페어링 구동 어셈블리는 날개의 페어링에 항공기의 날개의 플랩 어셈블리를 결합한다. 페어링 구동 어셈블리는 제1 조인트 및 제2 조인트를 포함하는 페어링 캠과, 페어링 캠의 제1 조인트 및 플랩 어셈블리에 선회가능하게 결합된 플랩 링크를 포함할 수 있다. 페어링 구동 암은 제2 조인트 및 페어링에 선회가능하게 결합된다. 페어링 캠은 플랩 어셈블리의 작동에 따라 회전하고 플랩 어셈블리로부터 떨어져 페어링의 방향을 바꾸도록 구성된다.

    A fairing drive assembly (200) 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 (204) including a first joint and a second joint, and a flap link (240) pivotally coupled to the first joint of the fairing cam and the flap assembly. A fairing drive arm (220) 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.


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    Title :

    AIRCRAFT WING FAIRING DRIVE ASSEMBLY SYSTEM AND METHOD


    Additional title:

    항공기 날개 페어링 구동 어셈블리, 시스템 및 방법


    Contributors:

    Publication date :

    2017-06-13


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Korean


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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