发明名称 Input system for flap control of an airplane
摘要 <p>The system (2) has a selector lever (4) pivotably supported by a shaft unit (10) to input a landing flap position. A sensor arrangement (22) arranged at a side of the lever includes two optoelectronic sensor units (24) to detect a position of the lever. A single-piece shaft element of the shaft unit is guided-through by the lever until the sensor units. The sensor units have sensor elements (28) fastened to the shaft element for transferring a movement of the shaft element to the sensor elements. The shaft element supports a brake unit (34) to decelerate the movement of the lever.</p>
申请公布号 EP2130764(B1) 申请公布日期 2013.11.20
申请号 EP20090006195 申请日期 2009.05.07
申请人 DIEHL AEROSPACE GMBH 发明人 KUMMLE, WOLFGANG
分类号 B64C13/04 主分类号 B64C13/04
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