Development of Aircraft Electric Starter-Generator System Based on Active Rectification Technology

被引：75

作者：

Bozhko, Serhiy ^{[1
]}

Yang, Tao ^{[1
]}

Le Peuvedic, Jean-Marc ^{[2
]}

Arumugam, Puvan ^{[3
,4
]}

Degano, Marco ^{[5
]}

La Rocca, Antonino ^{[6
]}

Xu, Zeyuan ^{[6
]}

Rashed, Mohamed ^{[1
]}

Fernando, Weeramundage ^{[1
,7
]}

Hill, Christopher Ian ^{[1
]}

Eastwick, Carol ^{[6
]}

Pickering, Stephen ^{[6
]}

Gerada, Chris ^{[1
]}

Wheeler, Patrick ^{[1
]}

机构：

[1] Univ Nottingham, Dept Elect & Elect Engn, Nottingham NG7 2RD, England

[2] Dassault Aviat, F-92210 Paris, France

[3] Univ Nottingham, Nottingham NG7 2RD, England

[4] Romax UK, Stockton On Tees TS18 2NH, England

[5] McLaren Appl Technol, Woking GU21 4YH, Surrey, England

[6] Univ Nottingham, Dept Mech Mat & Mfg Engn, Nottingham NG7 2RD, England

[7] RMIT Univ, Melbourne, Vic 3000, Australia

来源：

IEEE TRANSACTIONS ON TRANSPORTATION ELECTRIFICATION | 2018年 / 4卷 / 04期

基金：

欧盟地平线“2020”;

关键词：

Active front end; electric machine; more-electric aircraft (MEA); starter/generator (S/G); thermal management; PERMANENT-MAGNET MACHINES;

D O I：

10.1109/TTE.2018.2863031

中图分类号：

TM [电工技术]; TN [电子技术、通信技术];

学科分类号：

0808 ; 0809 ;

摘要：

More-electric aircraft (MEA) has become a dominant trend for modern aircraft. On-board MEA, many functions, which are conventionally driven by pneumatic and hydraulic power, are replaced with electrical subsystems. Starting aircraft engines with an electric motor instead of using pneumatic power from the auxiliary power unit is one of the major characteristics of future aircraft. This paper presents the development of a novel electric starter-generator system for aircraft applications. This paper describes the main achievements of the AEGART (EU CleanSky Project) project in the key areas, including electric machines, power electronic converters, thermal management, and overall system control design. The developed prototype has been tested successfully, and the test results are presented in this paper.

引用

页码：985 / 996

页数：12

共 18 条

[1] [Anonymous], P S DES PRINC METH A
[2] [Anonymous], TECH REP
[3] [Anonymous], 2014, 2014 16 EUR C POW EL
[4] [Anonymous], 2014012139 SAE
[5] [Anonymous], 2016, THESIS
[6] [Anonymous], 2013, 2013 48 INT U POW EN
[7] High-Speed Solid Rotor Permanent Magnet Machines: Concept and Design
Arumugam, Puvan
Xu, Zeyuan
La Rocca, Antonino
Vakil, Gaurang
Dickinson, Matthew
Amankwah, Emmanuel
Hamiti, Tahar
Bozhko, Serhiy
Gerada, Chris
Pickering, Stephen J.
[J]. IEEE TRANSACTIONS ON TRANSPORTATION ELECTRIFICATION, 2016, 2 (03): : 391 - 400
[8] Arumugam P, 2015, IEEE IND ELEC, P1741, DOI 10.1109/IECON.2015.7392353
[9] Design and Initial Testing of a High-Speed 45-kW Switched Reluctance Drive for Aerospace Application
Bartolo, James Borg
Degano, Marco
Espina, Jordi
Gerada, Chris
[J]. IEEE TRANSACTIONS ON INDUSTRIAL ELECTRONICS, 2017, 64 (02) : 988 - 997
[10] Global Energy Scenario and Impact of Power Electronics in 21st Century
Bose, Bimal K.
[J]. IEEE TRANSACTIONS ON INDUSTRIAL ELECTRONICS, 2013, 60 (07) : 2638 - 2651

← 1 2 →