Detail publikace

Electrical Drivetrain of the Small Airplane and Mutual Interaction of this Drivetrain

PAZDERA, I. PROCHÁZKA, P. ČERVINKA, D. KLÍMA, B.

Originální název

Electrical Drivetrain of the Small Airplane and Mutual Interaction of this Drivetrain

Anglický název

Electrical Drivetrain of the Small Airplane and Mutual Interaction of this Drivetrain

Jazyk

en

Originální abstrakt

This paper describes conception of the drivetrain system of the full electric piloted aircraft. There are described all basic drivetrain units and their mutual interaction to achieve safety operation of the aircraft during the flight. Therefore the whole complex drive system is designed with respect to high demands on safety operation of the aircraft. There are no duplications of the basic units therefore all the units are designed with appropriate reserve margins and control systems are combined with software and hardware protections where each replace the other in case of failure.

Anglický abstrakt

This paper describes conception of the drivetrain system of the full electric piloted aircraft. There are described all basic drivetrain units and their mutual interaction to achieve safety operation of the aircraft during the flight. Therefore the whole complex drive system is designed with respect to high demands on safety operation of the aircraft. There are no duplications of the basic units therefore all the units are designed with appropriate reserve margins and control systems are combined with software and hardware protections where each replace the other in case of failure.

Dokumenty

BibTex 


@inproceedings{BUT102717,
  author="Ivo {Pazdera} and Petr {Procházka} and Dalibor {Červinka} and Bohumil {Klíma}",
  title="Electrical Drivetrain of the Small Airplane and Mutual Interaction of this Drivetrain",
  annote="This paper describes conception of the drivetrain system of the full electric piloted aircraft. There are described all basic drivetrain units and their mutual interaction to achieve safety operation of the aircraft during the flight. Therefore the whole complex drive system is designed with respect to high demands on safety operation of the aircraft. There are no duplications of the basic units therefore all the units are designed with appropriate reserve margins and control systems are combined with software and hardware protections where each replace the other in case of failure.",
  booktitle="Proceedings of the IECON 2013 - 39th Annual Conference of the IEEE Industrial Electronics Society",
  chapter="102717",
  howpublished="electronic, physical medium",
  year="2013",
  month="november",
  pages="1--6",
  type="conference paper"
}