A repair system for gas turbine engine components includes a computer system configured to receive a set of measured parameters for each gas turbine engine component in a plurality of substantially identical gas turbine engine components, and determine a variation model based on the set of measured parameters wherein each of the gas turbine engine components is an as-run component and has been exposed to a substantially identical general wear pattern. The computer system includes at least one simulated engine model. The simulated engine model is configured to determine a predicted operation of each gas turbine engine component in the plurality of substantially identical gas turbine engine components. A correlation system is configured to correlate variations in the set of parameters for each of the gas turbine engine components in the plurality of substantially identical gas turbine engine components with a set of the predicted operations of each gas turbine engine component in the plurality of substantially identical gas turbine engine components, thereby generating a predictive model based on the variations. A repair module is configured to generate a repair formula based on the predictive model. The repair formula is configured to receive a set of measured parameters of an as-run gas turbine engine component and determine a suggested repair capable of repairing the as-run gas turbine engine component.


    Access

    Download


    Export, share and cite



    Title :

    AIRCRAFT COMPONENT REPAIR SYSTEM AND PROCESS


    Contributors:

    Publication date :

    2020-10-08


    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 / G01M TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES , Prüfen der statischen oder dynamischen Massenverteilung rotierender Teile von Maschinen oder Konstruktionen



    Aircraft component repair system and process

    SOMANATH NAGENDRA / HEINEMANN KURT R / SELIN EVAN et al. | European Patent Office | 2024

    Free access

    Aircraft component repair scheduling system and process

    SOMANATH NAGENDRA / HEINEMANN KURT R / SELIN EVAN et al. | European Patent Office | 2022

    Free access

    AIRCRAFT COMPONENT REPAIR SCHEDULING SYSTEM AND PROCESS

    SOMANATH NAGENDRA / HEINEMANN KURT R / SELIN EVAN et al. | European Patent Office | 2020

    Free access

    Aircraft repair

    Garbett, G.H.G. | Engineering Index Backfile | 1942


    In-situ corrosion prevention process for aircraft aluminum alloy component cracks after cold spraying reinforcement repair

    DAI XUETING / NAN JIAN / FAN XIN et al. | European Patent Office | 2020

    Free access