A system may include an aircraft galley insert configured to be installed within an aircraft galley insert bay, a mounting plate attached to a rear of the aircraft galley insert, and a power connector assembly attached to the mounting plate. The power connector assembly may include compressible spring assemblies that compress as the power connector assembly is mated with a corresponding power connector assembly of the aircraft galley insert bay. The power connector assembly may self-align with the corresponding power connector assembly of the aircraft galley insert bay when the aircraft galley insert is installed within the aircraft galley insert bay.


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    Titel :

    Galley Insert Power Connector Assembly with Spring Assemblies


    Beteiligte:

    Erscheinungsdatum :

    16.09.2021


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    H01R Elektrisch leitende Verbindungen , ELECTRICALLY-CONDUCTIVE CONNECTIONS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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