Systems, apparatuses and methods may provide for a verification system for an aircraft. The verification system includes a verification function subsystem to automatically verify an operational condition of one or more components of an aircraft based on airflow related signals, hydraulic related signals, and electrical signals and associated impedances and present the operational condition via a display. The airflow related signals may be obtained from a plurality of airflow fittings, the hydraulic related signals may be obtained from a plurality of hydraulic fittings, and the electrical signals and associated impedances may be obtained from a plurality of electrical connectors. At least two of the airflow fittings, at least two of the hydraulic fittings, and at least two of the electrical connectors may be positioned in different aircraft sections before additional aircraft sections are assembled.


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    Titel :

    CONTINUOUS AIRPLANE VERIFICATION TO IMPROVE PRODUCTION BUILD EFFICIENCY


    Beteiligte:
    DOAN VINH Q (Autor:in) / PHAN TRI MINH (Autor:in) / HSU SHU HSIN ROBIN (Autor:in) / GONZALEZ LUIS ROGELIO (Autor:in) / LEE RICKIE (Autor:in) / CERNA HOMERO S (Autor:in)

    Erscheinungsdatum :

    12.05.2022


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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    Freier Zugriff

    CONTINUOUS AIRPLANE VERIFICATION TO IMPROVE PRODUCTION BUILD EFFICIENCY

    DOAN VINH Q / PHAN TRI MINH / HSU SHU HSIN ROBIN et al. | Europäisches Patentamt | 2024

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