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ACTUATOR ASSEMBLIES TO DEPLOY AIRCRAFT LEADING EDGE FLAPS AND SEALS FOR AIRCRAFT LEADING EDGE FLAPS

机译:执行器组件,用于部署飞机前缘襟翼和密封件,用于飞机前缘襟翼

摘要

To provide an actuator system for leading edge flaps allowing application of simple, light, small and inexpensive actuators.SOLUTION: A system comprises: an aircraft flap 202 including a top panel 308, a notch formed in the top panel 308 and extending into a side of the top panel 308 near a trailing edge 313 of the flap 202; and a seal coupled to the flap 202, the seal movable to cover the notch when the flap 202 is in the deployed position.SELECTED DRAWING: Figure 3B
机译:为了提供一种用于前缘襟翼的致动器系统,允许应用简单,轻便,小型和廉价的致动器。解决方案:一种系统包括:飞机襟翼202,其包括顶板308,形成在顶板308中并延伸到侧面的凹口。顶板308在襟翼202的后缘313附近;密封件与翼片202相连,当翼片202处于展开位置时,该密封件可移动以覆盖凹口。

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