An assembly is provided for an aircraft propulsion system (20). This assembly includes a fanlet (32) and a track system (48) configured to enable axial translation of the fanlet (32) along a centerline (26) between an open position and a closed position. The track system (48) includes a first component (64), a second component (66) and a lock (68). One of the first and the second components (64, 66) is configured as or otherwise includes a slider (78). The other one of the first and the second components (64, 66) is configured as or otherwise includes a track (96). The slider (78) is mated with and configured to slide axially along the track (96). The lock (68) is configured as or otherwise includes a bolt (106) mounted with the first component (64). The lock (68) is configured to move the bolt (106) laterally into an aperture (100) in the second component (66) to prevent axial translation of the fanlet (32).


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    Title :

    LOCKABLE TRACK SYSTEM FOR A TRANSLATING NACELLE STRUCTURE


    Additional title:

    SPERRBARES VERRIEGELUNGSSYSTEM FÜR EINE VERSCHIEBBARE TRIEBWERKSGONDELSTRUKTUR
    SYSTEME DE VERROUILLAGE DE VOIES POUR UNE STRUCTURE DE NACELLE COULISSANTE


    Contributors:
    LU JINQIU (author)

    Publication date :

    2020-01-01


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F02K JET-PROPULSION PLANTS , Strahltriebwerke



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