Aircraft throttle control device including a cam coupling
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United States of America Patent
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Aug 8, 2017
Grant Date -
Mar 6, 2014
app pub date -
Sep 30, 2013
filing date -
Oct 6, 2009
priority date (Note) -
In Force
status (Latency Note)
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Abstract
An aeroengine control device including a mount and having pivotally mounted thereon a code wheel together with a main lever and a secondary lever, both for turning the code wheel. Each lever is movable between a rest position and a maximum actuation position. The secondary lever is mounted to pivot on the main lever. Cam paths are mounted on the code wheel and on the mount in such a manner that the main lever can move the code wheel when the main lever is moved while the secondary lever is in the rest position. The secondary lever can move the code wheel when the secondary lever is moved while the main lever is in the rest position, with movement of either lever being prevented when the other lever is clearly away from its rest position.
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