Apparatuses for and methods of deicing aircraft surfaces, engine inlets, windmill blades and other structures. Deicing apparatuses can comprise at least one standoff coupled with an actuator and a first region of an inner surface of a skin. A standoff can act as a moment arm and can create efficient, tailorable skin bending and acceleration, breaking an ice to skin bond. Integral as well as modular leading edges can comprise deicing apparatuses.


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    Titel :

    Electro-expulsive deicing apparatuses comprising at least one standoff


    Beteiligte:
    LENKEY PETER (Autor:in)

    Erscheinungsdatum :

    2018-06-19


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



    Deicing Apparatuses Comprising at least one standoff

    LENKEY PETER | Europäisches Patentamt | 2018

    Freier Zugriff

    Deicing apparatuses comprising at least one standoff

    LENKEY PETER | Europäisches Patentamt | 2018

    Freier Zugriff

    Deicing Apparatuses Comprising at least one standoff

    LENKEY PETER | Europäisches Patentamt | 2018

    Freier Zugriff


    Thermo-Mechanical Expulsive Deicing System - TMEDS AIAA Paper

    Al-Khalil, K. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2007