To provide a hybrid heater system for aircraft wing ice protection.SOLUTION: A hybrid heater system includes a voltage source, a carbon nano-tube (CNT) heater, a first positive temperature coefficient (PTC) heater disposed in parallel with the CNT heater to form a parallel formation, and a second PTC heater disposed in series between the voltage source and the parallel formation.SELECTED DRAWING: Figure 1

    【課題】 航空機のウイングの防除氷のためのハイブリッドヒータシステムを提供する。【解決手段】 ハイブリッドヒータシステムは、電圧源と、カーボンナノチューブ(CNT)ヒータと、並列構成を形成するように、CNTヒータに対して並列に配置された、第1の正の温度係数(PTC)ヒータと、電圧源と並列構成との間に直列に配置された第2のPTCヒータと、を備えている。【選択図】図1


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    Title :

    HYBRID HEATER SYSTEM


    Additional title:

    ハイブリッドヒータシステム


    Contributors:

    Publication date :

    2020-03-19


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Japanese


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / H05B ELECTRIC HEATING , Elektrische Heizung



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