发明名称 |
Method for determining the position of a component in a high lift system of an aircraft, high lift system of an aircraft and aircraft |
摘要 |
A method for determining the position of a component in a high lift system (2) of an aircraft, the high lift system comprising a central power control unit (4) for providing rotational power by means of a transmission shaft (6); and actuator drive stations (12) coupled with the power control unit (4) and movable high lift surfaces (18); the method comprises the steps of acquiring a first rotational position of a first position pick-off unit (20) mechanically coupled with the power control unit by means of a first gear having a first gear ratio, acquiring at least one second rotational position of at least one second position pick-off unit (20) mechanically coupled with a driven element in at least one drive station (12), determining the number of full rotations the first position pick-off unit (20) has already accomplished between a neutral position and an intended maximum number of rotations based on an associated number of angle sections of the second position pick-off unit (20) and the actual second rotational position and multiplying the number of full rotations of the first position pick-off unit with 360° and adding the resulting full rotations angle to the measured first rotational position to acquire the first rotational position. The accuracy and the reusability of feedback position pick-off units (20) is thereby clearly improved. |
申请公布号 |
EP2947004(A1) |
申请公布日期 |
2015.11.25 |
申请号 |
EP20140169679 |
申请日期 |
2014.05.23 |
申请人 |
AIRBUS OPERATIONS GMBH |
发明人 |
NEB, EUGEN;WYREMBEK, JÖRG;MAIRE, VINCENT |
分类号 |
B64C9/16;B64C9/00;B64C9/22;B64C13/16;B64C13/28;B64D45/00 |
主分类号 |
B64C9/16 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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