Proceedings of the International Conference "Actual Issues of Mechanical Engineering" (AIME 2018)

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Determining parameters of electric power unit for light aircraft

Authors
Dmitry Bakholdin, Valery Biryukov, Lyudmila Tolstobrova
Corresponding Author
Dmitry Bakholdin
Available Online April 2018.
DOI
10.2991/aime-18.2018.13How to use a DOI?
Keywords
electric power unit; light aircraft; flight range;
Abstract

The article is devoted to the comparison of the characteristics of electric traction aircrafts and those equipped with classic ICE. The calculation of the flight range of aircraft equipped with an electric motion has been made.

Copyright
© 2018, the Authors. Published by Atlantis Press.
Open Access
This is an open access article distributed under the CC BY-NC license (http://creativecommons.org/licenses/by-nc/4.0/).

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Volume Title
Proceedings of the International Conference "Actual Issues of Mechanical Engineering" (AIME 2018)
Series
Advances in Engineering Research
Publication Date
April 2018
ISBN
978-94-6252-563-4
ISSN
2352-5401
DOI
10.2991/aime-18.2018.13How to use a DOI?
Copyright
© 2018, the Authors. Published by Atlantis Press.
Open Access
This is an open access article distributed under the CC BY-NC license (http://creativecommons.org/licenses/by-nc/4.0/).

Cite this article

risenwbib
TY  - CONF
AU  - Dmitry Bakholdin
AU  - Valery Biryukov
AU  - Lyudmila Tolstobrova
PY  - 2018/04
DA  - 2018/04
TI  - Determining parameters of electric power unit for light aircraft
BT  - Proceedings of the International Conference "Actual Issues of Mechanical Engineering" (AIME 2018)
PB  - Atlantis Press
SP  - 65
EP  - 69
SN  - 2352-5401
UR  - https://doi.org/10.2991/aime-18.2018.13
DO  - 10.2991/aime-18.2018.13
ID  - Bakholdin2018/04
ER  -