A propeller blade for rotation about a hub assembly is provided, wherein the propeller blade defines a radial direction along its length from a blade root to a blade tip, the propeller blade including a radially inner region, a radially outer region located between the blade root and the blade tip at a position where rotational forces on the blade are sufficient, in use, to remove ice from an uncoated blade, a coating disposed at least along a leading edge of the propeller blade, the coating including an icephobic material, wherein the coating extends along the propeller blade from the radially inner region to the radially outer region.


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    Title :

    PROPELLER BLADES HAVING ICEPHOBIC COATING


    Additional title:

    PALES D'HELICE COMPORTANT UN REVETEMENT GLACIOPHOBE


    Contributors:

    Publication date :

    2017-07-29


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / 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



    PROPELLER BLADES HAVING ICEPHOBIC COATING

    METHVEN PAUL NICHOLAS | European Patent Office | 2017

    Free access

    Propeller blades having icephobic coating

    PAUL NICHOLAS METHVEN | European Patent Office | 2017

    Free access

    PROPELLER BLADES HAVING ICEPHOBIC COATING

    METHVEN PAUL NICHOLAS | European Patent Office | 2017

    Free access

    PROPELLER BLADES HAVING ICEPHOBIC COATING

    PAUL NICHOLAS METHVEN | European Patent Office | 2017

    Free access

    Propeller blades having icephobic coating

    METHVEN PAUL NICHOLAS | European Patent Office | 2019

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