All Outputs (4)

A Framework for Optimization of Hybrid Aircraft (2019)
Conference Proceeding
Zhao, X., Sahoo, S., Kyprianidis, K., Sumsurooah, S., Valente, G., Rashed, M., …Ekstedt, E. (2019). A Framework for Optimization of Hybrid Aircraft. In Proceedings of the ASME Turbo Expo : Turbomachinery Technical Conference and Exposition--2019-- : presented at The ASME Turbo Expo 2019 : Turbiomachinery Technical Conference and Exposition, June 17-21, 2019, Phoenix, Arizona, USA. Book 3. https://doi.org/10.1115/GT2019-91335

To achieve the goals of substantial improvements in efficiency and emissions set by Flightpath 2050, fundamentally different concepts are required. As one of the most promising solutions, electrification of the aircraft primary propulsion is currentl... Read More about A Framework for Optimization of Hybrid Aircraft.

Design of more electric aircraft dc power distribution architectures considering reliability performance (2019)
Conference Proceeding
Recalde, A. A., Bozhko, S., Atkin, J., & Hill, C. (2019). Design of more electric aircraft dc power distribution architectures considering reliability performance. https://doi.org/10.2514/6.2019-4506

© 2019 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved. The More Electric Aircraft (MEA) concept has started to define the future of aircraft electrification. The electrical system will certainly play a crucial rol... Read More about Design of more electric aircraft dc power distribution architectures considering reliability performance.

Implementation of an Advanced Modelica Library for Evaluation of Inverter Loss Modeling (2019)
Conference Proceeding
Lai, S. C., Ian Hill, C., & Suchato, N. (2019). Implementation of an Advanced Modelica Library for Evaluation of Inverter Loss Modeling. In Proceedings of 2019 IEEE Texas Power and Energy Conference (TPEC) (1-6). https://doi.org/10.1109/TPEC.2019.8662144

This paper introduces a newly developed Power Electronic Inverter library in Modelica. The library has different levels of complexity to approximate the power losses in the power inverter. In addition, it provides two different modelling domains (ABC... Read More about Implementation of an Advanced Modelica Library for Evaluation of Inverter Loss Modeling.

Finite state machine control for aircraft electrical distribution system (2019)
Journal Article
Spagnolo, C., Sumsurooah, S., Hill, C. I., & Bozhko, S. (2019). Finite state machine control for aircraft electrical distribution system. Journal of Engineering, 2018(13), 506-511. https://doi.org/10.1049/joe.2018.0039

This study deals with the development of new control logic for more electric aircraft (MEA) electrical power systems (EPSs). A key aspect of the MEA concept is that traditional pneumatic and hydraulic loads are replaced by electrical equivalents. The... Read More about Finite state machine control for aircraft electrical distribution system.