An anti-icing protection system for an aircraft engine nacelle, the nacelle comprising an inner shroud provided with at least one acoustic panel, an air intake lip forming a leading edge of the nacelle, the protection system comprising a heat exchanger device including at least one heat pipe configured to transfer heat emitted by a heat source to the acoustic panel or panels.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    AIRCRAFT ENGINE NACELLE COMPRISING AN ANTI-ICING PROTECTION SYSTEM


    Beteiligte:
    PORTE ALAIN (Autor:in) / LALANE JACQUES (Autor:in) / ALBET GREGORY (Autor:in) / ZEBIAN MAXIME (Autor:in) / BOURHIS ARNAUD (Autor:in)

    Erscheinungsdatum :

    2020-04-23


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



    Anti-icing system for an aircraft nacelle

    KROEGER DANIEL / PRETTY MICHAEL S / RAMLAOUI JIHAD | Europäisches Patentamt | 2022

    Freier Zugriff

    ANTI-ICING SYSTEM FOR AN AIRCRAFT NACELLE

    KROEGER DANIEL / PRETTY MICHAEL S / RAMLAOUI JIHAD | Europäisches Patentamt | 2020

    Freier Zugriff

    ANTI-ICING SYSTEM FOR AN AIRCRAFT NACELLE

    KROEGER DANIEL / PRETTY MICHAEL S / RAMLAOUI JIHAD | Europäisches Patentamt | 2022

    Freier Zugriff

    GAS TURBINE ENGINE NACELLE ANTI-ICING SYSTEM

    MARCHAJ IAN T | Europäisches Patentamt | 2018

    Freier Zugriff

    AIRCRAFT ENGINE NACELLE WITH ANTI-ICING SYSTEM USING TWO-PHASE FLUID

    ANTONIO MOSCATELLI / GIANNI MANCUSO | Europäisches Patentamt | 2020

    Freier Zugriff