| 摘要 |
<p>A wing assembly (24,38) for an aircraft moveable slat system (20) has a fixed structure (40) and a contoured surface (42,44). The fixed structure has an exterior surface defining an external contour and an internal surface defining a cavity (50). The fixed structure also has one or more edges defining a cutout (26). The contoured surface is coupled to one or more of the edges of the cutout and extends into the cavity. The contoured surface promotes airflow from the cavity to the external contour. The result is a solution to aerodynamic losses that does not require an auxiliary track system or moving parts. <IMAGE></p> |
