Conceptual design of battery energy storage for aircraft hybrid propulsion system

Rashed, Mohamed; Le Peuvedic, Jean-Marc; Bozhko, Serhiy

Abstract

The paper presents a conceptual design approach for Energy Storage (ES) devices in advanced hybrid propulsion system for small aircrafts. The study targets operational improvement and reduction of fuel consumption for different flight missions. Power sharing strategies for ES and the engine are proposed for cruise flight phase aiming to maximise the range and/or endurance for the available amount of fuel in the tank. The ES size is designed against the engine performance and the proposed power sharing strategy by optimizing the flight altitude.

Citation

Rashed, M., Le Peuvedic, J., & Bozhko, S. (2016). Conceptual design of battery energy storage for aircraft hybrid propulsion system.

• Conference Name: International Conference on Electrical Systems for Aircraft, Railway, Ship Propulsion and Road Vehicles & International Transportation Electrification Conference (ESARS-ITEC)
• End Date: Nov 4, 2016
• Acceptance Date: Sep 10, 2016
• Online Publication Date: Feb 9, 2017
• Publication Date: Nov 2, 2016
• Deposit Date: Jun 28, 2017
• Publicly Available Date: Jun 28, 2017
• Peer Reviewed: Peer Reviewed
• Keywords: hybrid propulsion; battery energy storage; fuel burn saving
• Public URL: https://nottingham-repository.worktribe.com/output/830390
• Publisher URL: http://ieeexplore.ieee.org/document/7841396/