Permanent magnet starter-generator for aircraft application

Puvan Arumugam; Chris Gerada; Serhiy Bozhko; He Zhang; Weeramundage Fernando; Antonino La Rocca; Stephen Pickering

doi:10.4271/2014-01-2157

Permanent magnet starter-generator for aircraft application

Puvan Arumugam, Chris Gerada, Serhiy Bozhko, He Zhang, Weeramundage Fernando, Antonino La Rocca, Stephen Pickering

Nottingham Electrification Centre

Research output: Journal Publication › Conference article › peer-review

25 Citations (Scopus)

Abstract

This paper describes a high-speed electrical machine for an aircraft starter-generator. A surface mounted permanent magnet machine is designed to have minimal rotor losses and a novel cooling system for the stator. An inner stator sleeve is adopted to allow for a flooded stator whilst minimizing rotor windage losses. Different slot-pole combinations are compared in view of attaining an optimal combination that provides minimum losses whilst satisfying the electromagnetic, mechanical and thermal constraints.

Original language	English
Journal	SAE Technical Papers
Volume	2014-September
Issue number	September
DOIs	https://doi.org/10.4271/2014-01-2157
Publication status	Published - 16 Sept 2014
Event	SAE 2014 Aerospace Systems and Technology Conference, ASTC 2014 - Cincinnati, United States Duration: 23 Sept 2014 → 25 Sept 2014

ASJC Scopus subject areas

Automotive Engineering
Safety, Risk, Reliability and Quality
Pollution
Industrial and Manufacturing Engineering

Access to Document

10.4271/2014-01-2157

Cite this

@article{9bcf1e6398864ada8becc8bebabc2fd0,

title = "Permanent magnet starter-generator for aircraft application",

abstract = "This paper describes a high-speed electrical machine for an aircraft starter-generator. A surface mounted permanent magnet machine is designed to have minimal rotor losses and a novel cooling system for the stator. An inner stator sleeve is adopted to allow for a flooded stator whilst minimizing rotor windage losses. Different slot-pole combinations are compared in view of attaining an optimal combination that provides minimum losses whilst satisfying the electromagnetic, mechanical and thermal constraints.",

author = "Puvan Arumugam and Chris Gerada and Serhiy Bozhko and He Zhang and Weeramundage Fernando and {La Rocca}, Antonino and Stephen Pickering",

note = "Publisher Copyright: Copyright {\textcopyright} 2014 SAE International. {\textcopyright} 2014 SAE International.; SAE 2014 Aerospace Systems and Technology Conference, ASTC 2014 ; Conference date: 23-09-2014 Through 25-09-2014",

year = "2014",

month = sep,

day = "16",

doi = "10.4271/2014-01-2157",

language = "English",

volume = "2014-September",

journal = "SAE Technical Papers",

issn = "0148-7191",

publisher = "SAE International",

number = "September",

}

TY - JOUR

T1 - Permanent magnet starter-generator for aircraft application

AU - Arumugam, Puvan

AU - Gerada, Chris

AU - Bozhko, Serhiy

AU - Zhang, He

AU - Fernando, Weeramundage

AU - La Rocca, Antonino

AU - Pickering, Stephen

PY - 2014/9/16

Y1 - 2014/9/16

N2 - This paper describes a high-speed electrical machine for an aircraft starter-generator. A surface mounted permanent magnet machine is designed to have minimal rotor losses and a novel cooling system for the stator. An inner stator sleeve is adopted to allow for a flooded stator whilst minimizing rotor windage losses. Different slot-pole combinations are compared in view of attaining an optimal combination that provides minimum losses whilst satisfying the electromagnetic, mechanical and thermal constraints.

AB - This paper describes a high-speed electrical machine for an aircraft starter-generator. A surface mounted permanent magnet machine is designed to have minimal rotor losses and a novel cooling system for the stator. An inner stator sleeve is adopted to allow for a flooded stator whilst minimizing rotor windage losses. Different slot-pole combinations are compared in view of attaining an optimal combination that provides minimum losses whilst satisfying the electromagnetic, mechanical and thermal constraints.

UR - http://www.scopus.com/inward/record.url?scp=84937802848&partnerID=8YFLogxK

U2 - 10.4271/2014-01-2157

DO - 10.4271/2014-01-2157

M3 - Conference article

AN - SCOPUS:84937802848

SN - 0148-7191

VL - 2014-September

JO - SAE Technical Papers

JF - SAE Technical Papers

IS - September

T2 - SAE 2014 Aerospace Systems and Technology Conference, ASTC 2014

Y2 - 23 September 2014 through 25 September 2014

ER -

Permanent magnet starter-generator for aircraft application

Abstract

ASJC Scopus subject areas

Access to Document

Other files and links

Fingerprint

Cite this