A heater mat for heating an airfoil having a chord, a leading edge, and a trailing edge includes a first zone element (200) configured to heat a first chord-wise segment of the airfoil. The system further includes a second zone element (202) configured to heat a second chord-wise segment of the airfoil that is adjacent to the first chord-wise segment of the airfoil. The system further includes a first zone busbar (300) located at the leading edge of the heater mat and electrically coupled to the first zone element.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    HIGH STRAIN TOLERANT CHORD-WISE ICE PROTECTION LAYOUT


    Weitere Titelangaben:

    HOCH-BELASTUNGSTOLERANTES PROFILTIEFEN EISSCHUTZLAYOUT
    AGENCEMENT DE PROTECTION CONTRE LA GLACE DANS LE SENS DE LA CORDE RÉSISTANT AUX CONTRAINTES ÉLEVÉES


    Beteiligte:
    ZADELL ALEX (Autor:in) / TAYLOR ANDREW (Autor:in)

    Erscheinungsdatum :

    30.08.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F03D Windkraftmaschinen , WIND MOTORS



    High strain tolerant chord-wise ice protection layout

    ZADELL ALEX / TAYLOR ANDREW | Europäisches Patentamt | 2022

    Freier Zugriff

    HIGH STRAIN TOLERANT CHORD-WISE ICE PROTECTION LAYOUT

    ZADELL ALEX / TAYLOR ANDREW | Europäisches Patentamt | 2021

    Freier Zugriff

    Chord-wise variable vortex generator

    BUSHMIRE TROY THOMAS | Europäisches Patentamt | 2021

    Freier Zugriff

    CHORD-WISE VARIABLE VORTEX GENERATOR

    BUSHMIRE TROY THOMAS | Europäisches Patentamt | 2020

    Freier Zugriff

    Two-dimensional Chord-wise Load Distributions at Transonic Speeds

    Lindsey, Walter F / Dick, Richard S | NTRS | 1952