircraft Wings with Distributed Electric Propulsors by Mohammadreza Amoozgar, Michael I. Friswell, Seyed Ahmad Fazelzadeh, Hamed Haddad Khodaparast, Abbas Mazidi, Jonathan E. Cooper

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Review on Design of Electric Environment Control System for More Electric Aircraft by YANG Jianzhong, OUYANG Jingpeng, CHEN Xiyuan, MENG Fanxin, WANG Lei, LIU Luxuan

Subjects: “…more electric aircraft…”
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Active Load-Sensitive Electro-Hydrostatic Actuator for More Electric Aircraft by Ligang Huang, Tian Yu, Zongxia Jiao, Yanpeng Li

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An improved 24‐pulse rectifier for harmonic mitigation in more electric aircraft by R. Abdollahi, G. B. Gharehpetian, A. Anvari‐Moghaddam, F. Blaabjerg

“…Also, it is shown that in comparison with other solutions, the proposed two configurations are cost‐effective, power factor is near unity, rating is almost 29% of the load rating, and the efficiency is almost 97.5%, which makes them a practical solution for more electric aircraft.…”
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Research on Fault-Tolerant Control of Combined Airframe Damage of Electric Aircraft by Lei Zhang, Jin Mu, Hongtu Ma, Guicheng Dai, Shengxi Tong

Subjects: “…electric aircraft…”
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Reliability analysis of multilevel and matrix converters used in more electric aircraft by Aanchal Verma, Aditya Singh, Kyadsandra Anand Kumar, Ram Khelawan Saket, Baseem Khan

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Design and integration of the battery energy storage system in more electric aircraft by Tariq, Mohd

“…A general background of the battery system is studied and the performance of the batteries based on energy densities and low temperature capabilities is evaluated for the deployment in the more electric aircraft (MEA). Evolution of MEA with its power system architecture and load profile is analysed to understand the requirements of the battery system. …”
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Graph-based modeling of hybrid-electric aircraft electro-thermal system by Choong, Hui Qian

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A high-performance electric motor drive for electric aircraft application by Zhang, Yuhui

“…This dissertation provides a comprehensive investigation into different motor types, focusing on the applicability of the FSPM motor in electric aircraft. Through meticulous research, six enhanced FSPM (Flux-Switching Permanent Magnet) motor topologies were developed. …”
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Voltage Transients Mitigation in the DC Distribution Network of More/All Electric Aircrafts by Nick Rigogiannis, Dionisis Voglitsis, Tiago Jappe, Nick Papanikolaou

Subjects: “…All Electric Aircraft…”
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A H‐type architecture for electric/hybrid‐electric aircraft propulsion systems by Anil Kumar Reddy Siddavatam, Kaushik Rajashekara, Ravi Prakash Reddy, Hao Huang, Harish S. Krishnamoorthy, Fred Wang

“…Abstract In this paper, an H‐type electric/hybrid electric aircraft propulsion architecture is proposed to address the issues associated with the radial electric propulsion architecture. …”
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Load Identification for the More Electric Aircraft Distribution System Based on Intelligent Algorithm by Juan Yang, Xingwang Bao, Zhangang Yang

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Robust performance comparison of PMSM for flight control applications in more electric aircraft. by Djaloul Karboua, Toual Belgacem, Zeashan Hameed Khan, Cherif Kellal

“…This paper describes a robust performance comparison of flight control actuation controllers based on a permanent magnet synchronous motor (PMSM) in more electric aircraft (MEA). Recently, the PMSM has become a favorite for the flight control applications of more electric aircraft (MEA) due to their improved efficiency, higher torque, less noise, and higher reliability as compared to their counterparts. …”
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A Novel Single-Turn Permanent Magnet Synchronous Machine for Electric Aircraft by Zeyu Cheng, Zhi Cao, John T. Hwang, Chris Mi

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Design Space Analysis of the Dual-Active-Bridge Converter for More Electric Aircraft by Alejandro Fernandez-Hernandez, Fernando Gonzalez-Hernando, Asier Garcia-Bediaga, Irma Villar, Gonzalo Abad

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Multidisciplinary Design Optimization of the Actuation System of a Hybrid Electric Aircraft Powertrain by Matthieu Pettes-Duler, Xavier Roboam, Bruno Sareni, Yvan Lefevre, Jean-François Llibre, Matthieu Fénot

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Multi-modal safety analysis of the more electric aircraft starter generator system by Z Zeng, Y Hu, Y Xiong, Q Gong, X Xu, H Ge

“…This paper analyses the architecture, operating process and modals of more electric aircraft starter generator system and decomposes the system into eight operating modals. …”
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