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Functional Modeling of 18-Pulse Autotransformer Rectifier Units for Aircraft Applications University of Nottingham

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
Yang, Yang, author.
Contributor:
Asher, Greg
Bozhko, Serhiy
Conference Name:
SAE 2015 AeroTech Congress & Exhibition (2015-09-22 : Seattle, Washington, United States)
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 2015
Summary:
This paper aims to develop a general functional model of 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 generic functional model has been developed for both symmetric and 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
Notes:
Vendor supplied data
Publisher Number:
2015-01-2412
Access Restriction:
Restricted for use by site license

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