| 摘要 |
<p>A nacelle (12) includes leading edge slats (28) movable to modify inlet shape and area airflow into the nacelle (12). The articulating leading edge slats (28) are movable for tailoring incoming airflow to current aircraft operating conditions. An actuator (36) disposed within a thickness of the nacelle (12) drives leading edge slats (28) to a desired position to vary the inlet area and shape.</p> |
