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.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    AIRCRAFT WIRE HARNESS


    Beteiligte:
    JAEGER MARK (Autor:in) / HINMAN WILLIAM (Autor:in)

    Erscheinungsdatum :

    18.07.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



    AIRCRAFT WIRE HARNESS

    BIELUCH THOMAS / DUTRA JOHN | Europäisches Patentamt | 2024

    Freier Zugriff

    WIRE HARNESS, WIRE HARNESS BODY, AND HARNESS MODULE

    OHARA SHUNEI / KATSUMATA TAKAMITSU / OGUSU MASAMICHI et al. | Europäisches Patentamt | 2016

    Freier Zugriff

    WIRE HARNESS, WIRE HARNESS MANUFACTURING METHOD AND WIRE HARNESS MANUFACTURING DEVICE

    ENOMOTO SATOSHI / NAKAMURA MASASHI / TADOKORO SHINICHI et al. | Europäisches Patentamt | 2021

    Freier Zugriff

    WIRE HARNESS SHEET, WIRE HARNESS, AND METHOD OF MANUFACTURING WIRE HARNESS

    KAWAGUCHI KENICHIRO / TSUNODA MITSUNORI | Europäisches Patentamt | 2018

    Freier Zugriff

    WIRE HARNESS SYSTEM AND WIRE HARNESS

    INOUE HIROMICHI / KINOSHITA KOSUKE / KIYOSUE KAZUOMI et al. | Europäisches Patentamt | 2017

    Freier Zugriff