A de-icing assembly includes an aircraft with an airfoil. A de-icer is disposed on a leading, edge of the airfoil. A tab extends from the de-icer in an aft direction from an aft edge of the de-icer. The de-icer and the tab are adhesively attached onto an outer skin of the airfoil. A supercooled large droplet sensor is built into the tab. The supercooled large droplet sensor is positioned in a location aft of the aft edge of the de-icer.


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    Title :

    PNEUMATIC DE-ICER WITH SENSOR FOR SUPERCOOLED LARGE DROPLET ICING DETECTION


    Additional title:

    DEGIVREUR PNEUMATIQUE DOTE D'UN CAPTEUR DESTINE A LA DETECTION DE GIVRAGE PAR GROSSE GOUTTELETTE SUPER REFROIDIE


    Contributors:

    Publication date :

    2017-10-01


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    PNEUMATIC DE-ICER WITH SENSOR FOR SUPERCOOLED LARGE DROPLET ICING DETECTION

    PUTT JAMES C | European Patent Office | 2019

    Free access

    PNEUMATIC DE-ICER WITH SENSOR FOR SUPERCOOLED LARGE DROPLET ICING DETECTION

    PUTT JAMES C | European Patent Office | 2017

    Free access

    Pneumatic de-icer

    Gulick, J.E. | Engineering Index Backfile | 1944


    THE PNEUMATIC DE-ICER

    Gulick, J. E. | SAE Technical Papers | 1944


    ELECTRO-PNEUMATIC DE-ICER

    WIEGERS ROBERT GLYNN / SCHROEDER CRISTOPHER ROBERT | European Patent Office | 2018

    Free access