A method for deicing in a laser sensor window in an aerospace vehicle. A deicing laser beam is transmitted from a laser beam generator in the aerospace vehicle into the laser sensor window in the aerospace vehicle. The deicing laser beam has properties that remove ice from the laser sensor window. A sensor laser beam is transmitted from the laser beam generator through the laser sensor window.


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    Title :

    Self Deicing of Aircraft Windows using Lidar


    Contributors:

    Publication date :

    2025-01-16


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / G01S RADIO DIRECTION-FINDING , Funkpeilung