Nonlinear aircraft engine model for future integrated power center development

Enalou, H.B. and Rashed, Mohamed and Kulsangcharoen, Ponggorn and 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.

[img]
Preview
PDF - Requires a PDF viewer such as GSview, Xpdf or Adobe Acrobat Reader
Download (441kB) | Preview

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)
Keywords: Turbofan, Modeling, power off-take
Schools/Departments: University of Nottingham, UK > Faculty of Engineering > Department of Electrical and Electronic Engineering
Related URLs:
URLURL Type
http://www.esars-itec.org/Organisation
Depositing User: Burns, Rebecca
Date Deposited: 18 Nov 2016 10:29
Last Modified: 19 Nov 2016 01:36
URI: http://eprints.nottingham.ac.uk/id/eprint/38777

Actions (Archive Staff Only)

Edit View Edit View