Electric power transfer concept for improved performance of multi-spool turbofan jet engine

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Electric power transfer concept for improved performance of multi-spool turbofan jet engine

Twin spool high-bypass turbofan engines are the dominant sources of propulsion for most civil aircraft. The shaft speeds in these engines are thermodynamically coupled even with no mechanical link between them. This coupling effect results in inevitable limitations on the engine design and performan...

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Bibliographic Details
Main Author:	Balaghi Enalou, Hossein
Format:	Thesis (University of Nottingham only)
Language:	English
Published:	2020
Subjects:	Airplanes Turbofan engines; Electric Power Transfer; engine shafts
Online Access:	https://eprints.nottingham.ac.uk/59843/

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