Conceptual design of battery energy storage for aircraft hybrid propulsion system

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 prop...

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Main Authors: Rashed, Mohamed, Le Peuvedic, Jean-Marc, Bozhko, Serhiy
Format: Conference or Workshop Item
Published: 2016
Subjects:
Online Access:https://eprints.nottingham.ac.uk/43792/
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author Rashed, Mohamed
Le Peuvedic, Jean-Marc
Bozhko, Serhiy
author_facet Rashed, Mohamed
Le Peuvedic, Jean-Marc
Bozhko, Serhiy
author_sort Rashed, Mohamed
building Nottingham Research Data Repository
collection Online Access
description 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.
first_indexed 2025-11-14T19:53:15Z
format Conference or Workshop Item
id nottingham-43792
institution University of Nottingham Malaysia Campus
institution_category Local University
last_indexed 2025-11-14T19:53:15Z
publishDate 2016
recordtype eprints
repository_type Digital Repository
spelling nottingham-437922020-05-04T18:22:40Z https://eprints.nottingham.ac.uk/43792/ Conceptual design of battery energy storage for aircraft hybrid propulsion system Rashed, Mohamed Le Peuvedic, Jean-Marc Bozhko, Serhiy 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. 2016-11-02 Conference or Workshop Item PeerReviewed Rashed, Mohamed, Le Peuvedic, Jean-Marc and Bozhko, Serhiy (2016) Conceptual design of battery energy storage for aircraft hybrid propulsion system. In: International Conference on Electrical Systems for Aircraft, Railway, Ship Propulsion and Road Vehicles & International Transportation Electrification Conference (ESARS-ITEC), 2-4 Nov 2016, Toulouse, France. hybrid propulsion; battery energy storage; fuel burn saving http://ieeexplore.ieee.org/document/7841396/
spellingShingle hybrid propulsion; battery energy storage; fuel burn saving
Rashed, Mohamed
Le Peuvedic, Jean-Marc
Bozhko, Serhiy
Conceptual design of battery energy storage for aircraft hybrid propulsion system
title Conceptual design of battery energy storage for aircraft hybrid propulsion system
title_full Conceptual design of battery energy storage for aircraft hybrid propulsion system
title_fullStr Conceptual design of battery energy storage for aircraft hybrid propulsion system
title_full_unstemmed Conceptual design of battery energy storage for aircraft hybrid propulsion system
title_short Conceptual design of battery energy storage for aircraft hybrid propulsion system
title_sort conceptual design of battery energy storage for aircraft hybrid propulsion system
topic hybrid propulsion; battery energy storage; fuel burn saving
url https://eprints.nottingham.ac.uk/43792/
https://eprints.nottingham.ac.uk/43792/