Provided is a transition assembly for a wire harness configured to be coupled to a plate in an aircraft. The transition assembly includes a slotted flange configured to abut a first side of the plate, a junction having a flange configured to abut a second side of the plate, the flange including inwardly extending cutouts on opposite sides thereof forming a reduced width portion of the flange, and a nut configured to couple to the junction.


    Access

    Download


    Export, share and cite



    Title :

    AIRCRAFT WIRE HARNESS


    Contributors:

    Publication date :

    2024-07-18


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B60R Fahrzeuge, Fahrzeugausstattung oder Fahrzeugteile, soweit nicht anderweitig vorgesehen , VEHICLES, VEHICLE FITTINGS, OR VEHICLE PARTS, NOT OTHERWISE PROVIDED FOR



    Wire harness protector and wire harness

    SHEN JUN | European Patent Office | 2020

    Free access

    WIRE HARNESS SYSTEM AND WIRE HARNESS

    KIYOSUE KAZUOMI / KINOSHITA KOUSUKE / NAGANISHI YUKINARI et al. | European Patent Office | 2017

    Free access

    Wire harness, wire harness manufacturing method, and wire harness routing structure

    TAMURA ISSEI / KOCHIBE MASAHIRO | European Patent Office | 2024

    Free access

    WIRE HARNESS SYSTEM AND WIRE HARNESS

    INOUE HIROMICHI / KINOSHITA KOSUKE / KIYOSUE KAZUOMI et al. | European Patent Office | 2017

    Free access

    Wire harness and wire harness routing structure

    MURATA TAKAHIRO | European Patent Office | 2023

    Free access