Apparatus and associated methods relate to determining, based on a spatial extent of ice accretion, a maximum size of super-cooled droplets contained in an atmosphere and/or if an atmosphere contains super-cooled water droplets that equal and/or exceed a predetermined size. A testing region (46) on an exterior surface (48) of an aircraft is monitored for ice accretion by an ice detector. A boundary calculator (66) determines a specific location to be tested within the testing region. The determined specific location corresponds to a calculated boundary that separates an ice-accretion region (70) from an ice-free region if the atmosphere contains super-cooled water droplets of no larger than the predetermined size. If the ice detector detects ice accretion at the determined specific location, an alert is generated. The alert can advantageously inform a pilot of the aircraft that the atmosphere contains super-cooled water droplets that equal or exceed the predetermined size.


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    Title :

    AUTOMATED SUPER-COOLED WATER-DROPLET SIZE DIFFERENTIATION USING AIRCRAFT ACCRETION PATTERNS


    Additional title:

    AUTOMATISIERTE GRÖSSENUNTERSCHEIDUNG VON SUPERGEKÜHLTEN WASSERTROPFEN UNTER VERWENDUNG VON FLUGZEUGANLAGERUNGSMUSTERN
    DIFFÉRENCIATION DE TAILLE DE GOUTTELETTES D'EAU SUPER REFROIDIE AUTOMATISÉE AU MOYEN DE MOTIFS D'ACCRÉTION D'AÉRONEF


    Contributors:

    Publication date :

    2019-03-20


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / G08B SIGNALLING OR CALLING SYSTEMS , Signalisier- oder Rufsysteme



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