A system for transmitting an alternating current in an aircraft. The system includes a source of electricity in the aircraft having a source connector housing, an electric load in the aircraft having a load connector housing, a cable electrically coupling the source of electricity to the electric load, a shield surrounding the cable and having a first end electrically connected to the source connector housing, and a capacitor disposed inside the load connector housing and electrically coupling a second end of the shield to the load connector housing.


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    Title :

    WIRING HARNESS CONDUCTIVE SHIELD TERMINATION ARRANGEMENT


    Contributors:

    Publication date :

    2025-08-07


    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 / H01B CABLES , Kabel



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