The present invention relates to an aircraft component comprising: a composite material structure comprising a fibrous reinforcement embedded in a matrix; a heating element (9) configured to heat the component, the heating element (9) being embedded in a matrix of the composite material structure.

    本发明涉及一种飞行器部件,该飞行器部件包括:复合材料结构,该复合材料结构包括嵌入基体中的纤维增强件;加热元件(9),该加热元件被构造成对部件进行加热,该加热元件(9)嵌入复合材料结构的基体中。


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    Title :

    Blade deicing device


    Additional title:

    叶片除冰装置


    Contributors:

    Publication date :

    2024-11-01


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge / F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES



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