Functional modelling of symmetrical multi-pulse auto- transformer rectifier units for aerospace applications

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Yang, Tao, Bozhko, Serhiy and Asher, Greg (2015) Functional modelling of symmetrical multi-pulse auto- transformer rectifier units for aerospace applications. IEEE Transactions on Power Electronics, 30 (9). pp. 4704-4713. ISSN 0885-8993

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Abstract

This paper aims to develop a functional model of symmetrical multi-pulse Auto-Transformer Rectifier Units (ATRUs) for More-Electric Aircraft (MEA) applications. The ATRU is seen as the most reliable way readily to be applied in the MEA. Interestingly, there is no model of ATRUs suitable for unbalanced or faulty conditions at the moment. This paper is aimed to fill this gap and develop functional models suitable for both balanced and unbalanced conditions. Using the fact that the DC voltage and current are strongly related to the voltage and current vectors at the AC terminals of ATRUs, a functional model has been developed for the asymmetric ATRUs. The developed functional models are validated through simulation and experiment. The efficiency of the developed model is also demonstrated by comparing with corresponding detailed switching models. The developed functional model shows significant improvement of simulation efficiency, especially under balanced conditions.

Item Type: Article
RIS ID: https://nottingham-repository.worktribe.com/output/982605
Additional Information: The authors gratefully acknowledge the EU FP7 funding via the Clean Sky JTI – Systems for green Operations ITD. The authors also would like to thank Thales for providing the 18-pulse ATRU that was used in our experiment. © 2015 IEEE. Personal use of this material is permitted. Permission from IEEE must be obtained for all other uses, in any current or future media, including reprinting/republishing this material for advertising or promotional purposes, creating new collective works, for resale or redistribution to servers or lists, or reuse of any copyrighted component of this work in other works.
Keywords: Functional modelling, Fault conditions, Multi-pulse rectifier, More-electric aircraft, Transformer rectifier unit
Schools/Departments: University of Nottingham, UK > Faculty of Engineering > Department of Electrical and Electronic Engineering
Identification Number: https://doi.org/10.1109/TPEL.2014.2364682
Depositing User: Burns, Rebecca
Date Deposited: 09 Mar 2016 14:17
Last Modified: 04 May 2020 20:07
URI: https://eprints.nottingham.ac.uk/id/eprint/32164

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