Studies Concerning Electrical Repowering of a Training Airplane Using Hydrogen Fuel Cells

Author:

Corcau Jenica-Ileana12ORCID,Dinca Liviu1,Cican Grigore34ORCID,Ionescu Adriana5ORCID,Negru Mihai6ORCID,Bogateanu Radu2,Cucu Andra-Adelina1ORCID

Affiliation:

1. Department of Electrical, Energetic and Aerospace Engineering, Faculty of Electrical Engineering, University of Craiova, 200441 Craiova, Romania

2. I.N.C.A.S.—National Institute for Aerospace Research, “Elie Carafoli”, 061126 Bucharest, Romania

3. National Research and Development Institute for Gas Turbines COMOTI, 220D Iuliu Maniu, 061126 Bucharest, Romania

4. Faculty of Aerospace Engineering, National Polytechnic University of Science and Technology Bucharest, 011061 Bucharest, Romania

5. Department of Applied Mechanics and Civil Constructions, Faculty of Mechanics, University of Craiova, 200441 Craiova, Romania

6. Department of Automotive, Transportation and Industrial Engineering, Faculty of Mechanics, University of Craiova, 200441 Craiova, Romania

Abstract

The increase in greenhouse gas emissions, as well as the risk of fossil fuel depletion, has prompted a transition to electric transportation. The European Union aims to substantially reduce pollutant emissions by 2035 through the use of renewable energies. In aviation, this transition is particularly challenging, mainly due to the weight of onboard equipment. Traditional electric motors with radial magnetic flux have been replaced by axial magnetic flux motors with reduced weight and volume, high efficiency, power, and torque. These motors were initially developed for electric vehicles with in-wheel motors but have been adapted for aviation without modifications. Worldwide, there are already companies developing propulsion systems for various aircraft categories using such electric motors. One category of aircraft that could benefit from this electric motor development is traditionally constructed training aircraft with significant remaining flight resource. Electric repowering would allow their continued use for pilot training, preparing them for future electrically powered aircraft. This article presents a study on the feasibility of repowering a classic training aircraft with an electric propulsion system. The possibilities of using either a battery or a hybrid source composed of a battery and a fuel cell as an energy source are explored. The goal is to utilize components already in production to eliminate the research phase for specific aircraft components.

Funder

Electric, Energetic and Aerospace Engineering Department of the University of Craiova

Publisher

MDPI AG

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