Systems and methods for structural integrity management system for an aircraft. The system includes an electronic processor configured to receive information regarding damage to a component of the aircraft, update a digital twin model associated with the aircraft based on the received information, and perform a rapid structural analysis using the updated digital twin model. The electronic processor is further configured to determine, based on the results of the rapid structural analysis and either or both of a historic use of the aircraft and a current future usage profile of the aircraft, an actionable direction, and perform the actionable direction.


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    Title :

    INTEGRAL STRUCTURAL INTEGRITY MANAGEMENT SYSTEM FOR AIRCRAFT


    Additional title:

    INTEGRIERTES SYSTEM ZUR VERWALTUNG DER STRUKTURELLEN INTEGRITÄT FÜR FLUGZEUGE
    SYSTÈME DE GESTION D'INTÉGRITÉ STRUCTURALE INTÉGRALE POUR AÉRONEF


    Contributors:

    Publication date :

    2025-02-19


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    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 / G05B Steuer- oder Regelsysteme allgemein , CONTROL OR REGULATING SYSTEMS IN GENERAL / G06Q Datenverarbeitungssysteme oder -verfahren, besonders angepasst an verwaltungstechnische, geschäftliche, finanzielle oder betriebswirtschaftliche Zwecke, sowie an geschäftsbezogene Überwachungs- oder Voraussagezwecke , DATA PROCESSING SYSTEMS OR METHODS, SPECIALLY ADAPTED FOR ADMINISTRATIVE, COMMERCIAL, FINANCIAL, MANAGERIAL, SUPERVISORY OR FORECASTING PURPOSES



    INTEGRATED STRUCTURAL INTEGRITY MANAGEMENT SYSTEM FOR AIRCRAFT

    BROOKHART ANDREW M / SARLASHKAR AVINASH V | European Patent Office | 2025

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