Nonlinear aircraft engine model for future integrated power center development

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Enalou, H.B., Rashed, Mohamed, Kulsangcharoen, Ponggorn, Hill, Christopher Ian and Bozhko, Serhiy (2016) Nonlinear aircraft engine model for future integrated power center development. In: ESARS Itec 2016, 2-4 Nov 2016, Toulouse, France.

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Abstract

Aircraft engines, the prime source of on-board power, play a vital role within the electrical power generation system. In literature these are considerably simplified to rudimentary engine speed. In this paper, a nonlinear zero-dimension (0-D) order turbofan engine model has been developed for use with an integrated power center. By analyzing the compressor maps in detail, the results reveal a limit on the amount power off-take from each engine shaft at different altitudes.

Item Type: Conference or Workshop Item (Paper)
RIS ID: https://nottingham-repository.worktribe.com/output/818450
Keywords: Turbofan, Modeling, power off-take
Schools/Departments: University of Nottingham, UK > Faculty of Engineering > Department of Electrical and Electronic Engineering
Related URLs:
URL
URL Type
http://www.esars-itec.org/
Organisation
Depositing User: Burns, Rebecca
Date Deposited: 18 Nov 2016 10:29
Last Modified: 04 May 2020 18:12
URI: https://eprints.nottingham.ac.uk/id/eprint/38777

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