An assembly is provided for an aircraft propulsion system. This assembly includes a fanlet and a track system configured to enable axial translation of the fanlet along a centerline between an open position and a closed position. The track system includes a first component, a second component and a lock. One of the first and the second components is configured as or otherwise includes a slider. The other one of the first and the second components is configured as or otherwise includes a track. The slider is mated with and configured to slide axially along the track. The lock is configured as or otherwise includes a bolt mounted with the first component. The lock is configured to move the bolt laterally into an aperture in the second component to prevent axial translation of the fanlet.


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    Titel :

    LOCKABLE TRACK SYSTEM FOR A TRANSLATING NACELLE STRUCTURE


    Beteiligte:
    LU JINQIU (Autor:in)

    Erscheinungsdatum :

    2018-05-24


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F02K JET-PROPULSION PLANTS , Strahltriebwerke



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