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


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    Titel :

    COMBINED ELECTRO-THERMAL AND PNEUMATIC BOOT DEICING SYSTEM


    Beteiligte:

    Erscheinungsdatum :

    2018-07-05


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    H05B ELECTRIC HEATING , Elektrische Heizung / B23P Sonstige Metallbearbeitung , OTHER WORKING OF METAL / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS



    COMBINED ELECTRO-THERMAL AND PNEUMATIC BOOT DEICING SYSTEM

    CHAUDHRY ZAFFIR A / ZHAO WENPING / BOTURA GALDEMIR CEZAR et al. | Europäisches Patentamt | 2022

    Freier Zugriff

    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