Nonlinear aircraft engine model for future integrated power center development

Enalou, H.B.; Rashed, Mohamed; Kulsangcharoen, Ponggorn; Hill, Christopher Ian; Bozhko, Serhiy

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.

Citation

Enalou, H., Rashed, M., Kulsangcharoen, P., Hill, C. I., & Bozhko, S. (in press). Nonlinear aircraft engine model for future integrated power center development.

• Conference Name: ESARS Itec 2016
• End Date: Nov 4, 2016
• Acceptance Date: Sep 9, 2016
• Deposit Date: Nov 18, 2016
• Peer Reviewed: Peer Reviewed
• Keywords: Turbofan, Modeling, power off-take
• Public URL: https://nottingham-repository.worktribe.com/output/818450
• Related Public URLs: http://www.esars-itec.org/