Aircraft throttle control device including an engaging roller coupling

An aeroengine control device comprising a mount, having pivotally mounted thereon a code wheel together with a main lever and a secondary lever, both for turning the code wheel, each lever being movable between a rest position and a maximum actuation position, the secondary lever being mounted to pi...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: Elabellaoui Hafid, Engler David, Besold Jean-Eric, Pautard Sébasiten, Merlet Etienne
Format: Patent
Sprache:eng
Schlagworte:
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