A hidden latch system for an interior structure of an aircraft includes at least two engagement features coupled to an interior structure of an aircraft. Each of the at least two engagement features includes an engagement portion, an engagement rod, and a self-centering feature. The engagement portion is configured to engage and release the engagement rod, and the self-centering feature is configured to self-center the engagement rod in at least one direction. Further, the engagement portion is configured to release the engagement rod using a cable pull system.


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    Titel :

    Remotely-activated self-centering cable latch


    Beteiligte:
    TERRY TROY N (Autor:in) / SCHOALES JASEN P (Autor:in)

    Erscheinungsdatum :

    16.04.2019


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    E05B LOCKS , Schlösser / B64C AEROPLANES , Flugzeuge / E05C Riegel oder Feststellvorrichtungen für Flügel, insbesondere für Türen oder Fenster , BOLTS OR FASTENING DEVICES FOR WINGS, SPECIALLY FOR DOORS OR WINDOWS



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    TERRY TROY N / SCHOALES JASEN P | Europäisches Patentamt | 2017

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    SIRAGUSA GEORGE | Europäisches Patentamt | 2022

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    SELF-CENTERING CABLE STRAP

    SIRAGUSA GEORGE | Europäisches Patentamt | 2017

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