PROBLEM TO BE SOLVED: To provide a heating element for in-flight de-icing of aircraft which does not damage components being fiber composite structures and requires only small amounts of energy.SOLUTION: A heating element 100' includes a carbon fiber material 110' that is designed to be arranged on a component 300 of an aircraft. The carbon fiber material includes at least two electrical contacts 120 for connecting to an electrical wiring system, and at least one insulation layer 130' for electrical insulation.SELECTED DRAWING: Figure 3

    【課題】繊維複合構造である構成部品を損傷せず、且つ必要エネルギーの少ない、航空機の飛行中の除氷のための加熱要素を提供する。【解決手段】加熱要素100’は、航空機の構成部品300上に配されるように設計された炭素繊維材料110’を備えている。該炭素繊維材料は、電気配線システムに接続するための少なくとも2つの電気接点120と、電気絶縁のための少なくとも1つの絶縁層130’とを備えている。【選択図】図3


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    Title :

    ELECTRICAL DE-ICING FOR AIRCRAFT


    Additional title:

    航空機用の電気的除氷


    Contributors:

    Publication date :

    2017-04-13


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Japanese


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B32B LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM , Schichtkörper, d.h. aus Ebenen oder gewölbten Schichten, z.B. mit zell- oder wabenförmiger Form, aufgebaute Erzeugnisse / B64C AEROPLANES , Flugzeuge



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