A computerized system for determining the design layout of an aircraft. The system includes an input module configured to receive a first input data indicating a first value of a first parameter, a first feature database that includes a plurality of feature settings, a feature search module configured to search the first feature database and select a feature setting based on the first value of the first parameter, a central database that includes a plurality of rules governing a design layout of a fuselage, and an optimizing module in communication with the central database and configured to generate an optimal design layout based on the selected feature setting.


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    Titel :

    DESIGN OPTIMIZER SYSTEM AND METHODS


    Weitere Titelangaben:

    PROCEDES ET SYSTEMES D'OPTIMISATEUR DE CONCEPTION


    Beteiligte:

    Erscheinungsdatum :

    2016-09-09


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B60N SEATS SPECIALLY ADAPTED FOR VEHICLES , Sitze besonders für Fahrzeuge ausgebildet / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / G06F ELECTRIC DIGITAL DATA PROCESSING , Elektrische digitale Datenverarbeitung



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