DE1004060675 A UPAB: 20060801 NOVELTY - The procedure involves using an electromechanical piezoelectric transducer (3). Deformation of the construction unit is done by suitable electrical control of the piezoelectric transducer in such a manner, that the ice formed on the component (1) is loosened from the component. DETAILED DESCRIPTION - An INDEPENDENT CLAIM is also included for the icing endangered component of an aircraft. USE - For deicing of a component in an aircraft e.g. for deicing of an airfoil wing of an airplane or a rotor blade of a helicopter. ADVANTAGE - Enables reliable and in particular long-term stable deicing with small energy expenditure with low system weight and low manufacturing cost.


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    Title :

    Enteisung von Fluggeraeten


    Contributors:
    Friedberger, A. (author) / Ziemann, T. (author) / Kloeppel, V. (author) / Schoenecker, A. (author) / Daue, T. (author)

    Publication date :

    2006


    Remarks:

    Patentblatt, Vol.126 (2006), No.25


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    German



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