Provided is a thermocouple wire harness including a first branch, a second branch extending about ninety degrees from the first branch in a first direction and having a first pair of thermocouple terminal breakouts extending therefrom for coupling to a first thermocouple, and a third branch extending about ninety degrees from the first branch in a second direction opposite the first direction, the third branch having a second pair of thermocouple terminal breakouts extending therefrom for coupling to a second thermocouple, a third pair of thermocouple terminal breakouts extending therefrom for coupling to a third thermocouple, and a fourth pair of thermocouple terminal breakouts extending therefrom for coupling to a fourth thermocouple.


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    Titel :

    AIRCRAFT WIRE HARNESS


    Beteiligte:
    BIELUCH THOMAS (Autor:in) / DUTRA JOHN (Autor:in)

    Erscheinungsdatum :

    17.10.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / H02G INSTALLATION OF ELECTRIC CABLES OR LINES, OR OF COMBINED OPTICAL AND ELECTRIC CABLES OR LINES , Verlegen oder Installieren elektrischer Kabel oder Leitungen, Verlegen oder Installieren kombinierter optischer und elektrischer Kabel oder Leitungen



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