Design Algorithm of an Aircraft Power Generation System

The paper deals with the design and testing of a power generation system for the future and existing aircrafts. A new design algorithm of the power generation components is presented. The proposed design algorithm was tested on a prototype: a full-size starter-generator and transformer-rectifier uni...

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Veröffentlicht in:IEEE transactions on aerospace and electronic systems 2019-12, Vol.55 (6), p.2899-2910
Hauptverfasser: Ismagilov, Flur Rashitovich, Kiselev, Mikhail Anatolyevich, Vavilov, Viacheslav Evgenievich, Gusakov, Denis Valerievich
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container_issue 6
container_start_page 2899
container_title IEEE transactions on aerospace and electronic systems
container_volume 55
creator Ismagilov, Flur Rashitovich
Kiselev, Mikhail Anatolyevich
Vavilov, Viacheslav Evgenievich
Gusakov, Denis Valerievich
description The paper deals with the design and testing of a power generation system for the future and existing aircrafts. A new design algorithm of the power generation components is presented. The proposed design algorithm was tested on a prototype: a full-size starter-generator and transformer-rectifier unit prototype was created with a transformer magnetic core made up of an amorphous magnetic material. Its stand tests were carried out both for each element and for the entire system. The proposed algorithm can be used to create power supply systems for aircraft with different voltage levels, including 270 Vdc and 200 Vac. The developed power generation system turned out to be 25-40% better than serial solutions by mass and efficiency.
doi_str_mv 10.1109/TAES.2019.2894893
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subjects Aerospace electronics
Aircraft
Aircraft design
Aircraft power supplies
Algorithms
Amorphous materials
Design algorithm
Electric power generation
Flight tests
Magnetic cores
Magnetic materials
Optimization
permanent magnet (PM) machines
Power generation
Prototypes
pulse transformers
Rectifiers
Transformers
Windings
title Design Algorithm of an Aircraft Power Generation System
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