Electric power transfer concept for improved performance of multi-spool turbofan jet engineTools Balaghi Enalou, Hossein (2020) Electric power transfer concept for improved performance of multi-spool turbofan jet engine. PhD thesis, University of Nottingham.
AbstractTwin 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 performance, including mismatches in the performance of the compressors at low-speed conditions, that push for undesirable air bleeding requirements. Therefore, decoupling the shaft speeds can introduce remarkable improvements to engine performance, which leads to better fuel efficiency and hence reduced emissions.
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