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Comparison of electro-hydraulic and electro-mechanic landing gear actuation for light VTOL aircraft
Publikationstyp
Conference Presentation
Date Issued
2021-09
Sprache
English
Author(s)
Springmann, Raphael
Institut
Citation
70. Deutscher Luft- und Raumfahrtkongress, (DLRK 2021)
Contribution to Conference
Peer Reviewed
false
In this paper, a landing gear actuation system for a light VTOL aircraft is predesigned aiming for minimal power consumption and low weight. Electro-hydraulic and electro-mechanic system architectures are taken into account.
DDC Class
600: Technik