K. Krall, L.-H. Lemke, F. Thielecke, J. Müller, C. Breitenstein

Dynamic load control offers a high potential for the improvement of aerodynamic performance and increase in passenger comfort. However, it is unclear if the implementation is feasible or even possible regarding the actuation system design. The demand of actively reducing gust loads acting on the wing results in challenging requirements for the actuation systems regarding high actuation speeds and loads. In this paper, promising actuation concepts for fast actuated droop noses and flap-tabs will be analysed based on preliminary designs. Furthermore, the impact on the overall system level is discussed.

Deutscher Luft- und Raumfahrtkongress 2023, Stuttgart

Deutsche Gesellschaft für Luft- und Raumfahrt - Lilienthal-Oberth e.V., Bonn, 2024

Conference Paper

englisch

21,0 x 29,7 cm, 9 Seiten

urn:nbn:de:101:1-2024011712360724345431

10.25967/610047

Droop nose, dynamic load control, fast actuation, preliminary sizing, systems architecture, system design

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Krall, K.; Lemke, L.-H.; et al. (2024): Systems for Fast Actuated Droop Noses and Flap-Tabs for Dynamic Load Control. Deutsche Gesellschaft für Luft- und Raumfahrt - Lilienthal-Oberth e.V.. (Text). https://doi.org/10.25967/610047. urn:nbn:de:101:1-2024011712360724345431.

17.01.2024