A fairing drive assembly couples a flap assembly of a wing of an aircraft to a fairing of the wing. The fairing drive assembly may include a fairing cam including a first joint and a second joint, and a flap link pivotally coupled to the first joint of the fairing cam and the flap assembly. A fairing drive arm is pivotally coupled to the second joint and the fairing. The fairing cam is configured to rotate upon actuation of the flap assembly and deflect the fairing away from the flap assembly.

    Un mécanisme dentraînement de carénage couple un assemblage de volet dune aile daéronef à un carénage de laile. Le mécanisme dentraînement de carénage peut comprendre une came de carénage ayant un premier et un deuxième joint, et un lien de volet raccordé en relation de pivot au premier joint de la came et à lassemblage de volet. Un bras dentraînement de carénage est raccordé en relation de pivot au deuxième joint et au carénage. La came de carénage est conçue pour tourner à lactionnement de lassemblage de volet et dévier le carénage pour léloigner de lassemblage de volet.


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    Title :

    AIRCRAFT WING FAIRING DRIVE ASSEMBLY, SYSTEM, AND METHOD


    Additional title:

    MECANISME D'ENTRAINEMENT DE CARENAGE D'AILE D'AERONEF, SYSTEME ET METHODE


    Contributors:

    Publication date :

    2021-01-05


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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