| Issue |
MATEC Web Conf.
Volume 304, 2019
9th EASN International Conference on “Innovation in Aviation & Space”
|
|
|---|---|---|
| Article Number | 03011 | |
| Number of page(s) | 8 | |
| Section | Propulsion & Engines | |
| DOI | https://doi.org/10.1051/matecconf/201930403011 | |
| Published online | 17 December 2019 | |
Electric motor-glider powered by a hydrogen fuel cell stack
1
Institute of Aviation and Applied Mechanics, Warsaw University of Technology,
Nowowiejska 24,
00-665
Warsaw,
Poland
2
AGH University of Science and Technology, Faculty of Energy and Fuels,
Al. Mickiewicza 30,
30-059
Krakow,
Poland
3
AGH University of Science and Technology, Faculty of Electrical Engineering, Automatics, Computer Science and Biomedical Engineering,
Al. Mickiewicza 30,
30-059
Krakow,
Poland
4
Institute of Control and Industrial Electronics, Warsaw University of Technology,
Koszykowa 75,
00-662
Warsaw,
Poland
5
Faculty of Transport, Warsaw University of Technology,
Koszykowa 75,
00-662
Warsaw,
Poland
* Corresponding author: pecz@meil.pw.edu.pl
The paper presents the current development of the AOS-H2 electric motor-glider project. The project encompasses the design and manufacture of an electric propulsion system (EPS) and a CF/epoxy airframe to be used as a flying test platform for the designed EPS. A 40-kW electric motor is supplied by a 10-kW PEM fuel cell stack and a Li-ion battery during run-up and ascent and by the fuel cell stack alone during steady flight. The airframe and the EPS have been completed; the results of bench tests of the EPS have proved that it meets the established requirements..
© The Authors, published by EDP Sciences, 2019
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