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Weight reduction of amorphous alloy core electrical transformers for aircraft applications
- Source :
- 2016 International Conference on Electrical Systems for Aircraft, Railway, Ship Propulsion and Road Vehicles & International Transportation Electrification Conference (ESARS-ITEC).
- Publication Year :
- 2016
- Publisher :
- IEEE, 2016.
-
Abstract
- Catalogues of manufactured transformers show that amorphous alloy core transformers applied to 50 or 60 Hz lines have about 70% core electrical losses reduction when compared to same power output transformers made with Grain Oriented (GO) Silicon Iron (FeSi) core, however amorphous alloy core transformers are also heavier than FeSi core transformers. Such weight fact makes apparently prohibitive the use of amorphous alloy core transformers onboard aircrafts, but more electrical aircrafts (MEA) require much more electrical power, which means more FeSi core losses, therefore ways of electrical losses reduction onboard must be studied. This paper shows by calculations that transformers with amorphous alloy core can be less heavy and have reduced losses than an equal calculated power output transformer with GO FeSi core if core temperature, safety limits for core induction value and cooper wire cross section area reduction are considered.
- Subjects :
- 010302 applied physics
Imagination
Engineering
Amorphous metal
Chemical substance
business.industry
media_common.quotation_subject
Electrical engineering
02 engineering and technology
021001 nanoscience & nanotechnology
01 natural sciences
law.invention
Magnetic core
Electromagnetic coil
law
0103 physical sciences
Electric power
Composite material
0210 nano-technology
business
Science, technology and society
Transformer
media_common
Subjects
Details
- Database :
- OpenAIRE
- Journal :
- 2016 International Conference on Electrical Systems for Aircraft, Railway, Ship Propulsion and Road Vehicles & International Transportation Electrification Conference (ESARS-ITEC)
- Accession number :
- edsair.doi...........c0e6a35a85456dc3307aba5890dbc4dc
- Full Text :
- https://doi.org/10.1109/esars-itec.2016.7841347