A system (200) for transmitting an alternating current in an aircraft. The system includes a source of electricity (121) in the aircraft having a source connector housing (202), an electric load (106) in the aircraft having a load connector housing (204), a cable (206) electrically coupling the source of electricity (121) to the electric load (106), a shield (220) surrounding the cable (206) and having a first end (208) electrically connected to the source connector housing (202), and a capacitor (226) disposed inside the load connector housing (204) and electrically coupling a second end (210) of the shield (220) to the load connector housing (204).


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    Title :

    WIRING HARNESS CONDUCTIVE SHIELD TERMINATION ARRANGEMENT


    Additional title:

    LEITFÄHIGE ABGESCHIRMTE KABELBAUMABSCHLUSSANORDNUNG
    AGENCEMENT DE TERMINAISON DE BLINDAGE CONDUCTEUR DE FAISCEAU DE CÂBLES


    Contributors:

    Publication date :

    2025-08-13


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    H02K Dynamoelektrische Maschinen , DYNAMO-ELECTRIC MACHINES / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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