A deicing assembly(18) includes a pneumatic deicing apparatus (24) configured for attachment to a leading edge of an aircraft surface (12), the pneumatic deicing assembly having a plurality of inflatable chambers (30), and a carbon allotrope heater (26) having at least one sheet of a carbon allotrope material.


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    Title :

    COMBINED ELECTRO-THERMAL AND PNEUMATIC BOOT DEICING SYSTEM


    Additional title:

    KOMBINIERTES ELEKTROTHERMISCHES UND PNEUMATISCHES GUMMIMATTEN-ENTEISUNGSSYSTEM
    SYSTÈME DE DÉGIVRAGE DE CHAUSSURE PNEUMATIQUE ET ÉLECTROTHERMIQUE COMBINÉ


    Contributors:

    Publication date :

    2022-01-26


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    COMBINED ELECTRO-THERMAL AND PNEUMATIC BOOT DEICING SYSTEM

    CHAUDHRY ZAFFIR A / ZHAO WENPING / BOTURA GALDEMIR CEZAR et al. | European Patent Office | 2018

    Free access

    Pneumatic boot for helicopter rotor deicing

    Blaha, B. J. / Evanich, P. L. | NTRS | 1981




    JUH-1H Pneumatic Boot Deicing System Flight Test Evaluation

    L. A. Haworth / R. G. Oliver / R. Woratschek | NTIS | 1983