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首页> 外国专利> METHOD FOR DETERMINING A STATE OF A COMPONENT IN A HIGH LIFT SYSTEM OF AN AIRCRAFT, HIGH LIFT SYSTEM OF AN AIRCRAFT AND AIRCRAFT HAVING SUCH A HIGH LIFT SYSTEM

METHOD FOR DETERMINING A STATE OF A COMPONENT IN A HIGH LIFT SYSTEM OF AN AIRCRAFT, HIGH LIFT SYSTEM OF AN AIRCRAFT AND AIRCRAFT HAVING SUCH A HIGH LIFT SYSTEM

机译：确定飞机高升降系统中组件状态的方法，飞机高升降系统和具有这种高升降系统的飞机

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A method for determining a state of a component in a high lift system (2) ofanaircraft is proposed, the high lift system (2) comprising a central powercontrol unit (4) forproviding rotational power by means of a transmission shaft (8, 10); and drivestations(12) coupled with the power control unit (4) and movable high lift surfaces(18); themethod comprising the steps of acquiring in an extended position in flight atleast one firstposition of a first position pick-off unit (20) coupled with the component,which ismechanically coupled with one of the high lift surfaces (18), and which iscoupled withone of the drive stations (12), acquiring on ground at least one secondposition of the firstposition pick-off unit (20) in the extended position, determining a deviationbetween ameasure based on the first position and an associated measure based on thesecondposition of the first position pick-off unit (20) between ground and flight,determining,whether the deviation exceeds a predetermined threshold and generating asignalindicating an abnormal state of the component in case the deviation exceedsthepredetermined threshold.
机译：确定高举升系统（2）中组件状态的方法一个提出了飞机，包括中央动力的高升力系统（2）控制单元（4）通过传动轴（8、10）提供旋转动力;开车车站（12）与动力控制单元（4）和可移动的高升力表面相连（18）;的方法包括以下步骤：在至少一个第一与部件耦合的第一位置拾取单元（20）的位置，这是与高升力面（18）之一机械耦合，加上其中一个驱动站（12），在地面上至少捕获一秒钟第一个位置位置拾取单元（20）处于伸出位置，确定偏差之间基于第一个位置的度量和基于第二第一位置传感器（20）在地面和飞行之间的位置，决定，偏差是否超过预定阈值并生成信号如果偏差超过指示组件的异常状态的预定阈值。

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