A propeller blade (18) for rotation about a hub assembly (19) is provided, wherein the propeller blade (18) defines a radial direction (26) along its length (25) from a blade root (28) to a blade tip (30), the propeller blade (18) including a radially inner region (32), a radially outer region (36) located between the blade root (28) and the blade tip (30) at a position where rotational forces on the blade (18) are sufficient, in use, to remove ice from an uncoated blade, a coating (40) disposed at least along a leading edge (38) of the propeller blade (18), the coating (40) including an icephobic material, wherein the coating (40) extends along the propeller blade (18) from the radially inner region (32) to the radially outer region (36).


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    Titel :

    PROPELLER BLADES HAVING ICEPHOBIC COATING


    Weitere Titelangaben:

    PROPELLERBLÄTTER MIT EISABSTOSSENDER BESCHICHTUNG
    PALES D'HÉLICE DOTÉES DE REVÊTEMENT GLACIOPHOBE


    Beteiligte:

    Erscheinungsdatum :

    02.08.2017


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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    METHVEN PAUL NICHOLAS | Europäisches Patentamt | 2017

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    Propeller blades having icephobic coating

    PAUL NICHOLAS METHVEN | Europäisches Patentamt | 2017

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    PROPELLER BLADES HAVING ICEPHOBIC COATING

    PAUL NICHOLAS METHVEN | Europäisches Patentamt | 2017

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    PROPELLER BLADES HAVING ICEPHOBIC COATING

    METHVEN PAUL NICHOLAS | Europäisches Patentamt | 2017

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    Propeller blades having icephobic coating

    METHVEN PAUL NICHOLAS | Europäisches Patentamt | 2019

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