An electrical connector includes a first pass-through connector, a second pass-through connector, and a center portion coupled between the first pass-through connector and the second pass-through connector. The center portion includes a plurality of electrical connection points on an exterior surface of the center portion. The electrical connector also includes a plurality of pass-through wires extending from the first pass-through connector to the second pass-through connector through the center portion, wherein the plurality of electrical connection points are electronically coupled to the plurality of pass-through wires.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Avionics system interface electrical connector


    Beteiligte:

    Erscheinungsdatum :

    2020-02-04


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    H01R Elektrisch leitende Verbindungen , ELECTRICALLY-CONDUCTIVE CONNECTIONS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / H01B CABLES , Kabel / 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



    AVIONICS SYSTEM INTERFACE ELECTRICAL CONNECTOR

    ALLEN MICHAEL JAMES | Europäisches Patentamt | 2019

    Freier Zugriff

    Avionics interface

    FYMAT STÉPHANE | Europäisches Patentamt | 2017

    Freier Zugriff

    Modern avionics connector unreliability

    MORRISON, R. / SIMMONS, JONATHON | AIAA | 1989


    Avionics Interface

    FYMAT STÉPHANE | Europäisches Patentamt | 2018

    Freier Zugriff

    AVIONICS PLUGGABLE ACTIVE OPTICAL CONNECTOR

    TRUONG TUONG K / CHAN ERIC Y / KOSHINZ DENNIS G et al. | Europäisches Patentamt | 2020

    Freier Zugriff