A hybrid heater system for aircraft wing ice protection is provided. The hybrid heater system includes a voltage source (102), a carbon nano-tube (CNT) heater (103), a first positive temperature coefficient (PTC) heater (104) disposed in parallel with the CNT heater to form a parallel formation (105) and a second PTC heater (106) disposed in series between the voltage source and the parallel formation.


    Access

    Download


    Export, share and cite



    Title :

    HYBRID HEATER FOR AIRCRAFT WING ICE PROTECTION


    Additional title:

    HYBRIDHEIZUNG FÜR DEN EISSCHUTZ VON FLUGZEUGFLÜGELN
    APPAREIL DE CHAUFFAGE HYBRIDE POUR LA PROTECTION DES AILES D'AVION CONTRE LE GIVRE


    Contributors:

    Publication date :

    2020-03-18


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



    HYBRID HEATER FOR AIRCRAFT WING ICE PROTECTION

    JACOB ROBIN / MAHAPATRA GURU PRASAD | European Patent Office | 2020

    Free access

    Hybrid heater for aircraft wing ice protection

    JACOB ROBIN / MAHAPATRA GURU PRASAD | European Patent Office | 2022

    Free access

    Enclosure for Contacts of Aircraft Wing Heater Blanket

    TORSKE NICHOLAS ALLEN | European Patent Office | 2020

    Free access

    Enclosure for contacts of aircraft wing heater blanket

    TORSKE NICHOLAS ALLEN | European Patent Office | 2024

    Free access

    Enclosure for contacts of aircraft wing heater blanket

    TORSKE NICHOLAS ALLEN | European Patent Office | 2022

    Free access