| タイトル | Method for a Leading Edge Slat on a Wing of an Aircraft |
| 本文（外部サイト） | http://hdl.handle.net/2060/20160011993 |
| 著者（英） | Eckstein, Nicholas Stephen; Pitt, Dale M. |
| 著者所属（英） | Boeing Co. |
| 発行日 | 2016-09-20 |
| 言語 | eng |
| 内容記述 | A method for managing a flight control surface system. A leading edge device is moved on a leading edge from an undeployed position to a deployed position. The leading edge device has an outer surface, an inner surface, and a deformable fairing attached to the leading edge device such that the deformable fairing covers at least a portion of the inner surface. The deformable fairing changes from a deformed shape to an original shape when the leading edge device is moved to the deployed position. The leading edge device is then moved from the deployed position to the undeployed position, wherein the deformable fairing changes from the original shape to the deformed shape. |
| NASA分類 | Aircraft Design, Testing and Performance |
| 権利 | No Copyright |
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