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Airplane wing with slat and Krueger flap

机译:带有机翼和克鲁格襟翼的飞机机翼

摘要

The present invention relates to an airplane wing (1) with leading edge devices, said leading edge devices comprising one or more slats (12) and at least one Krueger flap (13) per side. Said one or more slats (12) and said at least one Krueger flap (13) are driven by a common power drive unit (21) through a common shaft system (22) between a normal flight position (a hold/descent position), a take-off position and a landing position. The incompatibility of the flap sequence between slat (12) and Krueger (13) is overcome by using an over center drive arrangement in the Krueger actuation (20).
机译:具有前缘装置的飞机机翼(1),所述前缘装置每侧包括一个或多个板条(12)和至少一个克鲁格襟翼(13)。所述一个或多个板条(12)和所述至少一个克鲁格襟翼(13)由共同的动力驱动单元(21)在正常飞行位置(保持/下降位置)之间通过共同的轴系统(22)驱动,起飞位置和着陆位置。通过在克鲁格致动器(20)中使用偏心驱动装置,可以克服板条(12)和克鲁格(13)之间的襟翼顺序不兼容的问题。

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