Input system for a landing flap control of an aircraft
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United States of America Patent
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-
Feb 28, 2012
Grant Date -
Apr 1, 2010
app pub date -
Apr 21, 2009
filing date -
May 14, 2008
priority date (Note) -
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status (Latency Note)
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Abstract
An input system (2) for a landing flap control of an aircraft. In order to make the input system (2) compact, light and reliable, it is provided with a selector lever (4) mounted pivotably by a shaft unit (10) for the input of a landing flap position, and a sensor arrangement (22) being arranged at one side of the selector lever (4) and having two mutually redundant optoelectronic sensor units (24) each for detecting a position of the selector lever (4), wherein a one-piece shaft element (40) of the shaft unit (10) is passed from the selector lever (4) through the sensor units (24).
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