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Low noise blade slat system with deployable blade leading edge element

机译:具有可展开叶片前缘元件的低噪声叶片板条系统

摘要

Concepts and technologies described herein provide for a low noise aircraft wing slat system. According to one aspect of the disclosure provided herein, a cove-filled wing slat is used in conjunction with a moveable leading edge element of an aircraft wing to provide a high lift system. The moveable leading edge element may include a one-piece or two-piece panel that retracts within the aircraft wing to accommodate the cove-filled slat in the stowed position. Upon deployment of the cove-filled slat, the moveable leading edge element deploys outward to create a continuous outer mold line shape with the wing.
机译:本文描述的概念和技术提供了低噪声的飞机机翼板条系统。根据本文提供的本公开的一个方面,将充满凹面的机翼板条与飞机机翼的可移动的前缘元件结合使用以提供高升力系统。可移动的前缘元件可以包括一件式或两件式的面板,该面板在飞机机翼内缩回以在收起位置容纳充满海湾的板条。在展开充满海湾的板条时,可移动的前缘元件向外展开,以与机翼形成连续的外部造型线形状。

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