According to one implementation, a method of making design information of an aircraft structural object, executed by a computer, includes: setting at least one parameter as a variable for an optimization calculation which minimizes a weight of the structural object composing an aircraft; setting at least one allowable range for at least a strength of the structural object corresponding to the at least one parameter; and calculating an optimal value of the weight of the structural object and a value of the at least one parameter by the optimization calculation. The at least one parameter expresses the design information of the structural object. The at least one allowable range is set as at least one constraint condition of the optimization calculation. The value of the at least one parameter corresponds to the optimal value and meets the at least one allowable range.


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    Titel :

    AIRCRAFT STRUCTURAL OBJECT, METHOD OF MANUFACTURING AIRCRAFT STRUCTURAL OBJECT, METHOD OF MAKING DESIGN INFORMATION OF AIRCRAFT STRUCTURAL OBJECT, DESIGNING SYSTEM OF AIRCRAFT STRUCTURAL OBJECT AND RECORDING MEDIUM WITH DESIGN PROGRAM OF AIRCRAFT STRUCTURAL OBJECT RECORDED


    Beteiligte:

    Erscheinungsdatum :

    2016-09-29


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    G06F ELECTRIC DIGITAL DATA PROCESSING , Elektrische digitale Datenverarbeitung / 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



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