An air delivery lock for a cargo located in an aircraft, comprises a housing (4), a restraining device (10) having an engagement end (12) for contacting and restraining the cargo, and a force reaction end (38); a bell crank (22) having a bell crank joint (28) for swivably mounting the bell crank (22); an elastically deformable force introduction unit (36); and a latching unit (46); wherein the restraining device (10) is swivably mounted on a first leg (24) of the bell crank around a restraining device axis. The force introduction unit is attached to a second leg (26) of the bell crank (22) and the force reaction end (38) of the restraining device (10). A first guide means (48, 82) attached to the housing (4) and a second guide means (54, 88) attached to the restraining device (10) are designed to prevent a rotation of the bell crank (22) until a predetermined release force is reached on the engagement end (12) of the restraining device (10). A contacting head 14, that is swivably mounted on the restraining device (10), at the engagement end (12) by means of an axis (16, 80) or, in a different embodiment, by a spherical joint.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    ЗАМОК ДЛЯ ДОСТАВЛЯЕМОГО ВОЗДУХОМ ГРУЗА, РАЗМЕЩЕННОГО НА БОРТУ ЛЕТАТЕЛЬНОГО АППАРАТА, И СИСТЕМА ЕГО ЗАКРЕПЛЕНИЯ


    Erscheinungsdatum :

    23.09.2019


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Russisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT